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

 
Date: July 20th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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


217/02:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 212 7

Coasting Arc #1 (Orbit 1015)
---------------------------------------

Vector Time (GMT): 2016/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2226869
66                 A    =         6787354
07  meter
 Y    =       -6404861
95  meter          E    =           
0013900
 Z    =          -8595
91                 I    =           51
30901
 XDOT =       4529
175644                 Wp   =           47
21215
 YDOT =      -1574
469750  meter/sec      RA   =          250
88641  deg
 ZDOT =       5987
111106                 TA   =          312
69479
                                          MA   =          312
81178
                                          Ha   =            220
516  n
mi
                                          Hp   =            213
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7306002
81                 X    =        -2155041
62
 Y    =      -21013326
60  feet           Y    =        -6429362
67  meter
 Z    =         -28201
80                 Z    =          -19239
36
 XDOT =      14859
500145                 XDOT =        4517
362921
 YDOT =      -5165
583169  feet/sec       YDOT =       -1523
888045  meter/sec
 ZDOT =      19642
752973                 ZDOT =        6009
083447

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15167612
41                 X    =        -4623088
26
 Y    =       16275027
16  feet           Y    =         4960628
28  meter
 Z    =         -73429
42                 Z    =          -22381
29
 XDOT =     -10260
482026                 XDOT =       -3127
394921
 YDOT =      -9508
373138  feet/sec       YDOT =       -2898
152133  meter/sec
 ZDOT =      19738
790621                 ZDOT =        6016
383381


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   16202
50004597  
00016717  00000-0  10270-3 0  9008
2 25544  51
6405 251
8313 0001866  58
1247 302
0088 15
54808031 10168


Satellite: ISS
Catalog Number: 25544
Epoch time:      16202
50004597   =   yrday
fracday
Element set:     900
Inclination:       51
6405  deg
RA of node:       251
8313  deg
Eccentricity:     
0001866     
Arg of perigee:    58
1247  deg
Mean anomaly:     302
0088  deg
Mean motion:   15
54808031  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1016
Checksum:              270


Coasting Arc #2 (Orbit 1031)
---------------------------------------

Vector Time (GMT): 2016/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1171151
85                 A    =         6785598
36  meter
 Y    =        6397819
82  meter          E    =           
0007695
 Z    =       -1929020
93                 I    =           51
31570
 XDOT =      -5212
691129                 Wp   =          127
31834
 YDOT =       -720
576254  meter/sec      RA   =          245
88901  deg
 ZDOT =      -5574
557648                 TA   =           74
04370
                                          MA   =           73
95894
                                          Ha   =            220
471  n
mi
                                          Hp   =            212
863

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3842361
72                 X    =         1108892
93
 Y    =       20990222
52  feet           Y    =         6410568
44  meter
 Z    =       -6328808
83                 Z    =        -1923482
67
 XDOT =     -17102
005018                 XDOT =       -5177
167820
 YDOT =      -2364
095320  feet/sec       YDOT =        -778
669049  meter/sec
 ZDOT =     -18289
231130                 ZDOT =       -5599
792835

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16515129
47                 X    =         5033811
46
 Y    =      -13523840
96  feet           Y    =        -4122066
72  meter
 Z    =       -6305809
27                 Z    =        -1922010
66
 XDOT =       5131
426121                 XDOT =        1564
058682
 YDOT =      14814
815931  feet/sec       YDOT =        4515
555896  meter/sec
 ZDOT =     -18399
084710                 ZDOT =       -5608
041020


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   16203
52839707  
00016717  00000-0  10270-3 0  9011
2 25544  51
6410 246
6989 0001865  66
2452 293
8897 15
54871509 10325


Satellite: ISS
Catalog Number: 25544
Epoch time:      16203
52839707   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:       246
6989  deg
Eccentricity:     
0001865     
Arg of perigee:    66
2452  deg
Mean anomaly:     293
8897  deg
Mean motion:   15
54871509  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1032
Checksum:              330


