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

 
Date: May 25th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 ET - UTC (sec) : 68 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


160/13:47:39 077 -0 3 1 9 2 0
N/A 1 9 -0 2 220 2
000/00:05:18 153 0 2 -0 0 214 8

161/01:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 7

Coasting Arc #1 (Orbit 144)
---------------------------------------

Vector Time (GMT): 2016/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1081240
15                 A    =         6776592
42  meter
 Y    =        4307113
08  meter          E    =           
0015082
 Z    =       -5132298
32                 I    =           51
68134
 XDOT =      -7488
616798                 Wp   =          104
11474
 YDOT =         27
311705  meter/sec      RA   =          170
06445  deg
 ZDOT =       1600
931743                 TA   =          181
33690
                                          MA   =          181
34093
                                          Ha   =            220
651  n
mi
                                          Hp   =            213
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3547375
82                 X    =        -1104392
31
 Y    =       14130948
41  feet           Y    =         4294892
99  meter
 Z    =      -16838249
08                 Z    =        -5137606
56
 XDOT =     -24568
952749                 XDOT =       -7496
142332
 YDOT =         89
605331  feet/sec       YDOT =         -56
473228  meter/sec
 ZDOT =       5252
400732                 ZDOT =        1564
535340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10970366
59                 X    =         3343767
74
 Y    =        9545455
67  feet           Y    =         2909454
89  meter
 Z    =      -16862074
11                 Z    =        -5139560
19
 XDOT =     -10526
089249                 XDOT =       -3208
352003
 YDOT =      21093
937963  feet/sec       YDOT =        6429
432291  meter/sec
 ZDOT =       5094
029718                 ZDOT =        1552
660258


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   16146
51341461  
00016717  00000-0  10270-3 0  9000
2 25544  51
6412 171
1494 0001530 120
7050 239
4254 15
54665671  1457


Satellite: ISS
Catalog Number: 25544
Epoch time:      16146
51341461   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:       171
1494  deg
Eccentricity:     
0001530     
Arg of perigee:   120
7050  deg
Mean anomaly:     239
4254  deg
Mean motion:   15
54665671  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             145
Checksum:              271


Coasting Arc #2 (Orbit 160)
---------------------------------------

Vector Time (GMT): 2016/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2984797
98                 A    =         6779718
58  meter
 Y    =       -4304629
42  meter          E    =           
0010883
 Z    =        4296221
29                 I    =           51
72196
 XDOT =       6714
052713                 Wp   =           79
07514
 YDOT =       1106
208548  meter/sec      RA   =          165
06953  deg
 ZDOT =      -3546
581803                 TA   =           47
04037
                                          MA   =           46
94916
                                          Ha   =            220
556  n
mi
                                          Hp   =            213
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9792644
31                 X    =         3011842
29
 Y    =      -14122799
92  feet           Y    =        -4271100
61  meter
 Z    =       14095214
22                 Z    =         4310786
06
 XDOT =      22027
731998                 XDOT =        6718
411664
 YDOT =       3629
293137  feet/sec       YDOT =        1181
314256  meter/sec
 ZDOT =     -11635
767069                 ZDOT =       -3513
955749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8344876
29                 X    =        -2543518
29
 Y    =      -14963320
48  feet           Y    =        -4560820
08  meter
 Z    =       14159325
68                 Z    =         4315762
47
 XDOT =      11974
211081                 XDOT =        3649
739538
 YDOT =     -17584
034275  feet/sec       YDOT =       -5359
613647  meter/sec
 ZDOT =     -11493
972218                 ZDOT =       -3503
362732


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   16147
54187760  
00016717  00000-0  10270-3 0  9015
2 25544  51
6393 166
0186 0001637 120
9463 239
1851 15
54711862  1616


Satellite: ISS
Catalog Number: 25544
Epoch time:      16147
54187760   =   yrday
fracday
Element set:     901
Inclination:       51
6393  deg
RA of node:       166
0186  deg
Eccentricity:     
0001637     
Arg of perigee:   120
9463  deg
Mean anomaly:     239
1851  deg
Mean motion:   15
54711862  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             161
Checksum:              305


