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

 
Date: February 17th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


050/12:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 213 7

Coasting Arc #1 (Orbit 2622)
---------------------------------------

Vector Time (GMT): 2016/048/14:39:04
880
Vector Time (MET): N/A
Weight (LBS)     : 922145
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3526232
18                 A    =         6777338
27  meter
 Y    =        2365141
04  meter          E    =           
0005466
 Z    =        5277936
52                 I    =           51
30099
 XDOT =      -3910
629440                 Wp   =          112
19669
 YDOT =       6592
700940  meter/sec      RA   =          298
61901  deg
 ZDOT =       -343
332652                 TA   =          341
07995
                                          MA   =          341
10025
                                          Ha   =            221
973  n
mi
                                          Hp   =            213
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11569003
23                 X    =         3473885
01
 Y    =        7759649
08  feet           Y    =         2404281
24  meter
 Z    =       17316064
70                 Z    =         5294938
54
 XDOT =     -12830
149080                 XDOT =       -3982
392274
 YDOT =      21629
596260  feet/sec       YDOT =        6548
568424  meter/sec
 ZDOT =      -1126
419462                 ZDOT =        -362
503766

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12199350
67                 X    =         3718362
08
 Y    =        6533620
11  feet           Y    =         1991447
41  meter
 Z    =       17389299
52                 Z    =         5300258
49
 XDOT =     -10038
548495                 XDOT =       -3059
749581
 YDOT =      21950
944507  feet/sec       YDOT =        6690
647886  meter/sec
 ZDOT =      -1210
771647                 ZDOT =        -369
043198


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   16048
65809445  
00016717  00000-0  10270-3 0  9007
2 25544  51
6417 299
0882 0003811 137
9621 222
1824 15
54145293 26239


Satellite: ISS
Catalog Number: 25544
Epoch time:      16048
65809445   =   yrday
fracday
Element set:     900
Inclination:       51
6417  deg
RA of node:       299
0882  deg
Eccentricity:     
0003811     
Arg of perigee:   137
9621  deg
Mean anomaly:     222
1824  deg
Mean motion:   15
54145293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2623
Checksum:              310


Coasting Arc #2 (Orbit 2637)
---------------------------------------

Vector Time (GMT): 2016/049/14:39:04
880
Vector Time (MET): N/A
Weight (LBS)     : 922145
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2587581
87                 A    =         6778916
50  meter
 Y    =       -3909049
25  meter          E    =           
0015443
 Z    =       -4911148
24                 I    =           51
29062
 XDOT =       4486
326730                 Wp   =          114
48375
 YDOT =      -5785
482039  meter/sec      RA   =          293
59426  deg
 ZDOT =       2240
525596                 TA   =          177
54557
                                          MA   =          177
53798
                                          Ha   =            221
995  n
mi
                                          Hp   =            213
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8489441
85                 X    =        -2519821
85
 Y    =      -12824964
73  feet           Y    =        -3937606
67  meter
 Z    =      -16112691
08                 Z    =        -4923553
04
 XDOT =      14718
919717                 XDOT =        4539
804706
 YDOT =     -18981
240286  feet/sec       YDOT =       -5735
013836  meter/sec
 ZDOT =       7350
805760                 ZDOT =        2262
448767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9871441
41                 X    =        -3008815
34
 Y    =      -11721496
72  feet           Y    =        -3572712
20  meter
 Z    =      -16165714
22                 Z    =        -4927309
70
 XDOT =      11420
519474                 XDOT =        3480
974336
 YDOT =     -19891
559733  feet/sec       YDOT =       -6062
947407  meter/sec
 ZDOT =       7446
921298                 ZDOT =        2269
821612


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   16049
62260279  
00016717  00000-0  10270-3 0  9012
2 25544  51
6403 294
2780 0003791 141
8309 218
3112 15
54179999 26385