Coasting Arc #3 (Orbit 1047)
---------------------------------------

Vector Time (GMT): 2016/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          63429
94                 A    =         6781786
35  meter
 Y    =       -5758842
56  meter          E    =           
0013919
 Z    =        3568934
84                 I    =           51
31634
 XDOT =       5611
931598                 Wp   =           89
64381
 YDOT =       2808
171586  meter/sec      RA   =          240
88358  deg
 ZDOT =       4416
667651                 TA   =          312
79450
                                          MA   =          312
91146
                                          Ha   =            220
526  n
mi
                                          Hp   =            212
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         208103
47                 X    =          110486
06
 Y    =      -18893840
41  feet           Y    =        -5757870
31  meter
 Z    =       11709103
80                 Z    =         3569356
97
 XDOT =      18411
849074                 XDOT =        5558
659000
 YDOT =       9213
161371  feet/sec       YDOT =        2870
629874  meter/sec
 ZDOT =      14490
379432                 ZDOT =        4443
799197

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16457496
07                 X    =        -5016244
80
 Y    =        9279256
68  feet           Y    =         2828317
44  meter
 Z    =       11711952
99                 Z    =         3569803
27
 XDOT =       -437
040117                 XDOT =        -133
209828
 YDOT =     -19274
554862  feet/sec       YDOT =       -5874
884322  meter/sec
 ZDOT =      14608
142807                 ZDOT =        4452
561928


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   16204
55674254  
00016717  00000-0  10270-3 0  9020
2 25544  51
6405 241
5669 0002015  68
2966 291
8401 15
54861853 10485


Satellite: ISS
Catalog Number: 25544
Epoch time:      16204
55674254   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:       241
5669  deg
Eccentricity:     
0002015     
Arg of perigee:    68
2966  deg
Mean anomaly:     291
8401  deg
Mean motion:   15
54861853  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1048
Checksum:              309


Coasting Arc #4 (Orbit 1062)
---------------------------------------

Vector Time (GMT): 2016/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1473731
78                 A    =         6777569
38  meter
 Y    =        4611398
46  meter          E    =           
0013064
 Z    =       -4755791
15                 I    =           51
31954
 XDOT =      -5604
008742                 Wp   =           71
67124
 YDOT =      -4506
698292  meter/sec      RA   =          235
86598  deg
 ZDOT =      -2635
233198                 TA   =          172
18695
                                          MA   =          172
16658
                                          Ha   =            220
501  n
mi
                                          Hp   =            212
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4835078
02                 X    =        -1502086
91
 Y    =       15129260
05  feet           Y    =         4594759
81  meter
 Z    =      -15602989
34                 Z    =        -4763018
77
 XDOT =     -18385
855454                 XDOT =       -5540
396613
 YDOT =     -14785
755552  feet/sec       YDOT =       -4569
010301  meter/sec
 ZDOT =      -8645
778208                 ZDOT =       -2662
301209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15418104
52                 X    =         4699438
26
 Y    =       -3680419
75  feet           Y    =        -1121791
94  meter
 Z    =      -15635291
14                 Z    =        -4765636
74
 XDOT =      -3582
657874                 XDOT =       -1091
994120
 YDOT =      22191
640777  feet/sec       YDOT =        6764
012109  meter/sec
 ZDOT =      -8762
985956                 ZDOT =       -2670
958119


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   16205
52081238  
00016717  00000-0  10270-3 0  9033
2 25544  51
6413 236
7559 0001889  72
1523 287
9836 15
54866774 10631


Satellite: ISS
Catalog Number: 25544
Epoch time:      16205
52081238   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:       236
7559  deg
Eccentricity:     
0001889     
Arg of perigee:    72
1523  deg
Mean anomaly:     287
9836  deg
Mean motion:   15
54866774  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1063
Checksum:              328


