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

 
Date: June 2nd 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) : 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


157/20:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 213 6

160/13:46:59 311 -0 2 1 5 1 5
N/A 1 5 -0 1 220 1
000/00:03:58 622 0 1 -0 0 214 5

161/01:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 4

166/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 214 5

Coasting Arc #1 (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    =        4430329
97                 A    =         6777127
40  meter
 Y    =        1145011
28  meter          E    =           
0013308
 Z    =       -5011092
62                 I    =           51
87830
 XDOT =      -3956
462652                 Wp   =           79
81715
 YDOT =       6219
741162  meter/sec      RA   =          135
24814  deg
 ZDOT =      -2079
142484                 TA   =          170
01050
                                          MA   =          169
98402
                                          Ha   =            220
472  n
mi
                                          Hp   =            213
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14535203
32                 X    =         4441538
98
 Y    =        3756598
69  feet           Y    =         1194617
17  meter
 Z    =      -16440592
57                 Z    =        -4989543
57
 XDOT =     -12980
520513                 XDOT =       -4015
619577
 YDOT =      20405
974940  feet/sec       YDOT =        6175
166726  meter/sec
 ZDOT =      -6821
333608                 ZDOT =       -2098
505569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8633513
10                 X    =         2631494
79
 Y    =      -12406321
13  feet           Y    =        -3781446
68  meter
 Z    =      -16346953
87                 Z    =        -4982551
54
 XDOT =      13695
237410                 XDOT =        4174
308363
 YDOT =      18620
568386  feet/sec       YDOT =        5675
549244  meter/sec
 ZDOT =      -6906
733874                 ZDOT =       -2105
172485


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
51976175  
00016717  00000-0  10270-3 0  9004
2 25544  51
6377 136
1938 0001344 134
0465 226
0799 15
54711194  2541


Satellite: ISS
Catalog Number: 25544
Epoch time:      16153
51976175   =   yrday
fracday
Element set:     900
Inclination:       51
6377  deg
RA of node:       136
1938  deg
Eccentricity:     
0001344     
Arg of perigee:   134
0465  deg
Mean anomaly:     226
0799  deg
Mean motion:   15
54711194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             254
Checksum:              309


Coasting Arc #2 (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    =       -3153684
90                 A    =         6775635
42  meter
 Y    =       -2743665
35  meter          E    =           
0003337
 Z    =        5329766
58                 I    =           51
89546
 XDOT =       4988
234907                 Wp   =          106
85330
 YDOT =      -5829
340264  meter/sec      RA   =          130
26024  deg
 ZDOT =        -50
157585                 TA   =          343
61733
                                          MA   =          343
62811
                                          Ha   =            220
514  n
mi
                                          Hp   =            213
445

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10346735
22                 X    =        -3148660
29
 Y    =       -9001526
75  feet           Y    =        -2778904
30  meter
 Z    =       17486110
82                 Z    =         5314458
49
 XDOT =      16365
600088                 XDOT =        5053
292960
 YDOT =     -19125
132099  feet/sec       YDOT =       -5773
194735  meter/sec
 ZDOT =       -164
559005                 ZDOT =         -25
768039

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11970614
82                 X    =        -3648643
40
 Y    =        6862727
02  feet           Y    =         2091759
20  meter
 Z    =       17419926
63                 Z    =         5309593
64
 XDOT =     -12078
528308                 XDOT =       -3681
535428
 YDOT =     -20930
688371  feet/sec       YDOT =       -6379
673815  meter/sec
 ZDOT =        -57
316485                 ZDOT =         -17
470065


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
54819986  
00016717  00000-0  10270-3 0  9015
2 25544  51
6376 131
0624 0001264 141
3075 218
8169 15
54715981  2701


Satellite: ISS
Catalog Number: 25544
Epoch time:      16154
54819986   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       131
0624  deg
Eccentricity:     
0001264     
Arg of perigee:   141
3075  deg
Mean anomaly:     218
8169  deg
Mean motion:   15
54715981  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             270
Checksum:              310