Satellite: ISS
Catalog Number: 25544
Epoch time:      16049
62260279   =   yrday
fracday
Element set:     901
Inclination:       51
6403  deg
RA of node:       294
2780  deg
Eccentricity:     
0003791     
Arg of perigee:   141
8309  deg
Mean anomaly:     218
3112  deg
Mean motion:   15
54179999  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2638
Checksum:              321


Coasting Arc #3 (Orbit 2651)
---------------------------------------

Vector Time (GMT): 2016/050/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -131238
07                 A    =         6786074
27  meter
 Y    =       -6229759
29  meter          E    =           
0006179
 Z    =       -2693319
62                 I    =           51
30621
 XDOT =       5169
996315                 Wp   =           91
63201
 YDOT =      -2331
551979  meter/sec      RA   =          289
04877  deg
 ZDOT =       5151
156895                 TA   =          237
81465
                                          MA   =          237
87459
                                          Ha   =            221
902  n
mi
                                          Hp   =            213
702

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -430571
11                 X    =          -48482
92
 Y    =      -20438842
80  feet           Y    =        -6230764
32  meter
 Z    =       -8836350
46                 Z    =        -2693755
76
 XDOT =      16961
930167                 XDOT =        5170
662538
 YDOT =      -7649
448749  feet/sec       YDOT =       -2273
733620  meter/sec
 ZDOT =      16900
121046                 ZDOT =        5176
272619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8526933
76                 X    =         2599009
41
 Y    =      -18579836
64  feet           Y    =        -5663134
21  meter
 Z    =       -8837072
31                 Z    =        -2693539
64
 XDOT =      17147
598262                 XDOT =        5226
587950
 YDOT =       -204
747483  feet/sec       YDOT =         -62
407033  meter/sec
 ZDOT =      17009
415895                 ZDOT =        5184
469965


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   16050
52280056  
00016717  00000-0  10270-3 0  9029
2 25544  51
6428 289
7919 0003639 144
2490 215
8907 15
54189097 26524


Satellite: ISS
Catalog Number: 25544
Epoch time:      16050
52280056   =   yrday
fracday
Element set:     902
Inclination:       51
6428  deg
RA of node:       289
7919  deg
Eccentricity:     
0003639     
Arg of perigee:   144
2490  deg
Mean anomaly:     215
8907  deg
Mean motion:   15
54189097  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2652
Checksum:              327


Coasting Arc #4 (Orbit 2667)
---------------------------------------

Vector Time (GMT): 2016/051/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -794956
13                 A    =         6788700
30  meter
 Y    =        6650134
61  meter          E    =           
0017144
 Z    =        1052942
39                 I    =           51
30505
 XDOT =      -4931
863282                 Wp   =          128
76998
 YDOT =        348
014292  meter/sec      RA   =          284
05125  deg
 ZDOT =      -5867
371194                 TA   =           39
75224
                                          MA   =           39
62674
                                          Ha   =            221
888  n
mi
                                          Hp   =            213
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2608123
79                 X    =         -874375
12
 Y    =       21818026
94  feet           Y    =         6640800
91  meter
 Z    =        3454535
39                 Z    =         1048887
39
 XDOT =     -16180
653811                 XDOT =       -4906
887853
 YDOT =       1141
779174  feet/sec       YDOT =         293
002129  meter/sec
 ZDOT =     -19249
905493                 ZDOT =       -5891
267729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11511401
44                 X    =        -3508675
16
 Y    =       18720198
40  feet           Y    =         5705916
47  meter
 Z    =        3435728
88                 Z    =         1047210
16
 XDOT =     -13697
494984                 XDOT =       -4174
996471
 YDOT =      -4838
132079  feet/sec       YDOT =       -1474
662658  meter/sec
 ZDOT =     -19353
545112                 ZDOT =       -5898
960550


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   16051
55158514  
00016717  00000-0  10270-3 0  9037
2 25544  51
6424 284
6628 0003815 148
0963 212
0422 15
54186599 26686