Coasting Arc #5 (Orbit 1078)
---------------------------------------

Vector Time (GMT): 2016/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2905509
09                 A    =         6775236
46  meter
 Y    =       -3109003
71  meter          E    =           
0004574
 Z    =        5268286
45                 I    =           51
32976
 XDOT =       5144
180252                 Wp   =           96
92396
 YDOT =       5671
261222  meter/sec      RA   =          230
83869  deg
 ZDOT =        508
827708                 TA   =          348
19875
                                          MA   =          348
20947
                                          Ha   =            220
420  n
mi
                                          Hp   =            212
760

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9532510
15                 X    =         2914468
13
 Y    =      -10200143
40  feet           Y    =        -3076462
38  meter
 Z    =       17284404
35                 Z    =         5282422
17
 XDOT =      16877
231799                 XDOT =        5077
908825
 YDOT =      18606
500072  feet/sec       YDOT =        5728
416325  meter/sec
 ZDOT =       1669
382243                 ZDOT =         533
655628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13631421
84                 X    =        -4154857
38
 Y    =       -2635078
45  feet           Y    =         -803171
91  meter
 Z    =       17346556
12                 Z    =         5287230
30
 XDOT =       6738
611959                 XDOT =        2053
928925
 YDOT =     -23143
869739  feet/sec       YDOT =       -7054
251496  meter/sec
 ZDOT =       1776
643262                 ZDOT =         541
520866


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   16206
54914947  
00016717  00000-0  10270-3 0  9049
2 25544  51
6402 231
6238 0002024  74
4266 285
7110 15
54885870 10794


Satellite: ISS
Catalog Number: 25544
Epoch time:      16206
54914947   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:       231
6238  deg
Eccentricity:     
0002024     
Arg of perigee:    74
4266  deg
Mean anomaly:     285
7110  deg
Mean motion:   15
54885870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1079
Checksum:              307


Coasting Arc #6 (Orbit 1093)
---------------------------------------

Vector Time (GMT): 2016/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4252702
43                 A    =         6776120
07  meter
 Y    =        1456867
05  meter          E    =           
0015096
 Z    =       -5083852
48                 I    =           51
35558
 XDOT =      -4149
095998                 Wp   =           99
40568
 YDOT =      -6210
237079  meter/sec      RA   =          225
81069  deg
 ZDOT =       1693
005860                 TA   =          187
02589
                                          MA   =          187
04708
                                          Ha   =            220
491  n
mi
                                          Hp   =            212
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13952435
81                 X    =        -4243982
53
 Y    =        4779747
54  feet           Y    =         1409359
34  meter
 Z    =      -16679306
03                 Z    =        -5104489
61
 XDOT =     -13612
519678                 XDOT =       -4087
566994
 YDOT =     -20374
793567  feet/sec       YDOT =       -6256
291042  meter/sec
 ZDOT =       5554
481169                 ZDOT =        1673
000144

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11511960
00                 X    =         3508845
41
 Y    =        9053930
40  feet           Y    =         2759637
98  meter
 Z    =      -16769520
64                 Z    =        -5111349
89
 XDOT =      -9082
542335                 XDOT =       -2768
358904
 YDOT =      21665
227476  feet/sec       YDOT =        6603
561335  meter/sec
 ZDOT =       5468
316789                 ZDOT =        1666
742957


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   16207
51321055  
00016717  00000-0  10270-3 0  9050
2 25544  51
6421 226
8129 0001871  73
2044 286
9314 15
54869253 10943


Satellite: ISS
Catalog Number: 25544
Epoch time:      16207
51321055   =   yrday
fracday
Element set:     905
Inclination:       51
6421  deg
RA of node:       226
8129  deg
Eccentricity:     
0001871     
Arg of perigee:    73
2044  deg
Mean anomaly:     286
9314  deg
Mean motion:   15
54869253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1094
Checksum:              297