Coasting Arc #3 (Orbit 175)
---------------------------------------

Vector Time (GMT): 2016/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4535780
14                 A    =         6783909
25  meter
 Y    =        4104062
33  meter          E    =           
0005598
 Z    =       -2937203
97                 I    =           51
76807
 XDOT =      -5315
719590                 Wp   =           82
32117
 YDOT =      -2285
025603  meter/sec      RA   =          160
08876  deg
 ZDOT =       5024
938588                 TA   =          244
23935
                                          MA   =          244
29713
                                          Ha   =            220
580  n
mi
                                          Hp   =            213
214

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14881168
45                 X    =        -4567067
97
 Y    =       13464771
43  feet           Y    =         4053165
52  meter
 Z    =       -9636495
95                 Z    =        -2959313
39
 XDOT =     -17440
024900                 XDOT =       -5314
181856
 YDOT =      -7496
803161  feet/sec       YDOT =       -2344
461332  meter/sec
 ZDOT =      16486
018988                 ZDOT =        4999
119607

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5813818
62                 X    =         1772051
91
 Y    =       19159105
90  feet           Y    =         5839695
48  meter
 Z    =       -9733420
41                 Z    =        -2966746
54
 XDOT =     -12894
573631                 XDOT =       -3930
266043
 YDOT =      12216
634637  feet/sec       YDOT =        3723
630237  meter/sec
 ZDOT =      16374
031518                 ZDOT =        4990
804807


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   16148
50605941  
00016717  00000-0  10270-3 0  9029
2 25544  51
6407 161
2085 0001624 124
8859 235
2447 15
54707989  1764


Satellite: ISS
Catalog Number: 25544
Epoch time:      16148
50605941   =   yrday
fracday
Element set:     902
Inclination:       51
6407  deg
RA of node:       161
2085  deg
Eccentricity:     
0001624     
Arg of perigee:   124
8859  deg
Mean anomaly:     235
2447  deg
Mean motion:   15
54707989  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             176
Checksum:              317


Coasting Arc #4 (Orbit 191)
---------------------------------------

Vector Time (GMT): 2016/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5615569
18                 A    =         6787045
85  meter
 Y    =       -3615242
33  meter          E    =           
0015321
 Z    =        1165950
09                 I    =           51
80737
 XDOT =       3477
078509                 Wp   =          122
41605
 YDOT =       3488
392929  meter/sec      RA   =          155
12114  deg
 ZDOT =      -5882
032947                 TA   =           44
94432
                                          MA   =           44
82039
                                          Ha   =            220
597  n
mi
                                          Hp   =            213
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18423783
38                 X    =         5649914
66
 Y    =      -11861031
26  feet           Y    =        -3552253
34  meter
 Z    =        3825295
58                 Z    =         1193312
39
 XDOT =      11407
737889                 XDOT =        3466
384479
 YDOT =      11444
858692  feet/sec       YDOT =        3527
216546  meter/sec
 ZDOT =     -19298
008355                 ZDOT =       -5865
167845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3204007
28                 X    =         -976581
42
 Y    =      -21654651
49  feet           Y    =        -6600337
78  meter
 Z    =        3945015
72                 Z    =         1202440
79
 XDOT =      13604
891711                 XDOT =        4146
770993
 YDOT =      -5543
341007  feet/sec       YDOT =       -1689
610339  meter/sec
 ZDOT =     -19225
187410                 ZDOT =       -5859
837123


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   16149
53451640  
00016717  00000-0  10270-3 0  9039
2 25544  51
6397 156
0770 0001597 123
5579 236
5727 15
54704398  1923


Satellite: ISS
Catalog Number: 25544
Epoch time:      16149
53451640   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       156
0770  deg
Eccentricity:     
0001597     
Arg of perigee:   123
5579  deg
Mean anomaly:     236
5727  deg
Mean motion:   15
54704398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             192
Checksum:              326