Satellite: ISS
Catalog Number: 25544
Epoch time:      16051
55158514   =   yrday
fracday
Element set:     903
Inclination:       51
6424  deg
RA of node:       284
6628  deg
Eccentricity:     
0003815     
Arg of perigee:   148
0963  deg
Mean anomaly:     212
0422  deg
Mean motion:   15
54186599  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2668
Checksum:              317


Coasting Arc #5 (Orbit 2683)
---------------------------------------

Vector Time (GMT): 2016/052/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1587185
83                 A    =         6788766
75  meter
 Y    =       -6562366
14  meter          E    =           
0013003
 Z    =         667134
02                 I    =           51
29806
 XDOT =       4542
610038                 Wp   =           68
09008
 YDOT =       1711
053547  meter/sec      RA   =          279
05578  deg
 ZDOT =       5935
174466                 TA   =          299
14851
                                          MA   =          299
27858
                                          Ha   =            221
675  n
mi
                                          Hp   =            213
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5207302
60                 X    =         1657209
30
 Y    =      -21530072
63  feet           Y    =        -6544225
59  meter
 Z    =        2188759
92                 Z    =          675014
67
 XDOT =      14903
576240                 XDOT =        4494
309182
 YDOT =       5613
692740  feet/sec       YDOT =        1761
582518  meter/sec
 ZDOT =      19472
357171                 ZDOT =        5957
123311

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13417821
78                 X    =         4089752
08
 Y    =      -17620047
32  feet           Y    =        -5370590
42  meter
 Z    =        2224115
29                 Z    =          677910
34
 XDOT =       9984
314678                 XDOT =        3043
219114
 YDOT =      10109
103632  feet/sec       YDOT =        3081
254787  meter/sec
 ZDOT =      19567
179600                 ZDOT =        5964
076342


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   16052
58035246  
00016717  00000-0  10270-3 0  9048
2 25544  51
6414 279
5323 0003630 153
5109 206
6230 15
54255298 26845


Satellite: ISS
Catalog Number: 25544
Epoch time:      16052
58035246   =   yrday
fracday
Element set:     904
Inclination:       51
6414  deg
RA of node:       279
5323  deg
Eccentricity:     
0003630     
Arg of perigee:   153
5109  deg
Mean anomaly:     206
6230  deg
Mean motion:   15
54255298  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2684
Checksum:              297


Coasting Arc #6 (Orbit 2698)
---------------------------------------

Vector Time (GMT): 2016/053/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2318341
92                 A    =         6786617
00  meter
 Y    =        5921656
32  meter          E    =           
0009020
 Z    =       -2362213
01                 I    =           51
28557
 XDOT =      -4040
412236                 Wp   =          143
21297
 YDOT =      -3711
190534  meter/sec      RA   =          274
05809  deg
 ZDOT =      -5355
668508                 TA   =           63
29151
                                          MA   =           63
19920
                                          Ha   =            221
580  n
mi
                                          Hp   =            213
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7606108
67                 X    =        -2372912
70
 Y    =       19428006
30  feet           Y    =         5895425
69  meter
 Z    =       -7750042
68                 Z    =        -2373607
88
 XDOT =     -13255
945657                 XDOT =       -3972
597564
 YDOT =     -12175
821963  feet/sec       YDOT =       -3755
994532  meter/sec
 ZDOT =     -17571
090907                 ZDOT =       -5375
130237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14479204
61                 X    =        -4413261
57
 Y    =       14995610
68  feet           Y    =         4570662
13  meter
 Z    =       -7800498
30                 Z    =        -2377591
88
 XDOT =      -6319
680402                 XDOT =       -1926
238586
 YDOT =     -15255
737162  feet/sec       YDOT =       -4649
948687  meter/sec
 ZDOT =     -17654
778697                 ZDOT =       -5381
176547


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   16053
54481196  
00016717  00000-0  10270-3 0  9055
2 25544  51
6403 274
7232 0003583 158
3174 201
8131 15
54235552 26995