Coasting Arc #3 (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    =        1769592
90                 A    =         6777164
21  meter
 Y    =        4255967
19  meter          E    =           
0013472
 Z    =       -4980862
45                 I    =           51
92175
 XDOT =      -5517
660084                 Wp   =          109
04786
 YDOT =       4843
932552  meter/sec      RA   =          125
27354  deg
 ZDOT =       2179
185533                 TA   =          182
13943
                                          MA   =          182
14519
                                          Ha   =            220
368  n
mi
                                          Hp   =            213
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5805750
98                 X    =         1746065
36
 Y    =       13963146
94  feet           Y    =         4275624
92  meter
 Z    =      -16341412
25                 Z    =        -4972322
78
 XDOT =     -18102
559330                 XDOT =       -5582
001780
 YDOT =      15892
167164  feet/sec       YDOT =        4781
870422  meter/sec
 ZDOT =       7149
558835                 ZDOT =        2152
225904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15115232
05                 X    =         4607122
73
 Y    =       -1181298
78  feet           Y    =         -360059
87  meter
 Z    =      -16304976
68                 Z    =        -4969756
89
 XDOT =       9235
584329                 XDOT =        2815
006104
 YDOT =      21147
418897  feet/sec       YDOT =        6445
733280  meter/sec
 ZDOT =       7031
273768                 ZDOT =        2143
132244


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
51235446  
00016717  00000-0  10270-3 0  9027
2 25544  51
6386 126
2517 0001197 142
1441 217
9796 15
54717449  2853


Satellite: ISS
Catalog Number: 25544
Epoch time:      16155
51235446   =   yrday
fracday
Element set:     902
Inclination:       51
6386  deg
RA of node:       126
2517  deg
Eccentricity:     
0001197     
Arg of perigee:   142
1441  deg
Mean anomaly:     217
9796  deg
Mean motion:   15
54717449  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             285
Checksum:              314


Coasting Arc #4 (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    =        -389467
54                 A    =         6780858
50  meter
 Y    =       -5481761
73  meter          E    =           
0011500
 Z    =        3963194
65                 I    =           51
95223
 XDOT =       5608
653262                 Wp   =           84
71735
 YDOT =      -3328
746736  meter/sec      RA   =          120
29680  deg
 ZDOT =      -4041
964951                 TA   =           47
31526
                                          MA   =           47
21845
                                          Ha   =            220
306  n
mi
                                          Hp   =            213
457

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1277780
64                 X    =         -347391
91
 Y    =      -17984782
56  feet           Y    =        -5485882
25  meter
 Z    =       13002607
11                 Z    =         3961404
20
 XDOT =      18401
093379                 XDOT =        5665
093681
 YDOT =     -10921
085092  feet/sec       YDOT =       -3265
710962  meter/sec
 ZDOT =     -13261
039867                 ZDOT =       -4014
582470

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17561223
00                 X    =        -5352660
77
 Y    =       -4106775
02  feet           Y    =        -1251745
03  meter
 Z    =       12995797
97                 Z    =         3961119
22
 XDOT =      -5160
309924                 XDOT =       -1572
862465
 YDOT =     -19633
707691  feet/sec       YDOT =       -5984
354104  meter/sec
 ZDOT =     -13141
161897                 ZDOT =       -4005
426146


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
54078128  
00016717  00000-0  10270-3 0  9034
2 25544  51
6386 121
1202 0001080 144
3159 215
8067 15
54749716  3018


Satellite: ISS
Catalog Number: 25544
Epoch time:      16156
54078128   =   yrday
fracday
Element set:     903
Inclination:       51
6386  deg
RA of node:       121
1202  deg
Eccentricity:     
0001080     
Arg of perigee:   144
3159  deg
Mean anomaly:     215
8067  deg
Mean motion:   15
54749716  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             301
Checksum:              286


