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

 
Date: May 20th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 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


There are no maneuvers



Coasting Arc #1 (Orbit 67)
---------------------------------------

Vector Time (GMT): 2016/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6491853
94                 A    =         6787922
71  meter
 Y    =       -1947462
21  meter          E    =           
0013342
 Z    =         248335
37                 I    =           51
55900
 XDOT =       1589
178239                 Wp   =           53
67445
 YDOT =      -4504
711873  meter/sec      RA   =          195
03189  deg
 ZDOT =       6000
245657                 TA   =          309
00502
                                          MA   =          309
12375
                                          Ha   =            220
779  n
mi
                                          Hp   =            213
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21298733
40                 X    =        -6470800
77
 Y    =       -6389311
70  feet           Y    =        -2019940
74  meter
 Z    =         814748
59                 Z    =          216849
99
 XDOT =       5213
839368                 XDOT =        1610
285773
 YDOT =     -14779
238429  feet/sec       YDOT =       -4486
822919  meter/sec
 ZDOT =      19685
845331                 ZDOT =        6008
016669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16778109
24                 X    =        -5113967
70
 Y    =       14599941
54  feet           Y    =         4450062
18  meter
 Z    =         678174
75                 Z    =          206707
66
 XDOT =      -8712
972467                 XDOT =       -2655
714008
 YDOT =     -10968
610464  feet/sec       YDOT =       -3343
232469  meter/sec
 ZDOT =      19720
387288                 ZDOT =        6010
774046


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   16141
56388740  
00016717  00000-0  10270-3 0  9001
2 25544  51
6408 195
8427 0001546 107
3899 252
7423 15
54606860   685


Satellite: ISS
Catalog Number: 25544
Epoch time:      16141
56388740   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       195
8427  deg
Eccentricity:     
0001546     
Arg of perigee:   107
3899  deg
Mean anomaly:     252
7423  deg
Mean motion:   15
54606860  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              68
Checksum:              320


Coasting Arc #2 (Orbit 82)
---------------------------------------

Vector Time (GMT): 2016/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5839038
01                 A    =         6785929
33  meter
 Y    =        2734407
01  meter          E    =           
0008031
 Z    =       -2109830
79                 I    =           51
58475
 XDOT =      -3754
489734                 Wp   =          134
01328
 YDOT =       3776
212953  meter/sec      RA   =          190
05320  deg
 ZDOT =      -5515
126527                 TA   =           69
37272
                                          MA   =           69
28661
                                          Ha   =            220
761  n
mi
                                          Hp   =            213
280

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19156948
84                 X    =         5818276
05
 Y    =        8971151
60  feet           Y    =         2799587
07  meter
 Z    =       -6922017
03                 Z    =        -2081515
91
 XDOT =     -12317
879705                 XDOT =       -3769
646637
 YDOT =      12389
150109  feet/sec       YDOT =        3734
143386  meter/sec
 ZDOT =     -18094
247135                 ZDOT =       -5533
401797

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17638351
30                 X    =         5376169
48
 Y    =      -11749129
06  feet           Y    =        -3581134
54  meter
 Z    =       -6799345
50                 Z    =        -2072440
51
 XDOT =       3391
886443                 XDOT =        1033
846988
 YDOT =      15573
949275  feet/sec       YDOT =        4746
939739  meter/sec
 ZDOT =     -18174
351439                 ZDOT =       -5539
542319


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   16142
52808866  
00016717  00000-0  10270-3 0  9015
2 25544  51
6414 191
0322 0001665 111
3987 248
7344 15
54670054   839


Satellite: ISS
Catalog Number: 25544
Epoch time:      16142
52808866   =   yrday
fracday
Element set:     901
Inclination:       51
6414  deg
RA of node:       191
0322  deg
Eccentricity:     
0001665     
Arg of perigee:   111
3987  deg
Mean anomaly:     248
7344  deg
Mean motion:   15
54670054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              83
Checksum:              298


