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

 
Date: December 5th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


332/03:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 217 7

336/14:51:52 000 0 0 0 0 0 0
N/A 0 0 0 0 219 7
000/00:00:00 000 0 0 0 0 217 6

338/15:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 217 5

338/16:38:45 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 217 5

Coasting Arc #1 (Orbit 3006)
---------------------------------------

Vector Time (GMT): 2016/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -262250
41                 A    =         6779465
10  meter
 Y    =       -4443667
70  meter          E    =           
0008465
 Z    =       -5120661
30                 I    =           51
45901
 XDOT =       7156
916742                 Wp   =          120
79917
 YDOT =      -2237
194819  meter/sec      RA   =          333
02400  deg
 ZDOT =       1572
574817                 TA   =          164
42757
                                          MA   =          164
40152
                                          Ha   =            219
903  n
mi
                                          Hp   =            217
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -860401
60                 X    =         -187666
27
 Y    =      -14578962
28  feet           Y    =        -4446183
30  meter
 Z    =      -16800069
87                 Z    =        -5121754
14
 XDOT =      23480
697974                 XDOT =        7173
762679
 YDOT =      -7339
878016  feet/sec       YDOT =       -2157
067188  meter/sec
 ZDOT =       5159
366196                 ZDOT =        1607
382857

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13434737
21                 X    =         4094907
90
 Y    =        5715200
94  feet           Y    =         1741993
25  meter
 Z    =      -16803960
67                 Z    =        -5121847
21
 XDOT =      -3263
082362                 XDOT =        -994
587504
 YDOT =      23311
794255  feet/sec       YDOT =        7105
434889  meter/sec
 ZDOT =       5312
180502                 ZDOT =        1619
152617


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   16330
51329439  
00016717  00000-0  10270-3 0  9006
2 25544  51
6408 333
5634 0006155 255
7021 104
3448 15
53701844 30074


Satellite: ISS
Catalog Number: 25544
Epoch time:      16330
51329439   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       333
5634  deg
Eccentricity:     
0006155     
Arg of perigee:   255
7021  deg
Mean anomaly:     104
3448  deg
Mean motion:   15
53701844  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3007
Checksum:              284


Coasting Arc #2 (Orbit 3022)
---------------------------------------

Vector Time (GMT): 2016/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1188936
46                 A    =         6781969
09  meter
 Y    =        4951461
32  meter          E    =           
0003237
 Z    =        4478551
19                 I    =           51
43837
 XDOT =      -6848
341762                 Wp   =           46
24009
 YDOT =       1260
787220  meter/sec      RA   =          328
01950  deg
 ZDOT =      -3208
324646                 TA   =           76
13246
                                          MA   =           76
09645
                                          Ha   =            219
602  n
mi
                                          Hp   =            217
584

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3900710
17                 X    =        -1265971
90
 Y    =       16244951
85  feet           Y    =         4937735
02  meter
 Z    =       14693409
42                 Z    =         4472588
51
 XDOT =     -22468
312868                 XDOT =       -6846
346256
 YDOT =       4136
441010  feet/sec       YDOT =        1184
215684  meter/sec
 ZDOT =     -10525
999496                 ZDOT =       -3241
587960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13033605
77                 X    =        -3972643
04
 Y    =      -10489735
17  feet           Y    =        -3197271
28  meter
 Z    =       14666317
11                 Z    =         4470293
46
 XDOT =       4957
328822                 XDOT =        1510
993825
 YDOT =     -21097
236009  feet/sec       YDOT =       -6430
437536  meter/sec
 ZDOT =     -10671
848038                 ZDOT =       -3252
779282


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   16331
54239316  
00016717  00000-0  10270-3 0  9015
2 25544  51
6397 328
4362 0006211 260
2317  99
8135 15
53746063 30235


Satellite: ISS
Catalog Number: 25544
Epoch time:      16331
54239316   =   yrday
fracday
Element set:     901
Inclination:       51
6397  deg
RA of node:       328
4362  deg
Eccentricity:     
0006211     
Arg of perigee:   260
2317  deg
Mean anomaly:      99
8135  deg
Mean motion:   15
53746063  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3023
Checksum:              294


Coasting Arc #3 (Orbit 3032)
---------------------------------------

Vector Time (GMT): 2016/332/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4916785
07                 A    =         6781447
89  meter
 Y    =         994753
19  meter          E    =           
0004940
 Z    =        4564392
74                 I    =           51
42216
 XDOT =      -4003
705344                 Wp   =          162
09868
 YDOT =       5783
831015  meter/sec      RA   =          324
90361  deg
 ZDOT =       3046
805445                 TA   =          257
31609
                                          MA   =          257
37131
                                          Ha   =            219
557  n
mi
                                          Hp   =            217
668