Coasting Arc #5 (Orbit 207)
---------------------------------------

Vector Time (GMT): 2016/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6110051
76                 A    =         6787349
23  meter
 Y    =        2853300
05  meter          E    =           
0013480
 Z    =         718929
95                 I    =           51
83651
 XDOT =      -1432
131390                 Wp   =           59
36178
 YDOT =      -4591
356027  meter/sec      RA   =          150
16198  deg
 ZDOT =       5974
443792                 TA   =          308
38706
                                          MA   =          308
50807
                                          Ha   =            220
477  n
mi
                                          Hp   =            213
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20046101
57                 X    =        -6144996
23
 Y    =        9361220
62  feet           Y    =         2784777
95  meter
 Z    =        2358694
07                 Z    =          689163
99
 XDOT =      -4698
593799                 XDOT =       -1409
704677
 YDOT =     -15063
504024  feet/sec       YDOT =       -4607
246017  meter/sec
 ZDOT =      19601
193544                 ZDOT =        5967
541032

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         622177
78                 X    =          189639
79
 Y    =       22128899
77  feet           Y    =         6744888
65  meter
 Z    =        2228624
53                 Z    =          679284
76
 XDOT =     -14125
253239                 XDOT =       -4305
377187
 YDOT =      -1600
672823  feet/sec       YDOT =        -487
885076  meter/sec
 ZDOT =      19571
924170                 ZDOT =        5965
522487


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   16150
56296886  
00016717  00000-0  10270-3 0  9044
2 25544  51
6388 150
9467 0001578 135
8093 224
3186 15
54743356  2084


Satellite: ISS
Catalog Number: 25544
Epoch time:      16150
56296886   =   yrday
fracday
Element set:     904
Inclination:       51
6388  deg
RA of node:       150
9467  deg
Eccentricity:     
0001578     
Arg of perigee:   135
8093  deg
Mean anomaly:     224
3186  deg
Mean motion:   15
54743356  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             208
Checksum:              332


Coasting Arc #6 (Orbit 222)
---------------------------------------

Vector Time (GMT): 2016/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6035827
80                 A    =         6784987
44  meter
 Y    =       -1753420
67  meter          E    =           
0006794
 Z    =       -2552848
59                 I    =           51
85511
 XDOT =       -634
598104                 Wp   =          130
84199
 YDOT =       5506
054973  meter/sec      RA   =          145
19988  deg
 ZDOT =      -5295
760725                 TA   =           77
74442
                                          MA   =           77
66835
                                          Ha   =            220
596  n
mi
                                          Hp   =            213
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19802584
65                 X    =         6067387
13
 Y    =       -5752692
49  feet           Y    =        -1685747
44  meter
 Z    =       -8375487
51                 Z    =        -2523451
25
 XDOT =      -2082
014777                 XDOT =        -670
396297
 YDOT =      18064
484818  feet/sec       YDOT =        5498
758580  meter/sec
 ZDOT =     -17374
543060                 ZDOT =       -5298
930142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2254427
99                 X    =          687149
65
 Y    =      -20549596
89  feet           Y    =        -6263517
13  meter
 Z    =       -8247196
06                 Z    =        -2513745
36
 XDOT =      14447
679478                 XDOT =        4403
652705
 YDOT =       8545
788846  feet/sec       YDOT =        2604
756440  meter/sec
 ZDOT =     -17389
283605                 ZDOT =       -5300
253643


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   16151
52714459  
00016717  00000-0  10270-3 0  9053
2 25544  51
6384 146
1355 0001508 131
1667 228
9616 15
54698855  2230


Satellite: ISS
Catalog Number: 25544
Epoch time:      16151
52714459   =   yrday
fracday
Element set:     905
Inclination:       51
6384  deg
RA of node:       146
1355  deg
Eccentricity:     
0001508     
Arg of perigee:   131
1667  deg
Mean anomaly:     228
9616  deg
Mean motion:   15
54698855  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             223
Checksum:              317