Coasting Arc #7 (Orbit 1109)
---------------------------------------

Vector Time (GMT): 2016/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5330369
39                 A    =         6779493
31  meter
 Y    =         194093
14  meter          E    =           
0012183
 Z    =        4176538
08                 I    =           51
38881
 XDOT =       2667
332131                 Wp   =           74
96723
 YDOT =       6182
914832  meter/sec      RA   =          220
79141  deg
 ZDOT =      -3679
464377                 TA   =           52
94249
                                          MA   =           52
83114
                                          Ha   =            220
364  n
mi
                                          Hp   =            212
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17488088
56                 X    =         5307515
17
 Y    =         636788
51  feet           Y    =          253572
99  meter
 Z    =       13702552
76                 Z    =         4202375
98
 XDOT =       8751
089668                 XDOT =        2615
868089
 YDOT =      20285
153648  feet/sec       YDOT =        6212
455066  meter/sec
 ZDOT =     -12071
733520                 ZDOT =       -3666
632080

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9138508
37                 X    =        -2785417
35
 Y    =      -14819832
13  feet           Y    =        -4517084
83  meter
 Z    =       13815170
42                 Z    =         4210863
94
 XDOT =      10876
618716                 XDOT =        3315
193385
 YDOT =     -17945
829136  feet/sec       YDOT =       -5469
888721  meter/sec
 ZDOT =     -12016
825010                 ZDOT =       -3662
728263


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   16208
54153786  
00016717  00000-0  10270-3 0  9069
2 25544  51
6403 221
6810 0002044  75
7708 284
3672 15
54920230 11101


Satellite: ISS
Catalog Number: 25544
Epoch time:      16208
54153786   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       221
6810  deg
Eccentricity:     
0002044     
Arg of perigee:    75
7708  deg
Mean anomaly:     284
3672  deg
Mean motion:   15
54920230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1110
Checksum:              284


Coasting Arc #8 (Orbit 1124)
---------------------------------------

Vector Time (GMT): 2016/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5992519
40                 A    =         6783808
79  meter
 Y    =       -1641876
33  meter          E    =           
0006698
 Z    =       -2724123
67                 I    =           51
42824
 XDOT =       -790
823996                 Wp   =           65
50004
 YDOT =      -5627
068567  meter/sec      RA   =          215
78758  deg
 ZDOT =       5143
891320                 TA   =          263
59724
                                          MA   =          263
67352
                                          Ha   =            220
461  n
mi
                                          Hp   =            212
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19660496
73                 X    =        -5960481
62
 Y    =       -5386733
38  feet           Y    =        -1708709
44  meter
 Z    =       -8937413
61                 Z    =        -2753155
90
 XDOT =      -2594
566917                 XDOT =        -752
828569
 YDOT =     -18461
511045  feet/sec       YDOT =       -5635
699862  meter/sec
 ZDOT =      16876
283859                 ZDOT =        5140
141765

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6745085
61                 X    =         2055902
09
 Y    =       19177643
94  feet           Y    =         5845345
87  meter
 Z    =       -9063728
99                 Z    =        -2762624
60
 XDOT =     -12229
113950                 XDOT =       -3727
433932
 YDOT =      12250
524935  feet/sec       YDOT =        3733
960000  meter/sec
 ZDOT =      16860
875013                 ZDOT =        5139
194704


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   16209
50559217  
00016717  00000-0  10270-3 0  9076
2 25544  51
6404 216
8707 0002029  80
9058 279
2325 15
54912491 11256


Satellite: ISS
Catalog Number: 25544
Epoch time:      16209
50559217   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       216
8707  deg
Eccentricity:     
0002029     
Arg of perigee:    80
9058  deg
Mean anomaly:     279
2325  deg
Mean motion:   15
54912491  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1125
Checksum:              306