Satellite: ISS
Catalog Number: 25544
Epoch time:      16053
54481196   =   yrday
fracday
Element set:     905
Inclination:       51
6403  deg
RA of node:       274
7232  deg
Eccentricity:     
0003583     
Arg of perigee:   158
3174  deg
Mean anomaly:     201
8131  deg
Mean motion:   15
54235552  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2699
Checksum:              304


Coasting Arc #7 (Orbit 2714)
---------------------------------------

Vector Time (GMT): 2016/054/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2939620
22                 A    =         6782864
64  meter
 Y    =       -4810672
89  meter          E    =           
0013370
 Z    =        3764430
63                 I    =           51
27126
 XDOT =       3456
482490                 Wp   =          110
24962
 YDOT =       5409
833405  meter/sec      RA   =          269
04997  deg
 ZDOT =       4197
524534                 TA   =          295
13407
                                          MA   =          295
27271
                                          Ha   =            221
444  n
mi
                                          Hp   =            213
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9644423
29                 X    =         2974910
27
 Y    =      -15783047
55  feet           Y    =        -4777602
31  meter
 Z    =       12350494
19                 Z    =         3778796
60
 XDOT =      11340
165648                 XDOT =        3375
342154
 YDOT =      17748
797262  feet/sec       YDOT =        5448
032938  meter/sec
 ZDOT =      13771
405950                 ZDOT =        4214
117147

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14733488
65                 X    =         4490767
34
 Y    =      -11112183
99  feet           Y    =        -3386993
68  meter
 Z    =       12413616
57                 Z    =         3783670
33
 XDOT =       3060
109497                 XDOT =         932
721375
 YDOT =      19581
839097  feet/sec       YDOT =        5968
544557  meter/sec
 ZDOT =      13842
366170                 ZDOT =        4219
153209


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   16054
57355426  
00016717  00000-0  10270-3 0  9066
2 25544  51
6396 269
5921 0003433 161
4041 198
7238 15
54263606 27157


Satellite: ISS
Catalog Number: 25544
Epoch time:      16054
57355426   =   yrday
fracday
Element set:     906
Inclination:       51
6396  deg
RA of node:       269
5921  deg
Eccentricity:     
0003433     
Arg of perigee:   161
4041  deg
Mean anomaly:     198
7238  deg
Mean motion:   15
54263606  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2715
Checksum:              317


Coasting Arc #8 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2016/055/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3519495
45                 A    =         6779056
99  meter
 Y    =        3278023
40  meter          E    =           
0011791
 Z    =       -4787699
85                 I    =           51
25897
 XDOT =      -2755
688302                 Wp   =           89
13738
 YDOT =      -6676
303778  meter/sec      RA   =          264
03088  deg
 ZDOT =      -2550
656552                 TA   =          155
61812
                                          MA   =          155
56230
                                          Ha   =            221
370  n
mi
                                          Hp   =            213
864

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11546901
08                 X    =        -3532633
36
 Y    =       10754669
94  feet           Y    =         3238591
95  meter
 Z    =      -15707676
68                 Z    =        -4804828
74
 XDOT =      -9040
972121                 XDOT =       -2668
437635
 YDOT =     -21903
883785  feet/sec       YDOT =       -6706
632214  meter/sec
 ZDOT =      -8368
295773                 ZDOT =       -2563
829934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14515384
70                 X    =        -4424289
26
 Y    =        5995113
09  feet           Y    =         1827310
47  meter
 Z    =      -15782496
10                 Z    =        -4810504
81
 XDOT =       -197
334278                 XDOT =         -60
147488
 YDOT =     -22609
590356  feet/sec       YDOT =       -6891
403140  meter/sec
 ZDOT =      -8424
226555                 ZDOT =       -2567
704254


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   16055
53798656  
00016717  00000-0  10270-3 0  9070
2 25544  51
6383 264
7819 0003507 165
1166 195
0091 15
54292368 27308