Coasting Arc #7 (Orbit 238)
---------------------------------------

Vector Time (GMT): 2016/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5435370
49                 A    =         6780813
13  meter
 Y    =         412318
80  meter          E    =           
0011986
 Z    =        4025526
66                 I    =           51
86733
 XDOT =       2473
392749                 Wp   =          105
29978
 YDOT =      -6093
804715  meter/sec      RA   =          140
23008  deg
 ZDOT =       3950
940373                 TA   =          303
74673
                                          MA   =          303
86088
                                          Ha   =            220
516  n
mi
                                          Hp   =            213
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17832580
33                 X    =        -5459131
67
 Y    =        1352751
97  feet           Y    =          351403
81  meter
 Z    =       13207108
46                 Z    =         3999064
99
 XDOT =       8114
805608                 XDOT =        2522
159187
 YDOT =     -19992
797620  feet/sec       YDOT =       -6065
873125  meter/sec
 ZDOT =      12962
402800                 ZDOT =        3963
073769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5287297
71                 X    =        -1611568
34
 Y    =       17172867
59  feet           Y    =         5234290
04  meter
 Z    =       13091817
08                 Z    =         3990385
85
 XDOT =     -14421
765036                 XDOT =       -4395
753983
 YDOT =     -14395
751352  feet/sec       YDOT =       -4387
825012  meter/sec
 ZDOT =      13016
283822                 ZDOT =        3967
363309


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   16152
55559127  
00016717  00000-0  10270-3 0  9067
2 25544  51
6385 141
0047 0001339 139
3519 220
7734 15
54732255  2392


Satellite: ISS
Catalog Number: 25544
Epoch time:      16152
55559127   =   yrday
fracday
Element set:     906
Inclination:       51
6385  deg
RA of node:       141
0047  deg
Eccentricity:     
0001339     
Arg of perigee:   139
3519  deg
Mean anomaly:     220
7734  deg
Mean motion:   15
54732255  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             239
Checksum:              303


Coasting Arc #8 (Orbit 253)
---------------------------------------

Vector Time (GMT): 2016/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4429519
18                 A    =         6777142
56  meter
 Y    =        1146314
60  meter          E    =           
0013302
 Z    =       -5011522
43                 I    =           51
87816
 XDOT =      -3957
619289                 Wp   =           79
92789
 YDOT =       6219
447116  meter/sec      RA   =          135
24808  deg
 ZDOT =      -2077
818018                 TA   =          169
91325
                                          MA   =          169
88653
                                          Ha   =            220
481  n
mi
                                          Hp   =            213
528

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14532543
24                 X    =         4440715
76
 Y    =        3760874
67  feet           Y    =         1195911
35  meter
 Z    =      -16442002
74                 Z    =        -4989977
36
 XDOT =     -12984
315253                 XDOT =       -4016
779273
 YDOT =      20405
010222  feet/sec       YDOT =        6174
859729  meter/sec
 ZDOT =      -6816
988249                 ZDOT =       -2097
186729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8636593
35                 X    =         2632433
65
 Y    =      -12402343
39  feet           Y    =        -3780234
27  meter
 Z    =      -16348381
55                 Z    =        -4982986
70
 XDOT =      13693
288401                 XDOT =        4173
714305
 YDOT =      18623
588640  feet/sec       YDOT =        5676
469818  meter/sec
 ZDOT =      -6902
412964                 ZDOT =       -2103
855471


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   16153
51975941  
00016717  00000-0  10270-3 0  9071
2 25544  51
6377 136
1934 0001358 134
9659 225
1604 15
54705343  2540


Satellite: ISS
Catalog Number: 25544
Epoch time:      16153
51975941   =   yrday
fracday
Element set:     907
Inclination:       51
6377  deg
RA of node:       136
1934  deg
Eccentricity:     
0001358     
Arg of perigee:   134
9659  deg
Mean anomaly:     225
1604  deg
Mean motion:   15
54705343  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             254
Checksum:              315


Coasting Arc #9 (Orbit 269)
---------------------------------------

Vector Time (GMT): 2016/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3154694
60                 A    =         6775660
23  meter
 Y    =       -2742531
74  meter          E    =           
0003339
 Z    =        5329789
10                 I    =           51
89533
 XDOT =       4987
431290                 Wp   =          107
28929
 YDOT =      -5830
014718  meter/sec      RA   =          130
26024  deg
 ZDOT =        -48
820099                 TA   =          343
16850
                                          MA   =          343
17957
                                          Ha   =            220
527  n
mi
                                          Hp   =            213
461