Coasting Arc #3 (Orbit 98)
---------------------------------------

Vector Time (GMT): 2016/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4623114
72                 A    =         6782137
86  meter
 Y    =       -3329458
30  meter          E    =           
0013521
 Z    =        3669380
69                 I    =           51
60273
 XDOT =       5590
236651                 Wp   =           96
92047
 YDOT =      -2959
359377  meter/sec      RA   =          185
06817  deg
 ZDOT =       4342
689099                 TA   =          306
78100
                                          MA   =          306
90502
                                          Ha   =            220
813  n
mi
                                          Hp   =            213
263

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15167699
22                 X    =        -4603364
86
 Y    =      -10923419
63  feet           Y    =        -3381046
93  meter
 Z    =       12038650
57                 Z    =         3646970
06
 XDOT =      18340
671426                 XDOT =        5601
818193
 YDOT =      -9709
184307  feet/sec       YDOT =       -2896
781241  meter/sec
 ZDOT =      14247
667648                 ZDOT =        4369
873421

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17122406
60                 X    =        -5218909
53
 Y    =        7650313
64  feet           Y    =         2331815
60  meter
 Z    =       11941741
79                 Z    =         3639842
90
 XDOT =       1384
830772                 XDOT =         422
096419
 YDOT =     -19404
921814  feet/sec       YDOT =       -5914
620169  meter/sec
 ZDOT =      14366
394409                 ZDOT =        4378
877016


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   16143
55656586  
00016717  00000-0  10270-3 0  9020
2 25544  51
6404 185
9016 0001702 112
7461 247
3872 15
54667896   992


Satellite: ISS
Catalog Number: 25544
Epoch time:      16143
55656586   =   yrday
fracday
Element set:     902
Inclination:       51
6404  deg
RA of node:       185
9016  deg
Eccentricity:     
0001702     
Arg of perigee:   112
7461  deg
Mean anomaly:     247
3872  deg
Mean motion:   15
54667896  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              99
Checksum:              326


Coasting Arc #4 (Orbit 113)
---------------------------------------

Vector Time (GMT): 2016/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2928614
68                 A    =         6778096
09  meter
 Y    =        3803031
17  meter          E    =           
0012435
 Z    =       -4797300
11                 I    =           51
62171
 XDOT =      -6908
441087                 Wp   =           77
52821
 YDOT =       2047
994590  meter/sec      RA   =          180
07226  deg
 ZDOT =      -2596
936833                 TA   =          166
86109
                                          MA   =          166
82867
                                          Ha   =            220
705  n
mi
                                          Hp   =            213
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9608315
87                 X    =         2909174
12
 Y    =       12477136
39  feet           Y    =         3835672
65  meter
 Z    =      -15739173
57                 Z    =        -4783120
27
 XDOT =     -22665
489131                 XDOT =       -6918
213839
 YDOT =       6719
142356  feet/sec       YDOT =        1970
685411  meter/sec
 ZDOT =      -8520
133967                 ZDOT =       -2630
520349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15632093
07                 X    =         4764661
97
 Y    =       -2356698
18  feet           Y    =         -718321
61  meter
 Z    =      -15678134
17                 Z    =        -4778695
29
 XDOT =      -5385
768616                 XDOT =       -1641
582274
 YDOT =      21863
779811  feet/sec       YDOT =        6664
080086  meter/sec
 ZDOT =      -8666
561283                 ZDOT =       -2641
567879


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   16144
52075938  
00016717  00000-0  10270-3 0  9035
2 25544  51
6408 181
0913 0001653 118
9223 241
2096 15
54667329  1148


Satellite: ISS
Catalog Number: 25544
Epoch time:      16144
52075938   =   yrday
fracday
Element set:     903
Inclination:       51
6408  deg
RA of node:       181
0913  deg
Eccentricity:     
0001653     
Arg of perigee:   118
9223  deg
Mean anomaly:     241
2096  deg
Mean motion:   15
54667329  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             114
Checksum:              297