Coasting Arc #5 (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    =        -843466
12                 A    =         6784989
15  meter
 Y    =        6268335
77  meter          E    =           
0005329
 Z    =       -2455681
50                 I    =           51
98163
 XDOT =      -5296
214341                 Wp   =           60
06658
 YDOT =       1384
708031  meter/sec      RA   =          115
33420  deg
 ZDOT =       5364
976965                 TA   =          272
58371
                                          MA   =          272
64471
                                          Ha   =            220
276  n
mi
                                          Hp   =            213
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2767277
29                 X    =         -901568
78
 Y    =       20565406
07  feet           Y    =         6258579
04  meter
 Z    =       -8056697
82                 Z    =        -2459919
14
 XDOT =     -17376
031302                 XDOT =       -5337
365846
 YDOT =       4543
005351  feet/sec       YDOT =        1325
251400  meter/sec
 ZDOT =      17601
630464                 ZDOT =        5339
149283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18945662
23                 X    =         5774637
85
 Y    =        8446260
48  feet           Y    =         2574420
19  meter
 Z    =       -8076304
65                 Z    =        -2461657
66
 XDOT =          4
239560                 XDOT =           1
292218
 YDOT =      16678
039626  feet/sec       YDOT =        5083
466478  meter/sec
 ZDOT =      17488
859769                 ZDOT =        5330
604458


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
50492791  
00016717  00000-0  10270-3 0  9048
2 25544  51
6389 116
3099 0001089 148
6708 211
4510 15
54735906  3164


Satellite: ISS
Catalog Number: 25544
Epoch time:      16157
50492791   =   yrday
fracday
Element set:     904
Inclination:       51
6389  deg
RA of node:       116
3099  deg
Eccentricity:     
0001089     
Arg of perigee:   148
6708  deg
Mean anomaly:     211
4510  deg
Mean motion:   15
54735906  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             316
Checksum:              316


Coasting Arc #6 (Orbit 321)
---------------------------------------

Vector Time (GMT): 2016/157/20:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4288012
97                 A    =         6776116
78  meter
 Y    =        -408233
79  meter          E    =           
0004982
 Z    =        5228233
54                 I    =           51
95694
 XDOT =       2159
303229                 Wp   =          131
39988
 YDOT =      -7263
430655  meter/sec      RA   =          113
67396  deg
 ZDOT =       1199
889687                 TA   =          307
12291
                                          MA   =          307
16842
                                          Ha   =            220
394  n
mi
                                          Hp   =            213
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14068284
04                 X    =        -4308526
00
 Y    =       -1339349
71  feet           Y    =         -456300
64  meter
 Z    =       17152997
17                 Z    =         5207353
40
 XDOT =       7084
328178                 XDOT =        2234
535656
 YDOT =     -23830
153068  feet/sec       YDOT =       -7238
863410  meter/sec
 ZDOT =       3936
645954                 ZDOT =        1210
560821

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13982723
38                 X    =         4261934
09
 Y    =       -2702556
87  feet           Y    =         -823739
34  meter
 Z    =       17062104
75                 Z    =         5200529
53
 XDOT =       -271
343833                 XDOT =         -82
705600
 YDOT =      23833
523964  feet/sec       YDOT =        7264
458104  meter/sec
 ZDOT =       3984
468807                 ZDOT =        1214
466092


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
89058497  
00016717  00000-0  10270-3 0  9052
2 25544  51
6394 114
3846 0001074 158
9584 201
1613 15
54719035  3220


Satellite: ISS
Catalog Number: 25544
Epoch time:      16157
89058497   =   yrday
fracday
Element set:     905
Inclination:       51
6394  deg
RA of node:       114
3846  deg
Eccentricity:     
0001074     
Arg of perigee:   158
9584  deg
Mean anomaly:     201
1613  deg
Mean motion:   15
54719035  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             322
Checksum:              316


Coasting Arc #7 (Orbit 336)
---------------------------------------

Vector Time (GMT): 2016/158/20:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3553647
67                 A    =         6775802
05  meter
 Y    =        2368045
80  meter          E    =           
0014964
 Z    =       -5273789
38                 I    =           51
96819
 XDOT =      -3148
464813                 Wp   =          101
49525
 YDOT =       6911
957891  meter/sec      RA   =          108
68831  deg
 ZDOT =        981
534577                 TA   =          177
87235
                                          MA   =          177
86597
                                          Ha   =            220
173  n
mi
                                          Hp   =            213
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11658949
05                 X    =         3552521
33
 Y    =        7769179
13  feet           Y    =         2407779
51  meter
 Z    =      -17302458
61                 Z    =        -5256529
01
 XDOT =     -10329
608967                 XDOT =       -3230
289940
 YDOT =      22677
027201  feet/sec       YDOT =        6876
292010  meter/sec
 ZDOT =       3220
257799                 ZDOT =         966
042329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13548619
88                 X    =        -4129619
34
 Y    =       -3912525
75  feet           Y    =        -1192537
85  meter
 Z    =      -17227691
45                 Z    =        -5251000
35
 XDOT =       2846
627099                 XDOT =         867
651940
 YDOT =     -23742
114953  feet/sec       YDOT =       -7236
596638  meter/sec
 ZDOT =       3151
475241                 ZDOT =         960
569653