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10350047
89                 X    =        -3149682
70
 Y    =       -8997807
54  feet           Y    =        -2777782
04  meter
 Z    =       17486184
71                 Z    =         5314476
08
 XDOT =      16362
963549                 XDOT =        5052
490447
 YDOT =     -19127
344874  feet/sec       YDOT =       -5773
878169  meter/sec
 ZDOT =       -160
170928                 ZDOT =         -24
434455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11968212
06                 X    =        -3647911
04
 Y    =        6867090
02  feet           Y    =         2093089
04  meter
 Z    =       17419978
82                 Z    =         5309609
55
 XDOT =     -12081
183994                 XDOT =       -3682
344881
 YDOT =     -20929
088265  feet/sec       YDOT =       -6379
186103  meter/sec
 ZDOT =        -52
945280                 ZDOT =         -16
137721


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   16154
54820232  
00016717  00000-0  10270-3 0  9088
2 25544  51
6375 131
0621 0001278 142
1322 217
9921 15
54707455  2709


Satellite: ISS
Catalog Number: 25544
Epoch time:      16154
54820232   =   yrday
fracday
Element set:     908
Inclination:       51
6375  deg
RA of node:       131
0621  deg
Eccentricity:     
0001278     
Arg of perigee:   142
1322  deg
Mean anomaly:     217
9921  deg
Mean motion:   15
54707455  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             270
Checksum:              281


Coasting Arc #10 (Orbit 284)
---------------------------------------

Vector Time (GMT): 2016/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1773684
46                 A    =         6777190
31  meter
 Y    =        4252416
61  meter          E    =           
0013482
 Z    =       -4982485
03                 I    =           51
92160
 XDOT =      -5515
982386                 Wp   =          109
10390
 YDOT =       4847
923723  meter/sec      RA   =          125
27362  deg
 ZDOT =       2174
471458                 TA   =          182
03559
                                          MA   =          182
04108
                                          Ha   =            220
385  n
mi
                                          Hp   =            213
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5819174
74                 X    =         1750204
20
 Y    =       13951498
06  feet           Y    =         4272120
36  meter
 Z    =      -16346735
66                 Z    =        -4973925
36
 XDOT =     -18097
055071                 XDOT =       -5580
345937
 YDOT =      15905
261559  feet/sec       YDOT =        4785
880233  meter/sec
 ZDOT =       7134
092709                 ZDOT =        2147
519926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15108448
46                 X    =         4605055
09
 Y    =       -1197754
85  feet           Y    =         -365075
68  meter
 Z    =      -16310212
39                 Z    =        -4971352
74
 XDOT =       9248
578339                 XDOT =        2818
966678
 YDOT =      21146
748248  feet/sec       YDOT =        6445
528866  meter/sec
 ZDOT =       7015
842198                 ZDOT =        2138
428702


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   16155
51236309  
00016717  00000-0  10270-3 0  9093
2 25544  51
6386 126
2513 0001208 142
9433 217
1804 15
54706213  2850


Satellite: ISS
Catalog Number: 25544
Epoch time:      16155
51236309   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:       126
2513  deg
Eccentricity:     
0001208     
Arg of perigee:   142
9433  deg
Mean anomaly:     217
1804  deg
Mean motion:   15
54706213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             285
Checksum:              287


Coasting Arc #11 (Orbit 300)
---------------------------------------

Vector Time (GMT): 2016/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -397582
49                 A    =         6780879
71  meter
 Y    =       -5476976
37  meter          E    =           
0011472
 Z    =        3969047
94                 I    =           51
95203
 XDOT =       5607
922368                 Wp   =           84
68789
 YDOT =      -3338
861623  meter/sec      RA   =          120
29694  deg
 ZDOT =      -4034
592900                 TA   =           47
25085
                                          MA   =           47
15437
                                          Ha   =            220
327  n
mi
                                          Hp   =            213
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1304404
48                 X    =         -355588
20
 Y    =      -17969082
57  feet           Y    =        -5481188
09  meter
 Z    =       13021810
82                 Z    =         3967217
87
 XDOT =      18398
695434                 XDOT =        5664
440138
 YDOT =     -10954
270417  feet/sec       YDOT =       -3275
833591  meter/sec
 ZDOT =     -13236
853348                 ZDOT =       -4007
213783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17554286
69                 X    =        -5350546
58
 Y    =       -4076545
28  feet           Y    =        -1242531
00  meter
 Z    =       13014828
23                 Z    =         3966919
65
 XDOT =      -5190
521755                 XDOT =       -1582
071031
 YDOT =     -19641
751734  feet/sec       YDOT =       -5986
805928  meter/sec
 ZDOT =     -13116
988205                 ZDOT =       -3998
058005