Coasting Arc #9 (Orbit 1140)
---------------------------------------

Vector Time (GMT): 2016/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6096810
02                 A    =         6786707
29  meter
 Y    =        2840436
32  meter          E    =           
0014998
 Z    =         855732
65                 I    =           51
46371
 XDOT =      -1343
619554                 Wp   =          120
20576
 YDOT =       4688
866999  meter/sec      RA   =          210
79622  deg
 ZDOT =      -5920
647828                 TA   =           50
50899
                                          MA   =           50
37645
                                          Ha   =            220
503  n
mi
                                          Hp   =            212
648

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20002657
53                 X    =         6060437
66
 Y    =        9319016
81  feet           Y    =         2908411
50  meter
 Z    =        2807521
82                 Z    =          885261
05
 XDOT =      -4408
200635                 XDOT =       -1367
192038
 YDOT =      15383
421912  feet/sec       YDOT =        4673
710300  meter/sec
 ZDOT =     -19424
697598                 ZDOT =       -5927
231723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4105265
17                 X    =        -1251284
82
 Y    =      -21664725
58  feet           Y    =        -6603408
36  meter
 Z    =        2935817
55                 Z    =          894837
19
 XDOT =      13407
451877                 XDOT =        4086
591332
 YDOT =      -5206
734425  feet/sec       YDOT =       -1587
012653  meter/sec
 ZDOT =     -19454
189157                 ZDOT =       -5929
636855


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   16210
53391131  
00016717  00000-0  10270-3 0  9081
2 25544  51
6395 211
7379 0002069  80
8710 279
2677 15
54914806 11412


Satellite: ISS
Catalog Number: 25544
Epoch time:      16210
53391131   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:       211
7379  deg
Eccentricity:     
0002069     
Arg of perigee:    80
8710  deg
Mean anomaly:     279
2677  deg
Mean motion:   15
54914806  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1141
Checksum:              307


Coasting Arc #10 (Orbit 1156)
---------------------------------------

Vector Time (GMT): 2016/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5593621
00                 A    =         6786443
08  meter
 Y    =       -3671548
11  meter          E    =           
0015278
 Z    =        1092874
06                 I    =           51
49041
 XDOT =       3465
255029                 Wp   =           60
79336
 YDOT =      -3514
924307  meter/sec      RA   =          205
81240  deg
 ZDOT =       5872
852103                 TA   =          311
09499
                                          MA   =          311
22683
                                          Ha   =            220
400  n
mi
                                          Hp   =            212
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18351774
92                 X    =        -5557457
75
 Y    =      -12045761
53  feet           Y    =        -3733897
59  meter
 Z    =        3585544
80                 Z    =         1065789
48
 XDOT =      11368
946944                 XDOT =        3475
774756
 YDOT =     -11531
903894  feet/sec       YDOT =       -3476
115114  meter/sec
 ZDOT =      19267
887477                 ZDOT =        5889
710577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1329748
91                 X    =          405307
47
 Y    =       21930542
83  feet           Y    =         6684429
45  meter
 Z    =        3468025
96                 Z    =         1057054
31
 XDOT =     -14365
822426                 XDOT =       -4378
702675
 YDOT =      -2216
977882  feet/sec       YDOT =        -675
734858  meter/sec
 ZDOT =      19341
997002                 ZDOT =        5895
440686


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   16211
56222321  
00016717  00000-0  10270-3 0  9090
2 25544  51
6386 206
6066 0001932  89
1438 270
9937 15
54960078 11571


Satellite: ISS
Catalog Number: 25544
Epoch time:      16211
56222321   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:       206
6066  deg
Eccentricity:     
0001932     
Arg of perigee:    89
1438  deg
Mean anomaly:     270
9937  deg
Mean motion:   15
54960078  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1157
Checksum:              315