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
85472354  
00016717  00000-0  10270-3 0  9062
2 25544  51
6392 109
5726 0001155 160
2176 199
9022 15
54768173  3375


Satellite: ISS
Catalog Number: 25544
Epoch time:      16158
85472354   =   yrday
fracday
Element set:     906
Inclination:       51
6392  deg
RA of node:       109
5726  deg
Eccentricity:     
0001155     
Arg of perigee:   160
2176  deg
Mean anomaly:     199
9022  deg
Mean motion:   15
54768173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             337
Checksum:              321


Coasting Arc #8 (Orbit 352)
---------------------------------------

Vector Time (GMT): 2016/159/20:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2692108
35                 A    =         6778537
48  meter
 Y    =       -4170447
95  meter          E    =           
0008308
 Z    =        4610424
35                 I    =           51
98669
 XDOT =       3881
938868                 Wp   =           73
65355
 YDOT =      -5877
257722  meter/sec      RA   =          103
70917  deg
 ZDOT =      -3042
851260                 TA   =           46
60354
                                          MA   =           46
53439
                                          Ha   =            220
232  n
mi
                                          Hp   =            213
594

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8832376
49                 X    =        -2667668
69
 Y    =      -13682572
02  feet           Y    =        -4200416
87  meter
 Z    =       15126064
15                 Z    =         4597405
58
 XDOT =      12736
019909                 XDOT =        3962
152159
 YDOT =     -19282
341606  feet/sec       YDOT =       -5833
398390  meter/sec
 ZDOT =      -9983
107810                 ZDOT =       -3023
799760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12773894
02                 X    =         3893482
90
 Y    =       10185322
48  feet           Y    =         3104486
29  meter
 Z    =       15070113
00                 Z    =         4593370
44
 XDOT =      -5355
116618                 XDOT =       -1632
239545
 YDOT =      21395
707935  feet/sec       YDOT =        6521
411778  meter/sec
 ZDOT =      -9898
991278                 ZDOT =       -3017
212542


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
88313371  
00016717  00000-0  10270-3 0  9070
2 25544  51
6392 104
4415 0001147 168
6609 191
4570 15
54756293  3531


Satellite: ISS
Catalog Number: 25544
Epoch time:      16159
88313371   =   yrday
fracday
Element set:     907
Inclination:       51
6392  deg
RA of node:       104
4415  deg
Eccentricity:     
0001147     
Arg of perigee:   168
6609  deg
Mean anomaly:     191
4570  deg
Mean motion:   15
54756293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             353
Checksum:              315


Coasting Arc #9 (Orbit 363)
---------------------------------------

Vector Time (GMT): 2016/160/13:48:58
622
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3876004
18                 A    =         6776545
42  meter
 Y    =        1775359
86  meter          E    =           
0013734
 Z    =       -5279429
35                 I    =           51
98604
 XDOT =      -2055
065179                 Wp   =          101
44497
 YDOT =       7316
529250  meter/sec      RA   =          100
07513  deg
 ZDOT =        951
063237                 TA   =          177
62664
                                          MA   =          177
62012
                                          Ha   =            220
124  n
mi
                                          Hp   =            214
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12716549
14                 X    =         3881508
69
 Y    =        5824671
47  feet           Y    =         1818735
35  meter
 Z    =      -17320962
42                 Z    =        -5260587
16
 XDOT =      -6742
339825                 XDOT =       -2141
347545
 YDOT =      24004
361057  feet/sec       YDOT =        7293
065593  meter/sec
 ZDOT =       3120
286211                 ZDOT =         940
871608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2602481
09                 X    =          793236
24
 Y    =      -13845243
51  feet           Y    =        -4220030
22  meter
 Z    =      -17239184
53                 Z    =        -5254503
45
 XDOT =      23914
712295                 XDOT =        7289
204308
 YDOT =        664
768685  feet/sec       YDOT =         202
621495  meter/sec
 ZDOT =       3074
498167                 ZDOT =         937
107041