Satellite: ISS
Catalog Number: 25544
Epoch time:      16055
53798656   =   yrday
fracday
Element set:     907
Inclination:       51
6383  deg
RA of node:       264
7819  deg
Eccentricity:     
0003507     
Arg of perigee:   165
1166  deg
Mean anomaly:     195
0091  deg
Mean motion:   15
54292368  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2730
Checksum:              332


Coasting Arc #9 (Orbit 2745)
---------------------------------------

Vector Time (GMT): 2016/056/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4000937
82                 A    =         6777041
29  meter
 Y    =       -1512376
06  meter          E    =           
0005816
 Z    =        5254227
84                 I    =           51
25668
 XDOT =       1954
529577                 Wp   =          144
05934
 YDOT =       7391
080517  meter/sec      RA   =          259
00373  deg
 ZDOT =        634
141589                 TA   =          299
82789
                                          MA   =          299
88570
                                          Ha   =            221
248  n
mi
                                          Hp   =            214
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13126436
40                 X    =         3992029
80
 Y    =       -4961863
71  feet           Y    =        -1467684
00  meter
 Z    =       17238280
32                 Z    =         5273641
70
 XDOT =       6412
498612                 XDOT =        1868
655075
 YDOT =      24248
951826  feet/sec       YDOT =        7412
457299  meter/sec
 ZDOT =       2080
517023                 ZDOT =         643
426471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13926148
21                 X    =         4244689
97
 Y    =        -261616
31  feet           Y    =          -79740
65  meter
 Z    =       17322692
79                 Z    =         5279956
76
 XDOT =      -2206
418196                 XDOT =        -672
516266
 YDOT =      23968
157568  feet/sec       YDOT =        7305
494427  meter/sec
 ZDOT =       2119
483668                 ZDOT =         646
018622


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   16056
56670213  
00016717  00000-0  10270-3 0  9083
2 25544  51
6385 259
6512 0003503 167
9909 192
1328 15
54280983 27462


Satellite: ISS
Catalog Number: 25544
Epoch time:      16056
56670213   =   yrday
fracday
Element set:     908
Inclination:       51
6385  deg
RA of node:       259
6512  deg
Eccentricity:     
0003503     
Arg of perigee:   167
9909  deg
Mean anomaly:     192
1328  deg
Mean motion:   15
54280983  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2746
Checksum:              329


Coasting Arc #10 (Orbit 2760)
---------------------------------------

Vector Time (GMT): 2016/057/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4403644
16                 A    =         6777358
92  meter
 Y    =        -358801
60  meter          E    =           
0015407
 Z    =       -5152798
83                 I    =           51
26444
 XDOT =       -999
928294                 Wp   =          113
11612
 YDOT =      -7466
826786  meter/sec      RA   =          253
97312  deg
 ZDOT =       1371
828144                 TA   =          170
17654
                                          MA   =          170
14638
                                          Ha   =            221
220  n
mi
                                          Hp   =            213
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14447651
44                 X    =        -4374274
85
 Y    =       -1177170
61  feet           Y    =         -407882
56  meter
 Z    =      -16905507
96                 Z    =        -5174119
01
 XDOT =      -3280
604638                 XDOT =        -923
021750
 YDOT =     -24497
463208  feet/sec       YDOT =       -7477
578453  meter/sec
 ZDOT =       4500
748504                 ZDOT =        1367
158597

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13193869
55                 X    =        -4021491
44
 Y    =       -5736814
55  feet           Y    =        -1748581
08  meter
 Z    =      -16997862
44                 Z    =        -5180948
47
 XDOT =       4343
541189                 XDOT =        1323
911354
 YDOT =     -23294
493789  feet/sec       YDOT =       -7100
161707  meter/sec
 ZDOT =       4481
786404                 ZDOT =        1366
048496


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   16057
53110774  
00016717  00000-0  10270-3 0  9093
2 25544  51
6376 254
8400 0003539 171
7511 188
3700 15
54341478 27611