Coasting Arc #11 (Orbit 1171)
---------------------------------------

Vector Time (GMT): 2016/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4456179
66                 A    =         6783462
85  meter
 Y    =        4191127
31  meter          E    =           
0006427
 Z    =       -2934149
51                 I    =           51
50847
 XDOT =      -5368
347806                 Wp   =          106
85524
 YDOT =       2213
704244  meter/sec      RA   =          200
82364  deg
 ZDOT =      -5001
935553                 TA   =          106
68548
                                          MA   =          106
61491
                                          Ha   =            220
522  n
mi
                                          Hp   =            212
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14620011
99                 X    =         4423234
85
 Y    =       13750417
69  feet           Y    =         4240775
30  meter
 Z    =       -9626474
76                 Z    =        -2912582
50
 XDOT =     -17612
689653                 XDOT =       -5368
406113
 YDOT =       7262
809199  feet/sec       YDOT =        2153
671845  meter/sec
 ZDOT =     -16410
549715                 ZDOT =       -5028
013257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1899768
54                 X    =          579049
45
 Y    =      -20024955
47  feet           Y    =        -6103606
43  meter
 Z    =       -9533089
28                 Z    =        -2905685
61
 XDOT =      14991
010579                 XDOT =        4569
260024
 YDOT =       9271
726714  feet/sec       YDOT =        2826
022303  meter/sec
 ZDOT =     -16524
667755                 ZDOT =       -5036
718732


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   16212
52626612  
00016717  00000-0  10270-3 0  9100
2 25544  51
6377 201
7944 0002013  86
2273 273
9110 15
54913715 11727


Satellite: ISS
Catalog Number: 25544
Epoch time:      16212
52626612   =   yrday
fracday
Element set:     910
Inclination:       51
6377  deg
RA of node:       201
7944  deg
Eccentricity:     
0002013     
Arg of perigee:    86
2273  deg
Mean anomaly:     273
9110  deg
Mean motion:   15
54913715  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1172
Checksum:              281


Coasting Arc #12 (Orbit 1187)
---------------------------------------

Vector Time (GMT): 2016/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2814196
13                 A    =         6779021
68  meter
 Y    =       -4378813
84  meter          E    =           
0011453
 Z    =        4335289
83                 I    =           51
52475
 XDOT =       6787
944672                 Wp   =          105
55510
 YDOT =       -930
558709  meter/sec      RA   =          195
82549  deg
 ZDOT =       3455
781342                 TA   =          309
27743
                                          MA   =          309
37896
                                          Ha   =            220
427  n
mi
                                          Hp   =            212
725

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9232926
92                 X    =        -2786080
56
 Y    =      -14366187
14  feet           Y    =        -4410127
16  meter
 Z    =       14223391
83                 Z    =         4321687
40
 XDOT =      22270
159685                 XDOT =        6781
059530
 YDOT =      -3053
014137  feet/sec       YDOT =        -854
690118  meter/sec
 ZDOT =      11337
865294                 ZDOT =        3488
738097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5384056
05                 X    =        -1641060
28
 Y    =       16257628
61  feet           Y    =         4955325
20  meter
 Z    =       14164766
14                 Z    =         4317420
72
 XDOT =     -15071
226139                 XDOT =       -4593
709727
 YDOT =     -15025
378297  feet/sec       YDOT =       -4579
735305  meter/sec
 ZDOT =      11481
799866                 ZDOT =        3499
652599


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   16213
55456991  
00016717  00000-0  10270-3 0  9116
2 25544  51
6381 196
6626 0001803  89
9570 270
1790 15
54949260 11881


Satellite: ISS
Catalog Number: 25544
Epoch time:      16213
55456991   =   yrday
fracday
Element set:     911
Inclination:       51
6381  deg
RA of node:       196
6626  deg
Eccentricity:     
0001803     
Arg of perigee:    89
9570  deg
Mean anomaly:     270
1790  deg
Mean motion:   15
54949260  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1188
Checksum:              331