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
59016488  
00016717  00000-0  10270-3 0  9080
2 25544  51
6425 100
9168 0001227 223
5230 136
5826 15
54506964  3648


Satellite: ISS
Catalog Number: 25544
Epoch time:      16160
59016488   =   yrday
fracday
Element set:     908
Inclination:       51
6425  deg
RA of node:       100
9168  deg
Eccentricity:     
0001227     
Arg of perigee:   223
5230  deg
Mean anomaly:     136
5826  deg
Mean motion:   15
54506964  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             364
Checksum:              302


Coasting Arc #10 (Orbit 371)
---------------------------------------

Vector Time (GMT): 2016/161/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3732626
46                 A    =         6777041
84  meter
 Y    =       -2363336
97  meter          E    =           
0003442
 Z    =        5136851
45                 I    =           51
99141
 XDOT =       2258
157885                 Wp   =           62
97536
 YDOT =      -7144
554574  meter/sec      RA   =           97
66778  deg
 ZDOT =      -1643
803578                 TA   =           42
81915
                                          MA   =           42
79235
                                          Ha   =            220
192  n
mi
                                          Hp   =            214
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12246149
79                 X    =        -3730874
12
 Y    =       -7753730
20  feet           Y    =        -2405068
47  meter
 Z    =       16853187
17                 Z    =         5118723
34
 XDOT =       7408
654477                 XDOT =        2345
867110
 YDOT =     -23440
139678  feet/sec       YDOT =       -7118
811750  meter/sec
 ZDOT =      -5393
056358                 ZDOT =       -1632
621839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5898800
87                 X    =         1797954
50
 Y    =      -13339203
82  feet           Y    =        -4065789
32  meter
 Z    =       16774630
38                 Z    =         5112907
34
 XDOT =      23293
510709                 XDOT =        7099
862064
 YDOT =       3571
910055  feet/sec       YDOT =        1088
718185  meter/sec
 ZDOT =      -5342
979528                 ZDOT =       -1628
540160


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
10445497  
00016717  00000-0  10270-3 0  9095
2 25544  51
6432  98
3484 0001664 218
3806 141
7228 15
54534532  3728


Satellite: ISS
Catalog Number: 25544
Epoch time:      16161
10445497   =   yrday
fracday
Element set:     909
Inclination:       51
6432  deg
RA of node:        98
3484  deg
Eccentricity:     
0001664     
Arg of perigee:   218
3806  deg
Mean anomaly:     141
7228  deg
Mean motion:   15
54534532  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             372
Checksum:              307


Coasting Arc #11 (Orbit 386)
---------------------------------------

Vector Time (GMT): 2016/162/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3203589
81                 A    =         6780212
02  meter
 Y    =        4112263
71  meter          E    =           
0008151
 Z    =       -4344229
48                 I    =           52
00541
 XDOT =      -3040
031140                 Wp   =          121
27198
 YDOT =       6087
172585  meter/sec      RA   =           92
69532  deg
 ZDOT =       3521
061679                 TA   =          184
40013
                                          MA   =          184
40730
                                          Ha   =            220
027  n
mi
                                          Hp   =            214
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10510465
24                 X    =         3178469
64
 Y    =       13491678
82  feet           Y    =         4147948
34  meter
 Z    =      -14252721
38                 Z    =        -4328727
92
 XDOT =      -9973
855445                 XDOT =       -3124
977212
 YDOT =      19971
038666  feet/sec       YDOT =        6052
701632  meter/sec
 ZDOT =      11552
039629                 ZDOT =        3506
088297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11613557
20                 X    =        -3539812
24
 Y    =       12630109
57  feet           Y    =         3849657
40  meter
 Z    =      -14185942
52                 Z    =        -4323875
28
 XDOT =     -20405
053803                 XDOT =       -6219
460399
 YDOT =      -5865
020314  feet/sec       YDOT =       -1787
658192  meter/sec
 ZDOT =      11485
626271                 ZDOT =        3500
818887