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16131184
61                 X    =         4883123
75
 Y    =        3263625
94  feet           Y    =         1049547
63  meter
 Z    =       14975041
81                 Z    =         4588196
01
 XDOT =     -13135
516219                 XDOT =       -4082
884425
 YDOT =      18975
823540  feet/sec       YDOT =        5738
616085  meter/sec
 ZDOT =       9996
080855                 ZDOT =        3027
163904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3291050
08                 X    =        -1003112
06
 Y    =      -16028416
80  feet           Y    =        -4885461
44  meter
 Z    =       15079028
24                 Z    =         4596087
81
 XDOT =      21466
337531                 XDOT =        6542
939679
 YDOT =       4931
259998  feet/sec       YDOT =        1503
048047  meter/sec
 ZDOT =       9908
951794                 ZDOT =        3020
248507


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   16332
18557813  
00016717  00000-0  10270-3 0  9022
2 25544  51
6421 325
2275 0006387 259
0488 100
9946 15
53760299 30332


Satellite: ISS
Catalog Number: 25544
Epoch time:      16332
18557813   =   yrday
fracday
Element set:     902
Inclination:       51
6421  deg
RA of node:       325
2275  deg
Eccentricity:     
0006387     
Arg of perigee:   259
0488  deg
Mean anomaly:     100
9946  deg
Mean motion:   15
53760299  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3033
Checksum:              318


Coasting Arc #4 (Orbit 3047)
---------------------------------------

Vector Time (GMT): 2016/333/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3850912
76                 A    =         6779058
51  meter
 Y    =       -2142541
62  meter          E    =           
0007714
 Z    =       -5158153
14                 I    =           51
38815
 XDOT =       4991
820436                 Wp   =           76
41287
 YDOT =      -5646
393351  meter/sec      RA   =          319
89611  deg
 ZDOT =      -1381
358558                 TA   =          180
24738
                                          MA   =          180
24776
                                          Ha   =            219
423  n
mi
                                          Hp   =            217
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12634228
22                 X    =        -3801611
51
 Y    =       -7029336
04  feet           Y    =        -2185329
22  meter
 Z    =      -16923074
62                 Z    =        -5176740
64
 XDOT =      16377
363636                 XDOT =        5061
299028
 YDOT =     -18524
912570  feet/sec       YDOT =       -5590
182921  meter/sec
 ZDOT =      -4532
016265                 ZDOT =       -1356
940554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1304364
26                 X    =         -397570
22
 Y    =       14303438
22  feet           Y    =         4359687
97  meter
 Z    =      -17004000
45                 Z    =        -5182819
34
 XDOT =     -22566
582517                 XDOT =       -6878
294351
 YDOT =      -7317
320768  feet/sec       YDOT =       -2230
319370  meter/sec
 ZDOT =      -4424
014060                 ZDOT =       -1348
439485


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   16333
15035117  
00016717  00000-0  10270-3 0  9039
2 25544  51
6421 320
4219 0006240 263
4092  96
6351 15
53749190 30489


Satellite: ISS
Catalog Number: 25544
Epoch time:      16333
15035117   =   yrday
fracday
Element set:     903
Inclination:       51
6421  deg
RA of node:       320
4219  deg
Eccentricity:     
0006240     
Arg of perigee:   263
4092  deg
Mean anomaly:      96
6351  deg
Mean motion:   15
53749190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3048
Checksum:              282


Coasting Arc #5 (Orbit 3063)
---------------------------------------

Vector Time (GMT): 2016/334/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2669570
16                 A    =         6778464
91  meter
 Y    =        3305875
95  meter          E    =           
0003762
 Z    =        5284565
61                 I    =           51
36210
 XDOT =      -5626
026738                 Wp   =          278
42266
 YDOT =       5190
743713  meter/sec      RA   =          314
88152  deg
 ZDOT =       -404
826440                 TA   =          175
45584
                                          MA   =          175
45242
                                          Ha   =            219
190  n
mi
                                          Hp   =            217
530