Coasting Arc #13 (Orbit 1202)
---------------------------------------

Vector Time (GMT): 2016/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         794324
80                 A    =         6775735
75  meter
 Y    =        4328526
81  meter          E    =           
0015724
 Z    =       -5166003
24                 I    =           51
54506
 XDOT =      -7521
452450                 Wp   =           80
69973
 YDOT =       -298
581496  meter/sec      RA   =          190
81513  deg
 ZDOT =      -1407
856100                 TA   =          175
72924
                                          MA   =          175
71581
                                          Ha   =            220
465  n
mi
                                          Hp   =            212
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2606052
48                 X    =          770956
76
 Y    =       14201203
45  feet           Y    =         4337279
12  meter
 Z    =      -16948829
52                 Z    =        -5162201
20
 XDOT =     -24676
681266                 XDOT =       -7510
716018
 YDOT =       -979
598084  feet/sec       YDOT =        -382
631288  meter/sec
 ZDOT =      -4618
950460                 ZDOT =       -1444
366594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9195769
58                 X    =         2802870
57
 Y    =      -11155344
26  feet           Y    =        -3400148
93  meter
 Z    =      -16932945
03                 Z    =        -5161161
65
 XDOT =      14166
727377                 XDOT =        4318
018504
 YDOT =      18925
238912  feet/sec       YDOT =        5768
412820  meter/sec
 ZDOT =      -4778
211955                 ZDOT =       -1456
399004


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   16214
51860147  
00016717  00000-0  10270-3 0  9126
2 25544  51
6383 191
8503 0001976  89
5281 270
6099 15
54927452 12034


Satellite: ISS
Catalog Number: 25544
Epoch time:      16214
51860147   =   yrday
fracday
Element set:     912
Inclination:       51
6383  deg
RA of node:       191
8503  deg
Eccentricity:     
0001976     
Arg of perigee:    89
5281  deg
Mean anomaly:     270
6099  deg
Mean motion:   15
54927452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1203
Checksum:              314


Coasting Arc #14 (Orbit 1218)
---------------------------------------

Vector Time (GMT): 2016/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1351051
83                 A    =         6775200
81  meter
 Y    =       -4052766
53  meter          E    =           
0004882
 Z    =        5254746
49                 I    =           51
57509
 XDOT =       7495
083190                 Wp   =           73
28441
 YDOT =       1422
034871  meter/sec      RA   =          185
80183  deg
 ZDOT =       -828
298023                 TA   =           24
64671
                                          MA   =           24
62339
                                          Ha   =            220
370  n
mi
                                          Hp   =            212
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4432584
73                 X    =         1370745
77
 Y    =      -13296478
10  feet           Y    =        -4037548
26  meter
 Z    =       17239981
92                 Z    =         5261357
08
 XDOT =      24590
167945                 XDOT =        7482
648011
 YDOT =       4665
468738  feet/sec       YDOT =        1505
780402  meter/sec
 ZDOT =      -2717
513200                 ZDOT =        -791
919780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12900931
27                 X    =        -3932203
85
 Y    =        5384414
60  feet           Y    =         1641169
57  meter
 Z    =       17269486
56                 Z    =         5263739
50
 XDOT =     -12101
342327                 XDOT =       -3688
489141
 YDOT =     -20765
927510  feet/sec       YDOT =       -6329
454705  meter/sec
 ZDOT =      -2558
987536                 ZDOT =        -779
979401


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   16215
54689694  
00016717  00000-0  10270-3 0  9137
2 25544  51
6381 186
7183 0001864  92
8133 267
3234 15
54934398 12196


Satellite: ISS
Catalog Number: 25544
Epoch time:      16215
54689694   =   yrday
fracday
Element set:     913
Inclination:       51
6381  deg
RA of node:       186
7183  deg
Eccentricity:     
0001864     
Arg of perigee:    92
8133  deg
Mean anomaly:     267
3234  deg
Mean motion:   15
54934398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1219
Checksum:              337