Coasting Arc #5 (Orbit 129)
---------------------------------------

Vector Time (GMT): 2016/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -961334
39                 A    =         6775820
44  meter
 Y    =       -4118745
32  meter          E    =           
0004562
 Z    =        5290308
25                 I    =           51
64599
 XDOT =       7577
832195                 Wp   =          115
21125
 YDOT =      -1078
685338  meter/sec      RA   =          175
06872  deg
 ZDOT =        534
947116                 TA   =          329
67490
                                          MA   =          329
70129
                                          Ha   =            220
720  n
mi
                                          Hp   =            213
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3153984
22                 X    =         -940904
43
 Y    =      -13512943
95  feet           Y    =        -4129381
90  meter
 Z    =       17356654
35                 Z    =         5285687
48
 XDOT =      24861
654184                 XDOT =        7586
732550
 YDOT =      -3538
993890  feet/sec       YDOT =        -993
895266  meter/sec
 ZDOT =       1755
075839                 ZDOT =         571
780265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13442565
49                 X    =        -4097293
96
 Y    =       -3538082
39  feet           Y    =        -1078407
51  meter
 Z    =       17337246
81                 Z    =         5284392
83
 XDOT =       8421
023659                 XDOT =        2566
728011
 YDOT =     -22572
077527  feet/sec       YDOT =       -6879
969230  meter/sec
 ZDOT =       1915
500098                 ZDOT =         583
844430


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   16145
54922580  
00016717  00000-0  10270-3 0  9043
2 25544  51
6402 175
9601 0001690 116
4903 243
6423 15
54690907  1303


Satellite: ISS
Catalog Number: 25544
Epoch time:      16145
54922580   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:       175
9601  deg
Eccentricity:     
0001690     
Arg of perigee:   116
4903  deg
Mean anomaly:     243
6423  deg
Mean motion:   15
54690907  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             130
Checksum:              290


Coasting Arc #6 (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    =       -1085450
82                 A    =         6776572
29  meter
 Y    =        4307064
53  meter          E    =           
0015067
 Z    =       -5131409
15                 I    =           51
68170
 XDOT =      -7487
866103                 Wp   =          103
98634
 YDOT =         24
171223  meter/sec      RA   =          170
06506  deg
 ZDOT =       1604
602518                 TA   =          181
50125
                                          MA   =          181
50578
                                          Ha   =            220
636  n
mi
                                          Hp   =            213
280

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3561190
36                 X    =        -1108606
44
 Y    =       14130789
16  feet           Y    =         4294797
34  meter
 Z    =      -16835331
84                 Z    =        -5136737
85
 XDOT =     -24566
489838                 XDOT =       -7495
374406
 YDOT =         79
301914  feet/sec       YDOT =         -59
605219  meter/sec
 ZDOT =       5264
443958                 ZDOT =        1568
209803

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10963870
53                 X    =         3341787
74
 Y    =        9557669
58  feet           Y    =         2913177
69  meter
 Z    =      -16859245
90                 Z    =        -5138698
15
 XDOT =     -10533
253626                 XDOT =       -3210
535705
 YDOT =      21087
560153  feet/sec       YDOT =        6427
488334  meter/sec
 ZDOT =       5106
089525                 ZDOT =        1556
336087


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
51340802  
00016717  00000-0  10270-3 0  9053
2 25544  51
6415 171
1499 0001510 119
3543 240
7760 15
54673833  1450


Satellite: ISS
Catalog Number: 25544
Epoch time:      16146
51340802   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       171
1499  deg
Eccentricity:     
0001510     
Arg of perigee:   119
3543  deg
Mean anomaly:     240
7760  deg
Mean motion:   15
54673833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             145
Checksum:              287