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   16162
06874765  
00016717  00000-0  10270-3 0  9107
2 25544  51
6432  93
5399 0001631 220
7193 139
3838 15
54540641  3874


Satellite: ISS
Catalog Number: 25544
Epoch time:      16162
06874765   =   yrday
fracday
Element set:     910
Inclination:       51
6432  deg
RA of node:        93
5399  deg
Eccentricity:     
0001631     
Arg of perigee:   220
7193  deg
Mean anomaly:     139
3838  deg
Mean motion:   15
54540641  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             387
Checksum:              315


Coasting Arc #12 (Orbit 402)
---------------------------------------

Vector Time (GMT): 2016/163/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2568687
42                 A    =         6784372
96  meter
 Y    =       -5504077
18  meter          E    =           
0012280
 Z    =        3008686
27                 I    =           52
01930
 XDOT =       3725
149968                 Wp   =          102
57926
 YDOT =      -4476
435895  meter/sec      RA   =           87
73357  deg
 ZDOT =      -4994
296098                 TA   =           43
14805
                                          MA   =           43
05188
                                          Ha   =            220
086  n
mi
                                          Hp   =            214
444

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8427452
17                 X    =        -2521563
39
 Y    =      -18057996
01  feet           Y    =        -5532538
72  meter
 Z    =        9871017
95                 Z    =         2996322
28
 XDOT =      12221
620630                 XDOT =        3799
189793
 YDOT =     -14686
469472  feet/sec       YDOT =       -4434
364396  meter/sec
 ZDOT =     -16385
485886                 ZDOT =       -4976
020845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16263504
99                 X    =         4957116
32
 Y    =      -11560789
08  feet           Y    =        -3523728
51  meter
 Z    =        9818183
47                 Z    =         2992582
32
 XDOT =      15799
536821                 XDOT =        4815
698823
 YDOT =       8338
610372  feet/sec       YDOT =        2541
608441  meter/sec
 ZDOT =     -16304
978625                 ZDOT =       -4969
757485


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   16163
09732050  
00016717  00000-0  10270-3 0  9112
2 25544  51
6427  88
4099 0001513 225
2515 134
8515 15
54526543  4031


Satellite: ISS
Catalog Number: 25544
Epoch time:      16163
09732050   =   yrday
fracday
Element set:     911
Inclination:       51
6427  deg
RA of node:        88
4099  deg
Eccentricity:     
0001513     
Arg of perigee:   225
2515  deg
Mean anomaly:     134
8515  deg
Mean motion:   15
54526543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             403
Checksum:              287


Coasting Arc #13 (Orbit 417)
---------------------------------------

Vector Time (GMT): 2016/164/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1858071
02                 A    =         6787515
57  meter
 Y    =        6387029
62  meter          E    =           
0007386
 Z    =       -1333585
21                 I    =           52
02695
 XDOT =      -4293
185170                 Wp   =           33
80121
 YDOT =       2466
713854  meter/sec      RA   =           82
78246  deg
 ZDOT =       5853
826342                 TA   =          311
75897
                                          MA   =          311
82208
                                          Ha   =            219
995  n
mi
                                          Hp   =            214
572

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6096033
54                 X    =         1792989
54
 Y    =       20954821
57  feet           Y    =         6407444
01  meter
 Z    =       -4375279
55                 Z    =        -1324716
77
 XDOT =     -14085
253184                 XDOT =       -4348
884837
 YDOT =       8092
893222  feet/sec       YDOT =        2418
392727  meter/sec
 ZDOT =      19205
467002                 ZDOT =        5832
836041

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19364367
58                 X    =        -5902259
24
 Y    =       10080352
00  feet           Y    =         3072491
29  meter
 Z    =       -4337858
36                 Z    =        -1322179
23
 XDOT =      -9967
078452                 XDOT =       -3037
965512
 YDOT =     -10952
278496  feet/sec       YDOT =       -3338
254485  meter/sec
 ZDOT =      19113
505116                 ZDOT =        5825
796359