Coasting Arc #15 (Orbit 1233)
---------------------------------------

Vector Time (GMT): 2016/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3381835
42                 A    =         6777808
56  meter
 Y    =        3624335
75  meter          E    =           
0012290
 Z    =       -4634306
96                 I    =           51
61706
 XDOT =      -6639
131224                 Wp   =          107
95545
 YDOT =      -2427
966678  meter/sec      RA   =          180
79415  deg
 ZDOT =       2948
741483                 TA   =          191
44472
                                          MA   =          191
47269
                                          Ha   =            220
396  n
mi
                                          Hp   =            212
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11095260
58                 X    =        -3399601
39
 Y    =       11890865
31  feet           Y    =         3586418
56  meter
 Z    =      -15204419
15                 Z    =        -4650777
75
 XDOT =     -21781
926589                 XDOT =       -6625
811032
 YDOT =      -7965
769940  feet/sec       YDOT =       -2502
135460  meter/sec
 ZDOT =       9674
348696                 ZDOT =        2916
523313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16192220
06                 X    =         4935388
67
 Y    =         316989
62  feet           Y    =           96618
44  meter
 Z    =      -15276890
19                 Z    =        -4656396
13
 XDOT =       8586
669327                 XDOT =        2617
216811
 YDOT =      20435
556694  feet/sec       YDOT =        6228
757680  meter/sec
 ZDOT =       9534
119535                 ZDOT =        2905
999634


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   16216
51091880  
00016717  00000-0  10270-3 0  9140
2 25544  51
6391 181
9069 0001841  94
9322 265
2042 15
54933418 12348


Satellite: ISS
Catalog Number: 25544
Epoch time:      16216
51091880   =   yrday
fracday
Element set:     914
Inclination:       51
6391  deg
RA of node:       181
9069  deg
Eccentricity:     
0001841     
Arg of perigee:    94
9322  deg
Mean anomaly:     265
2042  deg
Mean motion:   15
54933418  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1234
Checksum:              302


Coasting Arc #16 (Orbit 1243)
---------------------------------------

Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3088695
53                 A    =         6777192
48  meter
 Y    =       -3670671
56  meter          E    =           
0009405
 Z    =        4781720
55                 I    =           51
63832
 XDOT =       6828
009874                 Wp   =          117
54631
 YDOT =      -2328
965942  meter/sec      RA   =          177
83487  deg
 ZDOT =       2614
452267                 TA   =          306
65532
                                          MA   =          306
74174
                                          Ha   =            220
371  n
mi
                                          Hp   =            212
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10133515
52                 X    =        -3070646
60
 Y    =      -12042885
70  feet           Y    =        -3705110
54  meter
 Z    =       15688059
54                 Z    =         4766760
59
 XDOT =      22401
607197                 XDOT =        6840
845903
 YDOT =      -7640
964375  feet/sec       YDOT =       -2252
538822  meter/sec
 ZDOT =       8577
599301                 ZDOT =        2647
651420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7625354
82                 X    =        -2324208
15
 Y    =      -13841942
98  feet           Y    =        -4219024
22  meter
 Z    =       15623348
66                 Z    =         4761996
67
 XDOT =      22411
642934                 XDOT =        6831
068766
 YDOT =      -2470
331677  feet/sec       YDOT =        -752
957095  meter/sec
 ZDOT =       8722
883746                 ZDOT =        2658
734966


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   16217
15359589  
00016717  00000-0  10270-3 0  9155
2 25544  51
6428 178
6961 0001846 112
4868 247
6480 15
54987152 12444


Satellite: ISS
Catalog Number: 25544
Epoch time:      16217
15359589   =   yrday
fracday
Element set:     915
Inclination:       51
6428  deg
RA of node:       178
6961  deg
Eccentricity:     
0001846     
Arg of perigee:   112
4868  deg
Mean anomaly:     247
6480  deg
Mean motion:   15
54987152  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1244
Checksum:              343
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