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   16156
54079831  
00016717  00000-0  10270-3 0  9104
2 25544  51
6386 121
1199 0001089 145
0708 215
0516 15
54735718  3018


Satellite: ISS
Catalog Number: 25544
Epoch time:      16156
54079831   =   yrday
fracday
Element set:     910
Inclination:       51
6386  deg
RA of node:       121
1199  deg
Eccentricity:     
0001089     
Arg of perigee:   145
0708  deg
Mean anomaly:     215
0516  deg
Mean motion:   15
54735718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             301
Checksum:              296


Coasting Arc #12 (Orbit 315)
---------------------------------------

Vector Time (GMT): 2016/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -831316
53                 A    =         6785012
75  meter
 Y    =        6265186
72  meter          E    =           
0005293
 Z    =       -2468004
41                 I    =           51
98141
 XDOT =      -5298
660601                 Wp   =           60
53247
 YDOT =       1403
064876  meter/sec      RA   =          115
33435  deg
 ZDOT =       5357
704285                 TA   =          271
96920
                                          MA   =          272
02982
                                          Ha   =            220
301  n
mi
                                          Hp   =            213
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2727416
45                 X    =         -889325
03
 Y    =       20555074
55  feet           Y    =         6255566
39  meter
 Z    =       -8097127
34                 Z    =        -2472182
80
 XDOT =     -17384
057090                 XDOT =       -5339
981867
 YDOT =       4603
231220  feet/sec       YDOT =        1343
579941  meter/sec
 ZDOT =      17577
769965                 ZDOT =        5331
864310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18947151
98                 X    =         5775091
92
 Y    =        8404856
88  feet           Y    =         2561800
38  meter
 Z    =       -8116475
48                 Z    =        -2473901
73
 XDOT =         56
725485                 XDOT =          17
289928
 YDOT =      16702
589275  feet/sec       YDOT =        5090
949211  meter/sec
 ZDOT =      17464
942361                 ZDOT =        5323
314432


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   16157
50495452  
00016717  00000-0  10270-3 0  9113
2 25544  51
6389 116
3097 0001096 149
2786 210
8432 15
54718993  3166


Satellite: ISS
Catalog Number: 25544
Epoch time:      16157
50495452   =   yrday
fracday
Element set:     911
Inclination:       51
6389  deg
RA of node:       116
3097  deg
Eccentricity:     
0001096     
Arg of perigee:   149
2786  deg
Mean anomaly:     210
8432  deg
Mean motion:   15
54718993  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             316
Checksum:              323


Coasting Arc #13 (Orbit 331)
---------------------------------------

Vector Time (GMT): 2016/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1897503
21                 A    =         6787400
63  meter
 Y    =       -6480601
02  meter          E    =           
0014078
 Z    =         612473
67                 I    =           52
00435
 XDOT =       4705
867814                 Wp   =          130
46541
 YDOT =        802
662494  meter/sec      RA   =          110
38283  deg
 ZDOT =      -6004
860671                 TA   =           42
95268
                                          MA   =           42
84284
                                          Ha   =            220
246  n
mi
                                          Hp   =            213
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6225404
23                 X    =         1966854
74
 Y    =      -21261814
36  feet           Y    =        -6458994
19  meter
 Z    =        2009428
04                 Z    =          621858
82
 XDOT =      15439
198865                 XDOT =        4725
711630
 YDOT =       2633
407133  feet/sec       YDOT =         855
398457  meter/sec
 ZDOT =     -19700
986452                 ZDOT =       -5981
952332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18823947
33                 X    =        -5737539
15
 Y    =      -11675123
06  feet           Y    =        -3558577
51  meter
 Z    =        2051515
83                 Z    =          625302
02
 XDOT =       5849
451995                 XDOT =        1782
912968
 YDOT =     -12921
382184  feet/sec       YDOT =       -3938
437290  meter/sec
 ZDOT =     -19601
323446                 ZDOT =       -5974
483386