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8758432
29                 X    =         2606733
97
 Y    =       10846049
71  feet           Y    =         3335377
22  meter
 Z    =       17337813
69                 Z    =         5297381
54
 XDOT =     -18458
092974                 XDOT =       -5681
686314
 YDOT =      17029
999060  feet/sec       YDOT =        5127
518518  meter/sec
 ZDOT =      -1328
170736                 ZDOT =        -432
291663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6159164
01                 X    =         1877313
19
 Y    =      -12429254
76  feet           Y    =        -3788436
85  meter
 Z    =       17393246
94                 Z    =         5301461
67
 XDOT =      22338
846579                 XDOT =        6808
880437
 YDOT =       9040
117309  feet/sec       YDOT =        2755
427756  meter/sec
 ZDOT =      -1449
414054                 ZDOT =        -441
781404


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   16334
17943650  
00016717  00000-0  10270-3 0  9043
2 25544  51
6420 315
2944 0006261 267
3464  92
6972 15
53767722 30648


Satellite: ISS
Catalog Number: 25544
Epoch time:      16334
17943650   =   yrday
fracday
Element set:     904
Inclination:       51
6420  deg
RA of node:       315
2944  deg
Eccentricity:     
0006261     
Arg of perigee:   267
3464  deg
Mean anomaly:      92
6972  deg
Mean motion:   15
53767722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3064
Checksum:              315


Coasting Arc #6 (Orbit 3078)
---------------------------------------

Vector Time (GMT): 2016/335/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1465459
09                 A    =         6779956
95  meter
 Y    =       -4411337
83  meter          E    =           
0006603
 Z    =       -4941687
90                 I    =           51
34596
 XDOT =       5905
853360                 Wp   =          120
36351
 YDOT =      -4379
716346  meter/sec      RA   =          309
86801  deg
 ZDOT =       2157
180897                 TA   =          170
77325
                                          MA   =          170
76112
                                          Ha   =            219
264  n
mi
                                          Hp   =            217
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4807936
64                 X    =        -1392016
47
 Y    =      -14472893
16  feet           Y    =        -4427314
57  meter
 Z    =      -16212886
82                 Z    =        -4948628
80
 XDOT =      19376
159317                 XDOT =        5943
910704
 YDOT =     -14369
148117  feet/sec       YDOT =       -4313
460496  meter/sec
 ZDOT =       7077
365149                 ZDOT =        2185
962647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10935076
07                 X    =        -3333011
19
 Y    =       10585248
13  feet           Y    =         3226383
63  meter
 Z    =      -16242389
71                 Z    =        -4950680
38
 XDOT =     -20629
556749                 XDOT =       -6287
888897
 YDOT =     -10251
340715  feet/sec       YDOT =       -3124
608650  meter/sec
 ZDOT =       7204
205180                 ZDOT =        2195
841739


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   16335
14419947  
00016717  00000-0  10270-3 0  9059
2 25544  51
6429 310
4890 0006208 270
5579  89
4862 15
53782231 30798


Satellite: ISS
Catalog Number: 25544
Epoch time:      16335
14419947   =   yrday
fracday
Element set:     905
Inclination:       51
6429  deg
RA of node:       310
4890  deg
Eccentricity:     
0006208     
Arg of perigee:   270
5579  deg
Mean anomaly:      89
4862  deg
Mean motion:   15
53782231  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3079
Checksum:              331


Coasting Arc #7 (Orbit 3094)
---------------------------------------

Vector Time (GMT): 2016/336/03:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         310590
07                 A    =         6783137
02  meter
 Y    =        5358371
09  meter          E    =           
0005035
 Z    =        4146206
02                 I    =           51
33656
 XDOT =      -5875
581338                 Wp   =           52
58008
 YDOT =       3225
288901  meter/sec      RA   =          304
85783  deg
 ZDOT =      -3721
958739                 TA   =           75
89117
                                          MA   =           75
83521
                                          Ha   =            219
426  n
mi
                                          Hp   =            217
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1018996
28                 X    =          230507
55
 Y    =       17579957
66  feet           Y    =         5361396
21  meter
 Z    =       13603038
11                 Z    =         4147520
74
 XDOT =     -19276
841661                 XDOT =       -5893
130741
 YDOT =      10581
656498  feet/sec       YDOT =        3159
486387  meter/sec
 ZDOT =     -12211
150720                 ZDOT =       -3750
543594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15233888
59                 X    =         4643289
24
 Y    =       -8825763
88  feet           Y    =        -2690092
83  meter
 Z    =       13607734
61                 Z    =         4147637
51
 XDOT =      17510
989884                 XDOT =        5337
349717
 YDOT =      11172
964351  feet/sec       YDOT =        3405
519534  meter/sec
 ZDOT =     -12336
897650                 ZDOT =       -3760
286404