Satellite: ISS
Catalog Number: 25544
Epoch time:      16057
53110774   =   yrday
fracday
Element set:     909
Inclination:       51
6376  deg
RA of node:       254
8400  deg
Eccentricity:     
0003539     
Arg of perigee:   171
7511  deg
Mean anomaly:     188
3700  deg
Mean motion:   15
54341478  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2761
Checksum:              308


Coasting Arc #11 (Orbit 2776)
---------------------------------------

Vector Time (GMT): 2016/058/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4642708
23                 A    =         6780164
97  meter
 Y    =        2136656
34  meter          E    =           
0008568
 Z    =        4447845
48                 I    =           51
28412
 XDOT =        -99
410138                 Wp   =           91
36915
 YDOT =       6957
769991  meter/sec      RA   =          248
94973  deg
 ZDOT =      -3233
403473                 TA   =           31
34523
                                          MA   =           31
29419
                                          Ha   =            220
955  n
mi
                                          Hp   =            214
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15231982
39                 X    =         4596865
01
 Y    =        7010027
37  feet           Y    =         2188318
43  meter
 Z    =       14592668
89                 Z    =         4470286
78
 XDOT =       -326
148747                 XDOT =        -161
499903
 YDOT =      22827
329366  feet/sec       YDOT =        6956
310744  meter/sec
 ZDOT =     -10608
279110                 ZDOT =       -3234
038072

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12266994
99                 X    =         3738980
07
 Y    =       11306488
09  feet           Y    =         3446217
57  meter
 Z    =       14689585
34                 Z    =         4477385
61
 XDOT =      -6404
695980                 XDOT =       -1952
151335
 YDOT =      20758
395520  feet/sec       YDOT =        6327
158955  meter/sec
 ZDOT =     -10612
210456                 ZDOT =       -3234
601747


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   16058
55979372  
00016717  00000-0  10270-3 0  9105
2 25544  51
6380 249
7097 0003497 177
6066 182
5104 15
54350688 27778


Satellite: ISS
Catalog Number: 25544
Epoch time:      16058
55979372   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:       249
7097  deg
Eccentricity:     
0003497     
Arg of perigee:   177
6066  deg
Mean anomaly:     182
5104  deg
Mean motion:   15
54350688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2777
Checksum:              347


Coasting Arc #12 (Orbit 2791)
---------------------------------------

Vector Time (GMT): 2016/059/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4694135
88                 A    =         6784029
56  meter
 Y    =       -3668460
03  meter          E    =           
0005593
 Z    =       -3252576
74                 I    =           51
30949
 XDOT =       1330
272157                 Wp   =          123
20837
 YDOT =      -5885
333274  meter/sec      RA   =          243
93589  deg
 ZDOT =       4720
892643                 TA   =          198
91747
                                          MA   =          198
93825
                                          Ha   =            221
033  n
mi
                                          Hp   =            214
055

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15400708
26                 X    =        -4636965
86
 Y    =      -12035630
02  feet           Y    =        -3720633
70  meter
 Z    =      -10671183
52                 Z    =        -3275240
23
 XDOT =       4364
409963                 XDOT =        1373
052630
 YDOT =     -19308
836201  feet/sec       YDOT =       -5870
217532  meter/sec
 ZDOT =      15488
492924                 ZDOT =        4727
459329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11190361
18                 X    =        -3410822
09
 Y    =      -15959976
19  feet           Y    =        -4864600
74  meter
 Z    =      -10768813
28                 Z    =        -3282334
29
 XDOT =       8508
246679                 XDOT =        2593
313588
 YDOT =     -16429
768276  feet/sec       YDOT =       -5007
793370  meter/sec
 ZDOT =      15517
949767                 ZDOT =        4729
871089


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   16059
52417393  
00016717  00000-0  10270-3 0  9114
2 25544  51
6378 244
8987 0003551 178
8841 181
2320 15
54380715 27921


Satellite: ISS
Catalog Number: 25544
Epoch time:      16059
52417393   =   yrday
fracday
Element set:     911
Inclination:       51
6378  deg
RA of node:       244
8987  deg
Eccentricity:     
0003551     
Arg of perigee:   178
8841  deg
Mean anomaly:     181
2320  deg
Mean motion:   15
54380715  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2792
Checksum:              329