Coasting Arc #7 (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    =        2992304
70                 A    =         6779699
65  meter
 Y    =       -4303324
64  meter          E    =           
0010911
 Z    =        4292285
23                 I    =           51
72235
 XDOT =       6709
797307                 Wp   =           78
94143
 YDOT =       1112
372323  meter/sec      RA   =          165
07012  deg
 ZDOT =      -3552
709199                 TA   =           47
24625
                                          MA   =           47
15449
                                          Ha   =            220
537  n
mi
                                          Hp   =            213
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9817272
65                 X    =         3019352
98
 Y    =      -14118519
16  feet           Y    =        -4269711
86  meter
 Z    =       14082300
63                 Z    =         4306886
47
 XDOT =      22013
770691                 XDOT =        6714
117414
 YDOT =       3649
515494  feet/sec       YDOT =        1187
430227  meter/sec
 ZDOT =     -11655
870074                 ZDOT =       -3520
103910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8330068
90                 X    =        -2539005
00
 Y    =      -14983561
28  feet           Y    =        -4566989
48  meter
 Z    =       14146570
61                 Z    =         4311874
72
 XDOT =      11984
710822                 XDOT =        3652
939859
 YDOT =     -17563
742097  feet/sec       YDOT =       -5353
428591  meter/sec
 ZDOT =     -11514
166634                 ZDOT =       -3509
517990


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
54186450  
00016717  00000-0  10270-3 0  9065
2 25544  51
6397 166
0190 0001620 119
6951 240
4364 15
54723278  1612


Satellite: ISS
Catalog Number: 25544
Epoch time:      16147
54186450   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:       166
0190  deg
Eccentricity:     
0001620     
Arg of perigee:   119
6951  deg
Mean anomaly:     240
4364  deg
Mean motion:   15
54723278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             161
Checksum:              301


Coasting Arc #8 (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    =       -4545477
17                 A    =         6783888
80  meter
 Y    =        4099780
37  meter          E    =           
0005606
 Z    =       -2928020
14                 I    =           51
76849
 XDOT =      -5305
134736                 Wp   =           81
59215
 YDOT =      -2294
628505  meter/sec      RA   =          160
08934  deg
 ZDOT =       5031
844854                 TA   =          245
08643
                                          MA   =          245
14470
                                          Ha   =            220
556  n
mi
                                          Hp   =            213
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14912982
85                 X    =        -4576761
00
 Y    =       13450723
01  feet           Y    =         4048775
14  meter
 Z    =       -9606365
28                 Z    =        -2950176
66
 XDOT =     -17405
297690                 XDOT =       -5303
523954
 YDOT =      -7528
308742  feet/sec       YDOT =       -2353
945458  meter/sec
 ZDOT =      16508
677344                 ZDOT =        5006
077469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5787410
67                 X    =         1764002
77
 Y    =       19182005
71  feet           Y    =         5846675
34  meter
 Z    =       -9703493
99                 Z    =        -2957624
97
 XDOT =     -12906
547180                 XDOT =       -3933
915580
 YDOT =      12173
815098  feet/sec       YDOT =        3710
578842  meter/sec
 ZDOT =      16396
916065                 ZDOT =        4997
780017


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
50603819  
00016717  00000-0  10270-3 0  9076
2 25544  51
6410 161
2090 0001608 123
6816 236
4490 15
54722874  1767


Satellite: ISS
Catalog Number: 25544
Epoch time:      16148
50603819   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       161
2090  deg
Eccentricity:     
0001608     
Arg of perigee:   123
6816  deg
Mean anomaly:     236
4490  deg
Mean motion:   15
54722874  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             176
Checksum:              297


Coasting Arc #9 (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    =        5625068
87                 A    =         6787010
35  meter
 Y    =       -3605601
10  meter          E    =           
0015298
 Z    =        1149857
77                 I    =           51
80777
 XDOT =       3457
352287                 Wp   =          122
46124
 YDOT =       3501
040278  meter/sec      RA   =          155
12175  deg
 ZDOT =      -5886
130055                 TA   =           45
07646
                                          MA   =           44
95244
                                          Ha   =            220
571  n
mi
                                          Hp   =            213
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18454950
37                 X    =         5659384
01
 Y    =      -11829399
93  feet           Y    =        -3542506
05  meter
 Z    =        3772499
23                 Z    =         1177266
14
 XDOT =      11343
019313                 XDOT =        3446
538199
 YDOT =      11486
352617  feet/sec       YDOT =        3539
642631  meter/sec
 ZDOT =     -19311
450311                 ZDOT =       -5869
361069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3162192
55                 X    =         -963836
29
 Y    =      -21670285
29  feet           Y    =        -6605102
96  meter
 Z    =        3892418
29                 Z    =         1186409
10
 XDOT =      13614
850729                 XDOT =        4149
806502
 YDOT =      -5470
393024  feet/sec       YDOT =       -1667
375794  meter/sec
 ZDOT =     -19239
049900                 ZDOT =       -5864
062409