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   16336
17327443  
00016717  00000-0  10270-3 0  9063
2 25544  51
6432 305
3617 0006075 274
9054  85
1405 15
53750497 30953


Satellite: ISS
Catalog Number: 25544
Epoch time:      16336
17327443   =   yrday
fracday
Element set:     906
Inclination:       51
6432  deg
RA of node:       305
3617  deg
Eccentricity:     
0006075     
Arg of perigee:   274
9054  deg
Mean anomaly:      85
1405  deg
Mean motion:   15
53750497  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3095
Checksum:              310


Coasting Arc #8 (Orbit 3101)
---------------------------------------

Vector Time (GMT): 2016/336/14:51:52
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1917055
12                 A    =         6788533
70  meter
 Y    =       -6157752
71  meter          E    =           
0006443
 Z    =       -2105278
95                 I    =           51
34419
 XDOT =       5343
492003                 Wp   =          343
16841
 YDOT =       -214
448983  meter/sec      RA   =          302
42868  deg
 ZDOT =       5494
821593                 TA   =          353
41691
                                          MA   =          353
42537
                                          Ha   =            219
679  n
mi
                                          Hp   =            217
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6289550
93                 X    =         1995996
87
 Y    =      -20202600
77  feet           Y    =        -6135873
35  meter
 Z    =       -6907083
17                 Z    =        -2095775
04
 XDOT =      17531
141741                 XDOT =        5318
801091
 YDOT =       -703
572780  feet/sec       YDOT =        -154
832988  meter/sec
 ZDOT =      18027
629898                 ZDOT =        5520
719263

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21072061
36                 X    =         6422764
30
 Y    =       -2064289
80  feet           Y    =         -629195
53  meter
 Z    =       -6864274
48                 Z    =        -2092230
86
 XDOT =       7300
397169                 XDOT =        2225
161057
 YDOT =      14218
348886  feet/sec       YDOT =        4333
752741  meter/sec
 ZDOT =      18141
022062                 ZDOT =        5529
383524


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   16336
62349243  
00016717  00000-0  10270-3 0  9076
2 25544  51
6415 303
1219 0006228 282
1832  77
8623 15
53763262 31026


Satellite: ISS
Catalog Number: 25544
Epoch time:      16336
62349243   =   yrday
fracday
Element set:     907
Inclination:       51
6415  deg
RA of node:       303
1219  deg
Eccentricity:     
0006228     
Arg of perigee:   282
1832  deg
Mean anomaly:      77
8623  deg
Mean motion:   15
53763262  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3102
Checksum:              296


Coasting Arc #9 (Orbit 3117)
---------------------------------------

Vector Time (GMT): 2016/337/14:51:52
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2715041
28                 A    =         6790248
41  meter
 Y    =        6193810
13  meter          E    =           
0007741
 Z    =         555450
59                 I    =           51
33436
 XDOT =      -4599
314783                 Wp   =          148
10055
 YDOT =      -1479
381905  meter/sec      RA   =          297
43836  deg
 ZDOT =      -5953
276158                 TA   =           25
88160
                                          MA   =           25
84290
                                          Ha   =            219
841  n
mi
                                          Hp   =            217
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8907615
76                 X    =        -2786798
43
 Y    =       20320899
37  feet           Y    =         6163047
45  meter
 Z    =        1822344
45                 Z    =          542087
72
 XDOT =     -15089
615429                 XDOT =       -4553
511426
 YDOT =      -4853
615174  feet/sec       YDOT =       -1530
557925  meter/sec
 ZDOT =     -19531
745926                 ZDOT =       -5975
507546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22192023
51                 X    =        -6764128
77
 Y    =         112593
26  feet           Y    =           34318
43  meter
 Z    =        1762646
91                 Z    =          537254
78
 XDOT =      -1638
737918                 XDOT =        -499
487317
 YDOT =     -14025
977284  feet/sec       YDOT =       -4275
117876  meter/sec
 ZDOT =     -19628
762735                 ZDOT =       -5982
846882


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   16337
65255980  
00016717  00000-0  10270-3 0  9085
2 25544  51
6424 297
9955 0006226 285
3418  74
7046 15
53770019 31186


Satellite: ISS
Catalog Number: 25544
Epoch time:      16337
65255980   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:       297
9955  deg
Eccentricity:     
0006226     
Arg of perigee:   285
3418  deg
Mean anomaly:      74
7046  deg
Mean motion:   15
53770019  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3118
Checksum:              335