Coasting Arc #13 (Orbit 2807)
---------------------------------------

Vector Time (GMT): 2016/060/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4454933
49                 A    =         6787243
97  meter
 Y    =        4834853
56  meter          E    =           
0015416
 Z    =        1651254
62                 I    =           51
33571
 XDOT =      -2661
825625                 Wp   =          127
86321
 YDOT =       4405
486196  meter/sec      RA   =          238
93528  deg
 ZDOT =      -5690
759714                 TA   =           33
95824
                                          MA   =           33
85966
                                          Ha   =            220
721  n
mi
                                          Hp   =            214
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14615923
53                 X    =         4392516
83
 Y    =       15862380
44  feet           Y    =         4884322
77  meter
 Z    =        5417502
04                 Z    =         1672743
32
 XDOT =      -8733
023705                 XDOT =       -2683
247940
 YDOT =      14453
694870  feet/sec       YDOT =        4375
599508  meter/sec
 ZDOT =     -18670
471503                 ZDOT =       -5703
742617

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9696126
06                 X    =         2955379
22
 Y    =       19241005
62  feet           Y    =         5864658
51  meter
 Z    =        5509855
22                 Z    =         1679403
87
 XDOT =     -10828
210040                 XDOT =       -3300
438420
 YDOT =      10844
492445  feet/sec       YDOT =        3305
401297  meter/sec
 ZDOT =     -18727
491682                 ZDOT =       -5708
139465


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   16060
55282954  
00016717  00000-0  10270-3 0  9123
2 25544  51
6379 239
7681 0003333 185
7696 174
3419 15
54435708 28082


Satellite: ISS
Catalog Number: 25544
Epoch time:      16060
55282954   =   yrday
fracday
Element set:     912
Inclination:       51
6379  deg
RA of node:       239
7681  deg
Eccentricity:     
0003333     
Arg of perigee:   185
7696  deg
Mean anomaly:     174
3419  deg
Mean motion:   15
54435708  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2808
Checksum:              339


Coasting Arc #14 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2016/061/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3915995
99                 A    =         6788439
83  meter
 Y    =       -5539566
98  meter          E    =           
0009884
 Z    =         118633
49                 I    =           51
35712
 XDOT =       3974
146263                 Wp   =           60
25076
 YDOT =      -2673
226179  meter/sec      RA   =          233
94188  deg
 ZDOT =       5986
446042                 TA   =          301
03198
                                          MA   =          301
12899
                                          Ha   =            220
818  n
mi
                                          Hp   =            214
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12847755
87                 X    =        -3854336
40
 Y    =      -18174432
35  feet           Y    =        -5583013
48  meter
 Z    =         389217
50                 Z    =           99760
99
 XDOT =      13038
537607                 XDOT =        3974
664197
 YDOT =      -8770
427097  feet/sec       YDOT =       -2628
781169  meter/sec
 ZDOT =      19640
571003                 ZDOT =        6005
752827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7759973
33                 X    =        -2365239
87
 Y    =      -20861784
94  feet           Y    =        -6358672
05  meter
 Z    =         308310
30                 Z    =           93972
98
 XDOT =      13207
597121                 XDOT =        4025
675602
 YDOT =      -4598
614482  feet/sec       YDOT =       -1401
657694  meter/sec
 ZDOT =      19724
721355                 ZDOT =        6012
095069


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   16061
58147258  
00016717  00000-0  10270-3 0  9135
2 25544  51
6380 234
6369 0003544 185
8326 174
2787 15
54432843 28248


Satellite: ISS
Catalog Number: 25544
Epoch time:      16061
58147258   =   yrday
fracday
Element set:     913
Inclination:       51
6380  deg
RA of node:       234
6369  deg
Eccentricity:     
0003544     
Arg of perigee:   185
8326  deg
Mean anomaly:     174
2787  deg
Mean motion:   15
54432843  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2824
Checksum:              327