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
53448439  
00016717  00000-0  10270-3 0  9086
2 25544  51
6401 156
0774 0001585 122
3638 237
7669 15
54722198  1929


Satellite: ISS
Catalog Number: 25544
Epoch time:      16149
53448439   =   yrday
fracday
Element set:     908
Inclination:       51
6401  deg
RA of node:       156
0774  deg
Eccentricity:     
0001585     
Arg of perigee:   122
3638  deg
Mean anomaly:     237
7669  deg
Mean motion:   15
54722198  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             192
Checksum:              329


Coasting Arc #10 (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    =       -6115410
15                 A    =         6787275
68  meter
 Y    =        2835661
51  meter          E    =           
0013540
 Z    =         741714
31                 I    =           51
83681
 XDOT =      -1402
226068                 Wp   =           59
48215
 YDOT =      -4605
267767  meter/sec      RA   =          150
16255  deg
 ZDOT =       5970
942349                 TA   =          308
51395
                                          MA   =          308
63528
                                          Ha   =            220
446  n
mi
                                          Hp   =            213
286

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20063681
60                 X    =        -6150267
67
 Y    =        9303351
40  feet           Y    =         2767079
98  meter
 Z    =        2433445
91                 Z    =          711922
53
 XDOT =      -4600
479226                 XDOT =       -1379
629004
 YDOT =     -15109
146217  feet/sec       YDOT =       -4620
822384  meter/sec
 ZDOT =      19589
705869                 ZDOT =        5964
185275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         561902
08                 X    =          171267
75
 Y    =       22122489
76  feet           Y    =         6742934
88  meter
 Z    =        2303266
96                 Z    =          702035
77
 XDOT =     -14128
604686                 XDOT =       -4306
398708
 YDOT =      -1704
515994  feet/sec       YDOT =        -519
536475  meter/sec
 ZDOT =      19561
073096                 ZDOT =        5962
215080


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
56292385  
00016717  00000-0  10270-3 0  9099
2 25544  51
6392 150
9471 0001560 134
7102 225
4178 15
54764111  2089


Satellite: ISS
Catalog Number: 25544
Epoch time:      16150
56292385   =   yrday
fracday
Element set:     909
Inclination:       51
6392  deg
RA of node:       150
9471  deg
Eccentricity:     
0001560     
Arg of perigee:   134
7102  deg
Mean anomaly:     225
4178  deg
Mean motion:   15
54764111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             208
Checksum:              292


Coasting Arc #11 (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    =        6032464
64                 A    =         6784859
22  meter
 Y    =       -1725350
61  meter          E    =           
0006720
 Z    =       -2579717
32                 I    =           51
85526
 XDOT =       -673
843454                 Wp   =          129
97601
 YDOT =       5517
328172  meter/sec      RA   =          145
20026  deg
 ZDOT =      -5279
088516                 TA   =           78
93956
                                          MA   =           78
86399
                                          Ha   =            220
560  n
mi
                                          Hp   =            213
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19791550
66                 X    =         6063840
85
 Y    =       -5660599
12  feet           Y    =        -1657716
01  meter
 Z    =       -8463639
49                 Z    =        -2550336
75
 XDOT =      -2210
772487                 XDOT =        -709
845777
 YDOT =      18101
470381  feet/sec       YDOT =        5509
591769  meter/sec
 ZDOT =     -17319
844214                 ZDOT =       -5282
449075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2335561
06                 X    =          711879
01
 Y    =      -20504801
46  feet           Y    =        -6249863
48  meter
 Z    =       -8335425
90                 Z    =        -2540637
81
 XDOT =      14435
899837                 XDOT =        4400
062270
 YDOT =       8673
329068  feet/sec       YDOT =        2643
630700  meter/sec
 ZDOT =     -17335
418884                 ZDOT =       -5283
835676