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   16164
06160181  
00016717  00000-0  10270-3 0  9121
2 25544  51
6424  83
6005 0001535 236
5298 123
5709 15
54495986  4181


Satellite: ISS
Catalog Number: 25544
Epoch time:      16164
06160181   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:        83
6005  deg
Eccentricity:     
0001535     
Arg of perigee:   236
5298  deg
Mean anomaly:     123
5709  deg
Mean motion:   15
54495986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             418
Checksum:              306


Coasting Arc #14 (Orbit 433)
---------------------------------------

Vector Time (GMT): 2016/165/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1014213
89                 A    =         6787998
61  meter
 Y    =       -6684696
57  meter          E    =           
0010868
 Z    =        -534170
17                 I    =           52
02404
 XDOT =       4750
900682                 Wp   =          146
68395
 YDOT =       -245
422659  meter/sec      RA   =           77
83697  deg
 ZDOT =      -6015
758604                 TA   =           39
05032
                                          MA   =           38
97191
                                          Ha   =            219
927  n
mi
                                          Hp   =            214
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3327473
40                 X    =         -936793
79
 Y    =      -21931419
18  feet           Y    =        -6695605
26  meter
 Z    =       -1752526
81                 Z    =         -538909
42
 XDOT =      15586
944495                 XDOT =        4782
513969
 YDOT =       -805
192451  feet/sec       YDOT =        -192
117722  meter/sec
 ZDOT =     -19736
740827                 ZDOT =       -5992
603113

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20736341
81                 X    =         6320436
98
 Y    =       -7873699
23  feet           Y    =        -2399903
53  meter
 Z    =       -1771881
95                 Z    =         -540069
62
 XDOT =       3533
765514                 XDOT =        1077
091729
 YDOT =      13676
747615  feet/sec       YDOT =        4168
672673  meter/sec
 ZDOT =     -19635
769152                 ZDOT =       -5984
982437


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   16165
09016257  
00016717  00000-0  10270-3 0  9130
2 25544  51
6423  78
4703 0001526 235
5357 124
5652 15
54543625  4342


Satellite: ISS
Catalog Number: 25544
Epoch time:      16165
09016257   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:        78
4703  deg
Eccentricity:     
0001526     
Arg of perigee:   235
5357  deg
Mean anomaly:     124
5652  deg
Mean motion:   15
54543625  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             434
Checksum:              296


Coasting Arc #15 (Orbit 449)
---------------------------------------

Vector Time (GMT): 2016/166/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          73632
23                 A    =         6785833
80  meter
 Y    =        6373715
88  meter          E    =           
0012445
 Z    =        2311113
10                 I    =           52
00951
 XDOT =      -5044
820648                 Wp   =           73
70473
 YDOT =      -1924
791514  meter/sec      RA   =           72
88810  deg
 ZDOT =       5448
204966                 TA   =          311
92191
                                          MA   =          312
02795
                                          Ha   =            219
906  n
mi
                                          Hp   =            214
460

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         241575
57                 X    =           -8872
17
 Y    =       20911141
34  feet           Y    =         6374077
80  meter
 Z    =        7582392
04                 Z    =         2311270
89
 XDOT =     -16551
248845                 XDOT =       -5049
387345
 YDOT =      -6314
932790  feet/sec       YDOT =       -1981
232017  meter/sec
 ZDOT =      17874
688208                 ZDOT =        5423
687144

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20317111
73                 X    =        -6192655
66
 Y    =        4955575
73  feet           Y    =         1510459
48  meter
 Z    =        7581826
95                 Z    =         2310940
85
 XDOT =       2708
411864                 XDOT =         825
523936
 YDOT =     -16185
058735  feet/sec       YDOT =       -4933
205902  meter/sec
 ZDOT =      17768
204902                 ZDOT =        5415
748854


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   16166
11871484  
00016717  00000-0  10270-3 0  9146
2 25544  51
6426  73
3397 0001415 242
1563 117
9447 15
54552733  4504