Coasting Arc #15 (Orbit 2838)
---------------------------------------

Vector Time (GMT): 2016/062/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2997955
68                 A    =         6786790
18  meter
 Y    =        5774046
76  meter          E    =           
0009572
 Z    =       -1915985
10                 I    =           51
37163
 XDOT =      -5184
937782                 Wp   =          156
00895
 YDOT =        844
271284  meter/sec      RA   =          228
94985  deg
 ZDOT =      -5587
021714                 TA   =           45
19076
                                          MA   =           45
11298
                                          Ha   =            220
650  n
mi
                                          Hp   =            214
236

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9835812
60                 X    =         2942472
99
 Y    =       18943722
97  feet           Y    =         5807261
50  meter
 Z    =       -6286040
35                 Z    =        -1901557
17
 XDOT =     -17010
950728                 XDOT =       -5166
854171
 YDOT =       2769
918911  feet/sec       YDOT =         786
390496  meter/sec
 ZDOT =     -18330
123735                 ZDOT =       -5612
164770

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5046107
41                 X    =         1538053
54
 Y    =       20758502
84  feet           Y    =         6327191
67  meter
 Z    =       -6224428
69                 Z    =        -1897205
86
 XDOT =     -15550
090208                 XDOT =       -4739
667495
 YDOT =      -1730
694921  feet/sec       YDOT =        -527
515812  meter/sec
 ZDOT =     -18439
284493                 ZDOT =       -5620
293913


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   16062
54580937  
00016717  00000-0  10270-3 0  9148
2 25544  51
6380 229
8268 0003294 189
1831 170
9262 15
54475868 28393


Satellite: ISS
Catalog Number: 25544
Epoch time:      16062
54580937   =   yrday
fracday
Element set:     914
Inclination:       51
6380  deg
RA of node:       229
8268  deg
Eccentricity:     
0003294     
Arg of perigee:   189
1831  deg
Mean anomaly:     170
9262  deg
Mean motion:   15
54475868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2839
Checksum:              345


Coasting Arc #16 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2016/063/12:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906643
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1774959
34                 A    =         6783232
25  meter
 Y    =       -5552593
05  meter          E    =           
0012068
 Z    =        3462131
54                 I    =           51
38145
 XDOT =       6125
281220                 Wp   =          107
46296
 YDOT =        877
495426  meter/sec      RA   =          223
95079  deg
 ZDOT =       4530
999048                 TA   =          293
34778
                                          MA   =          293
47470
                                          Ha   =            220
587  n
mi
                                          Hp   =            214
315

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5823357
41                 X    =        -1729554
30
 Y    =      -18217168
79  feet           Y    =        -5572187
66  meter
 Z    =       11358699
29                 Z    =         3453620
07
 XDOT =      20096
066996                 XDOT =        6093
004215
 YDOT =       2878
922002  feet/sec       YDOT =         945
812287  meter/sec
 ZDOT =      14865
482441                 ZDOT =        4560
675320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1685038
66                 X    =         -513599
78
 Y    =      -19072336
79  feet           Y    =        -5813248
25  meter
 Z    =       11322693
77                 Z    =         3451157
06
 XDOT =      17463
239063                 XDOT =        5322
795266
 YDOT =       7391
146681  feet/sec       YDOT =        2252
821508  meter/sec
 ZDOT =      14994
031558                 ZDOT =        4570
180819


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   16063
57442018  
00016717  00000-0  10270-3 0  9150
2 25544  51
6379 224
6956 0003492 193
4955 166
6105 15
54488614 28552


Satellite: ISS
Catalog Number: 25544
Epoch time:      16063
57442018   =   yrday
fracday
Element set:     915
Inclination:       51
6379  deg
RA of node:       224
6956  deg
Eccentricity:     
0003492     
Arg of perigee:   193
4955  deg
Mean anomaly:     166
6105  deg
Mean motion:   15
54488614  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              336
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