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
52708535  
00016717  00000-0  10270-3 0  9107
2 25544  51
6388 146
1358 0001499 130
0774 230
0511 15
54723128  2233


Satellite: ISS
Catalog Number: 25544
Epoch time:      16151
52708535   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:       146
1358  deg
Eccentricity:     
0001499     
Arg of perigee:   130
0774  deg
Mean anomaly:     230
0511  deg
Mean motion:   15
54723128  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             223
Checksum:              284


Coasting Arc #12 (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    =       -5418968
50                 A    =         6780645
71  meter
 Y    =         372459
04  meter          E    =           
0011916
 Z    =        4051193
67                 I    =           51
86738
 XDOT =       2518
851137                 Wp   =          105
65970
 YDOT =      -6097
101591  meter/sec      RA   =          140
23009  deg
 ZDOT =       3917
131615                 TA   =          303
81097
                                          MA   =          303
92437
                                          Ha   =            220
477  n
mi
                                          Hp   =            213
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17778768
06                 X    =        -5442409
86
 Y    =        1221978
48  feet           Y    =          311729
25  meter
 Z    =       13291317
82                 Z    =         4024812
46
 XDOT =       8263
947300                 XDOT =        2567
815293
 YDOT =     -20003
614145  feet/sec       YDOT =       -6068
660549  meter/sec
 ZDOT =      12851
481675                 ZDOT =        3929
486318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5389552
81                 X    =        -1642735
70
 Y    =       17075496
76  feet           Y    =         5204611
41  meter
 Z    =       13176383
62                 Z    =         4016161
73
 XDOT =     -14384
181637                 XDOT =       -4384
298563
 YDOT =     -14531
740147  feet/sec       YDOT =       -4429
274397  meter/sec
 ZDOT =      12906
326893                 ZDOT =        3933
848437


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
55551470  
00016717  00000-0  10270-3 0  9116
2 25544  51
6388 141
0049 0001328 138
1441 221
9813 15
54759555  2399


Satellite: ISS
Catalog Number: 25544
Epoch time:      16152
55551470   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:       141
0049  deg
Eccentricity:     
0001328     
Arg of perigee:   138
1441  deg
Mean anomaly:     221
9813  deg
Mean motion:   15
54759555  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             239
Checksum:              299


Coasting Arc #13 (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    =        4396950
43                 A    =         6776980
44  meter
 Y    =        1197023
45  meter          E    =           
0013438
 Z    =       -5028235
52                 I    =           51
87826
 XDOT =      -4003
527095                 Wp   =           80
12376
 YDOT =       6207
271066  meter/sec      RA   =          135
24761  deg
 ZDOT =      -2025
543528                 TA   =          170
24573
                                          MA   =          170
21961
                                          Ha   =            220
436  n
mi
                                          Hp   =            213
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14425690
40                 X    =         4407663
58
 Y    =        3927242
29  feet           Y    =         1246253
29  meter
 Z    =      -16496835
70                 Z    =        -5006849
83
 XDOT =     -13134
931414                 XDOT =       -4062
801442
 YDOT =      20365
062551  feet/sec       YDOT =        6162
169664  meter/sec
 ZDOT =      -6645
484016                 ZDOT =       -2045
135530

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8755265
38                 X    =         2668604
89
 Y    =      -12244434
91  feet           Y    =        -3732103
76  meter
 Z    =      -16403917
38                 Z    =        -4999914
02
 XDOT =      13614
382086                 XDOT =        4149
663660
 YDOT =      18743
141448  feet/sec       YDOT =        5712
909513  meter/sec
 ZDOT =      -6731
878959                 ZDOT =       -2051
876707


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
51966454  
00016717  00000-0  10270-3 0  9126
2 25544  51
6380 136
1936 0001354 133
9291 226
1974 15
54736483  2543