Satellite: ISS
Catalog Number: 25544
Epoch time:      16166
11871484   =   yrday
fracday
Element set:     914
Inclination:       51
6426  deg
RA of node:        73
3397  deg
Eccentricity:     
0001415     
Arg of perigee:   242
1563  deg
Mean anomaly:     117
9447  deg
Mean motion:   15
54552733  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             450
Checksum:              304


Coasting Arc #16 (Orbit 455)
---------------------------------------

Vector Time (GMT): 2016/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3695802
63                 A    =         6785938
16  meter
 Y    =        5225771
80  meter          E    =           
0005031
 Z    =       -2249110
49                 I    =           52
00621
 XDOT =      -2973
571878                 Wp   =           35
65196
 YDOT =       4458
016173  meter/sec      RA   =           70
66179  deg
 ZDOT =       5481
995882                 TA   =          299
47127
                                          MA   =          299
52145
                                          Ha   =            219
891  n
mi
                                          Hp   =            214
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12125336
70                 X    =         3648017
32
 Y    =       17144920
62  feet           Y    =         5266833
73  meter
 Z    =       -7378971
43                 Z    =        -2231272
75
 XDOT =      -9755
813247                 XDOT =       -3049
830841
 YDOT =      14626
037314  feet/sec       YDOT =        4424
336877  meter/sec
 ZDOT =      17985
550793                 ZDOT =        5467
366075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18609670
06                 X    =         5672227
43
 Y    =       -9786650
72  feet           Y    =        -2982971
14  meter
 Z    =       -7302257
23                 Z    =        -2225728
00
 XDOT =      12472
658879                 XDOT =        3801
666426
 YDOT =      10370
671287  feet/sec       YDOT =        3160
980608  meter/sec
 ZDOT =      17920
906099                 ZDOT =        5462
292179


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   16166
50442163  
00016717  00000-0  10270-3 0  9158
2 25544  51
6430  71
4177 0001252 254
0555 106
0460 15
54570875  4563


Satellite: ISS
Catalog Number: 25544
Epoch time:      16166
50442163   =   yrday
fracday
Element set:     915
Inclination:       51
6430  deg
RA of node:        71
4177  deg
Eccentricity:     
0001252     
Arg of perigee:   254
0555  deg
Mean anomaly:     106
0460  deg
Mean motion:   15
54570875  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             456
Checksum:              285


Coasting Arc #17 (Orbit 471)
---------------------------------------

Vector Time (GMT): 2016/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3086249
03                 A    =         6788046
74  meter
 Y    =       -6023435
26  meter          E    =           
0012142
 Z    =         429680
97                 I    =           52
00184
 XDOT =       4033
839429                 Wp   =          135
80192
 YDOT =      -2503
254941  meter/sec      RA   =           65
71351  deg
 ZDOT =      -6024
357606                 TA   =           39
58642
                                          MA   =           39
49782
                                          Ha   =            219
877  n
mi
                                          Hp   =            214
509

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10125488
96                 X    =        -3020751
31
 Y    =      -19761926
71  feet           Y    =        -6057581
57  meter
 Z    =        1409714
46                 Z    =          414847
17
 XDOT =      13234
381329                 XDOT =        4090
795586
 YDOT =      -8212
778678  feet/sec       YDOT =       -2457
826849  meter/sec
 ZDOT =     -19764
952777                 ZDOT =       -6004
623974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20802476
62                 X    =        -6340594
87
 Y    =        7777603
08  feet           Y    =         2370613
42  meter
 Z    =        1346263
53                 Z    =          410341
12
 XDOT =      -6044
833712                 XDOT =       -1842
465316
 YDOT =     -12706
013785  feet/sec       YDOT =       -3872
793002  meter/sec
 ZDOT =     -19678
444019                 ZDOT =       -5997
989737


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   16167
53296558  
00016717  00000-0  10270-3 0  9168
2 25544  51
6434  66
2881 0001371 253
1912 106
9090 15
54545678  4729


Satellite: ISS
Catalog Number: 25544
Epoch time:      16167
53296558   =   yrday
fracday
Element set:     916
Inclination:       51
6434  deg
RA of node:        66
2881  deg
Eccentricity:     
0001371     
Arg of perigee:   253
1912  deg
Mean anomaly:     106
9090  deg
Mean motion:   15
54545678  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             472
Checksum:              321
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