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   16158
53338423  
00016717  00000-0  10270-3 0  9122
2 25544  51
6408 111
1781 0001056 156
0269 204
0934 15
54735960  3322


Satellite: ISS
Catalog Number: 25544
Epoch time:      16158
53338423   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:       111
1781  deg
Eccentricity:     
0001056     
Arg of perigee:   156
0269  deg
Mean anomaly:     204
0934  deg
Mean motion:   15
54735960  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             332
Checksum:              288


Coasting Arc #14 (Orbit 347)
---------------------------------------

Vector Time (GMT): 2016/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2721917
60                 A    =         6786841
07  meter
 Y    =        6075226
81  meter          E    =           
0013671
 Z    =        1289229
55                 I    =           52
01270
 XDOT =      -3920
693705                 Wp   =           63
44127
 YDOT =      -3010
199375  meter/sec      RA   =          105
43551  deg
 ZDOT =       5865
390076                 TA   =          310
51821
                                          MA   =          310
63722
                                          Ha   =            220
216  n
mi
                                          Hp   =            213
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8930175
85                 X    =        -2795912
53
 Y    =       19931846
50  feet           Y    =         6044374
61  meter
 Z    =        4229755
74                 Z    =         1275828
27
 XDOT =     -12863
168323                 XDOT =       -3915
233031
 YDOT =      -9875
982200  feet/sec       YDOT =       -3054
013459  meter/sec
 ZDOT =      19243
405760                 ZDOT =        5846
357177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17046253
31                 X    =         5195698
01
 Y    =       13673032
64  feet           Y    =         4167540
35  meter
 Z    =        4170228
54                 Z    =         1271085
66
 XDOT =     -11820
463367                 XDOT =       -3602
877234
 YDOT =       8850
079869  feet/sec       YDOT =        2697
504344  meter/sec
 ZDOT =      19161
031815                 ZDOT =        5840
282497


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   16159
56180952  
00016717  00000-0  10270-3 0  9139
2 25544  51
6406 106
0473 0001036 156
9897 203
1303 15
54750040  3488


Satellite: ISS
Catalog Number: 25544
Epoch time:      16159
56180952   =   yrday
fracday
Element set:     913
Inclination:       51
6406  deg
RA of node:       106
0473  deg
Eccentricity:     
0001036     
Arg of perigee:   156
9897  deg
Mean anomaly:     203
1303  deg
Mean motion:   15
54750040  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             348
Checksum:              291


Coasting Arc #15 (Orbit 362)
---------------------------------------

Vector Time (GMT): 2016/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3362154
55                 A    =         6783579
32  meter
 Y    =       -5035469
75  meter          E    =           
0005157
 Z    =       -3060007
02                 I    =           52
01002
 XDOT =       3008
073776                 Wp   =          116
72776
 YDOT =       5014
582239  meter/sec      RA   =          100
48286  deg
 ZDOT =      -4955
450971                 TA   =           98
18453
                                          MA   =           98
12603
                                          Ha   =            220
184  n
mi
                                          Hp   =            213
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11030690
80                 X    =         3433076
70
 Y    =      -16520570
05  feet           Y    =        -4997474
97  meter
 Z    =      -10039393
12                 Z    =        -3043502
93
 XDOT =       9869
008452                 XDOT =        2975
847259
 YDOT =      16452
041467  feet/sec       YDOT =        5048
040948  meter/sec
 ZDOT =     -16258
041243                 ZDOT =       -4940
916198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13462239
48                 X    =        -4103290
59
 Y    =      -14657123
19  feet           Y    =        -4467491
15  meter
 Z    =       -9966525
80                 Z    =        -3037797
06
 XDOT =      17260
516907                 XDOT =        5261
005553
 YDOT =      -4860
207937  feet/sec       YDOT =       -1481
391379  meter/sec
 ZDOT =     -16195
642647                 ZDOT =       -4936
431879


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   16160
52595650  
00016717  00000-0  10270-3 0  9143
2 25544  51
6411 101
2371 0000930 159
3973 200
7217 15
54759193  3634


Satellite: ISS
Catalog Number: 25544
Epoch time:      16160
52595650   =   yrday
fracday
Element set:     914
Inclination:       51
6411  deg
RA of node:       101
2371  deg
Eccentricity:     
0000930     
Arg of perigee:   159
3973  deg
Mean anomaly:     200
7217  deg
Mean motion:   15
54759193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             363
Checksum:              291