Satellite: ISS
Catalog Number: 25544
Epoch time:      16153
51966454   =   yrday
fracday
Element set:     912
Inclination:       51
6380  deg
RA of node:       136
1936  deg
Eccentricity:     
0001354     
Arg of perigee:   133
9291  deg
Mean anomaly:     226
1974  deg
Mean motion:   15
54736483  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             254
Checksum:              313


Coasting Arc #14 (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    =       -3104608
58                 A    =         6775561
81  meter
 Y    =       -2800515
96  meter          E    =           
0003315
 Z    =        5328899
59                 I    =           51
89568
 XDOT =       5027
456560                 Wp   =          104
69025
 YDOT =      -5794
658716  meter/sec      RA   =          130
25934  deg
 ZDOT =       -117
058786                 TA   =          346
41626
                                          MA   =          346
42518
                                          Ha   =            220
475  n
mi
                                          Hp   =            213
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10185723
69                 X    =        -3098947
69
 Y    =       -9188044
50  feet           Y    =        -2835202
54  meter
 Z    =       17483266
36                 Z    =         5313831
45
 XDOT =      16494
280053                 XDOT =        5092
448863
 YDOT =     -19011
347492  feet/sec       YDOT =       -5738
074946  meter/sec
 ZDOT =       -384
051136                 ZDOT =         -92
478866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12092820
06                 X    =        -3685891
56
 Y    =        6648754
24  feet           Y    =         2026540
29  meter
 Z    =       17418137
14                 Z    =         5309048
20
 XDOT =     -11943
521658                 XDOT =       -3640
385401
 YDOT =     -21006
528203  feet/sec       YDOT =       -6402
789796  meter/sec
 ZDOT =       -275
985629                 ZDOT =         -84
120420


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
54808574  
00016717  00000-0  10270-3 0  9139
2 25544  51
6379 131
0621 0001275 141
2451 218
8794 15
54741993  2706


Satellite: ISS
Catalog Number: 25544
Epoch time:      16154
54808574   =   yrday
fracday
Element set:     913
Inclination:       51
6379  deg
RA of node:       131
0621  deg
Eccentricity:     
0001275     
Arg of perigee:   141
2451  deg
Mean anomaly:     218
8794  deg
Mean motion:   15
54741993  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             270
Checksum:              309


Coasting Arc #15 (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    =        1707356
31                 A    =         6777188
99  meter
 Y    =        4310048
84  meter          E    =           
0013327
 Z    =       -4955915
99                 I    =           51
92231
 XDOT =      -5542
565604                 Wp   =          109
50317
 YDOT =       4782
660121  meter/sec      RA   =          125
27256  deg
 ZDOT =       2250
498894                 TA   =          182
41202
                                          MA   =          182
41845
                                          Ha   =            220
330  n
mi
                                          Hp   =            213
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5601562
70                 X    =         1683107
46
 Y    =       14140580
20  feet           Y    =         4329006
57  meter
 Z    =      -16259566
90                 Z    =        -4947680
40
 XDOT =     -18184
270355                 XDOT =       -5606
566701
 YDOT =      15691
142128  feet/sec       YDOT =        4720
321378  meter/sec
 ZDOT =       7383
526555                 ZDOT =        2223
419100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15218645
47                 X    =         4638643
14
 Y    =        -930903
74  feet           Y    =         -283739
46  meter
 Z    =      -16224465
38                 Z    =        -4945217
05
 XDOT =       9036
828273                 XDOT =        2754
425258
 YDOT =      21155
100100  feet/sec       YDOT =        6448
074511  meter/sec
 ZDOT =       7264
729029                 ZDOT =        2214
289408


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
51222407  
00016717  00000-0  10270-3 0  9143
2 25544  51
6390 126
2512 0001207 141
9778 218
1460 15
54744153  2858


Satellite: ISS
Catalog Number: 25544
Epoch time:      16155
51222407   =   yrday
fracday
Element set:     914
Inclination:       51
6390  deg
RA of node:       126
2512  deg
Eccentricity:     
0001207     
Arg of perigee:   141
9778  deg
Mean anomaly:     218
1460  deg
Mean motion:   15
54744153  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             285
Checksum:              285
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