Coasting Arc #16 (Orbit 363)
---------------------------------------

Vector Time (GMT): 2016/160/13:50:18
153
Vector Time (MET): N/A
Weight (LBS)     : 923904
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3711583
16                 A    =         6777275
60  meter
 Y    =        2307279
34  meter          E    =           
0012799
 Z    =       -5191307
29                 I    =           51
98723
 XDOT =      -2410
576147                 Wp   =          105
58757
 YDOT =       7125
365763  meter/sec      RA   =          100
06722  deg
 ZDOT =       1443
012423                 TA   =          178
24966
                                          MA   =          178
24518
                                          Ha   =            220
164  n
mi
                                          Hp   =            214
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12177110
10                 X    =         3710723
78
 Y    =        7569814
12  feet           Y    =         2348780
57  meter
 Z    =      -17031848
08                 Z    =        -5173279
21
 XDOT =      -7908
714392                 XDOT =       -2497
084122
 YDOT =      23377
184262  feet/sec       YDOT =        7097
925224  meter/sec
 ZDOT =       4734
292728                 ZDOT =        1431
093245

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4346603
04                 X    =         1324844
61
 Y    =      -13760321
14  feet           Y    =        -4194145
88  meter
 Z    =      -16953717
86                 Z    =        -5167493
20
 XDOT =      23604
018701                 XDOT =        7194
504900
 YDOT =       1687
085679  feet/sec       YDOT =         514
223715  meter/sec
 ZDOT =       4681
012173                 ZDOT =        1426
772510


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   16160
59023361  
00016717  00000-0  10270-3 0  9156
2 25544  51
6425 100
9167 0001484 236
6937 123
4073 15
54387626  3642


Satellite: ISS
Catalog Number: 25544
Epoch time:      16160
59023361   =   yrday
fracday
Element set:     915
Inclination:       51
6425  deg
RA of node:       100
9167  deg
Eccentricity:     
0001484     
Arg of perigee:   236
6937  deg
Mean anomaly:     123
4073  deg
Mean motion:   15
54387626  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             364
Checksum:              302


Coasting Arc #17 (Orbit 371)
---------------------------------------

Vector Time (GMT): 2016/161/01:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 923904
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4230478
45                 A    =         6776872
42  meter
 Y    =         628088
80  meter          E    =           
0003758
 Z    =        5255905
60                 I    =           51
98959
 XDOT =        193
045671                 Wp   =          153
03959
 YDOT =      -7594
152101  meter/sec      RA   =           97
71328  deg
 ZDOT =       1059
339335                 TA   =          286
84413
                                          MA   =          286
88534
                                          Ha   =            220
240  n
mi
                                          Hp   =            214
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13879522
48                 X    =        -4262718
30
 Y    =        2060658
80  feet           Y    =          580599
91  meter
 Z    =       17243784
77                 Z    =         5235276
84
 XDOT =        633
351938                 XDOT =         272
805244
 YDOT =     -24915
197181  feet/sec       YDOT =       -7591
547494  meter/sec
 ZDOT =       3475
522752                 ZDOT =        1060
469955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3661871
78                 X    =        -1116138
52
 Y    =      -13659230
20  feet           Y    =        -4163333
36  meter
 Z    =       17153766
28                 Z    =         5228467
96
 XDOT =      23823
055973                 XDOT =        7261
267461
 YDOT =      -1999
264901  feet/sec       YDOT =        -609
375942  meter/sec
 ZDOT =       3481
881443                 ZDOT =        1061
277464


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   16161
10456219  
00016717  00000-0  10270-3 0  9167
2 25544  51
6433  98
3487 0001944 227
4991 132
5998 15
54419677  3723


Satellite: ISS
Catalog Number: 25544
Epoch time:      16161
10456219   =   yrday
fracday
Element set:     916
Inclination:       51
6433  deg
RA of node:        98
3487  deg
Eccentricity:     
0001944     
Arg of perigee:   227
4991  deg
Mean anomaly:     132
5998  deg
Mean motion:   15
54419677  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             372
Checksum:              334
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