Coasting Arc #10 (Orbit 3133)
---------------------------------------

Vector Time (GMT): 2016/338/14:51:52
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3306814
60                 A    =         6789879
37  meter
 Y    =       -5830633
74  meter          E    =           
0011033
 Z    =        1036512
55                 I    =           51
31922
 XDOT =       3770
050949                 Wp   =           29
13974
 YDOT =       3184
913146  meter/sec      RA   =          292
44814  deg
 ZDOT =       5871
252175                 TA   =          342
14923
                                          MA   =          342
18795
                                          Ha   =            219
988  n
mi
                                          Hp   =            217
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10849129
27                 X    =         3366733
51
 Y    =      -19129375
79  feet           Y    =        -5793319
77  meter
 Z    =        3400631
72                 Z    =         1052721
39
 XDOT =      12368
933559                 XDOT =        3705
636069
 YDOT =      10449
190112  feet/sec       YDOT =        3226
711759  meter/sec
 ZDOT =      19262
638370                 ZDOT =        5889
410035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21911638
61                 X    =         6678667
45
 Y    =        1738196
09  feet           Y    =          529802
17  meter
 Z    =        3472706
13                 Z    =         1058480
83
 XDOT =      -4177
735732                 XDOT =       -1273
373851
 YDOT =      13913
563066  feet/sec       YDOT =        4240
854023  meter/sec
 ZDOT =      19341
500872                 ZDOT =        5895
289466


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   16338
68162130  
00016717  00000-0  10270-3 0  9094
2 25544  51
6424 292
8684 0006301 289
8205  70
2268 15
53777034 31345


Satellite: ISS
Catalog Number: 25544
Epoch time:      16338
68162130   =   yrday
fracday
Element set:     909
Inclination:       51
6424  deg
RA of node:       292
8684  deg
Eccentricity:     
0006301     
Arg of perigee:   289
8205  deg
Mean anomaly:      70
2268  deg
Mean motion:   15
53777034  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3134
Checksum:              313


Coasting Arc #11 (Orbit 3133)
---------------------------------------

Vector Time (GMT): 2016/338/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 896210
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4563833
84                 A    =         6784731
30  meter
 Y    =       -3488655
39  meter          E    =           
0006097
 Z    =        3603813
36                 I    =           51
30228
 XDOT =       1250
847731                 Wp   =           78
21207
 YDOT =       6167
975128  meter/sec      RA   =          292
43563  deg
 ZDOT =       4381
738522                 TA   =          324
70372
                                          MA   =          324
74407
                                          Ha   =            219
881  n
mi
                                          Hp   =            217
489

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14973208
15                 X    =         4584999
82
 Y    =      -11445719
77  feet           Y    =        -3437501
47  meter
 Z    =       11823534
63                 Z    =         3626034
58
 XDOT =       4103
831138                 XDOT =        1160
498174
 YDOT =      20236
138873  feet/sec       YDOT =        6181
457427  meter/sec
 ZDOT =      14375
782553                 ZDOT =        4387
595899

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16961744
97                 X    =         5169939
87
 Y    =        8073111
27  feet           Y    =         2460684
32  meter
 Z    =       11921472
92                 Z    =         3633664
95
 XDOT =     -15619
471652                 XDOT =       -4760
814960
 YDOT =      11527
707811  feet/sec       YDOT =        3513
645341  meter/sec
 ZDOT =      14400
228390                 ZDOT =        4389
189613


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   16338
68162098  
00016717  00000-0  10270-3 0  9109
2 25544  51
6426 292
8685 0006258 289
4478  70
5998 15
53784477 31349


Satellite: ISS
Catalog Number: 25544
Epoch time:      16338
68162098   =   yrday
fracday
Element set:     910
Inclination:       51
6426  deg
RA of node:       292
8685  deg
Eccentricity:     
0006258     
Arg of perigee:   289
4478  deg
Mean anomaly:      70
5998  deg
Mean motion:   15
53784477  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3134
Checksum:              362


Coasting Arc #12 (Orbit 3134)
---------------------------------------

Vector Time (GMT): 2016/338/16:38:45
000
Vector Time (MET): N/A
Weight (LBS)     : 911335
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4616274
99                 A    =         6780180
90  meter
 Y    =       -1010993
17  meter          E    =           
0001432
 Z    =        4862605
72                 I    =           51
28761
 XDOT =       -898
827478                 Wp   =          184
79614
 YDOT =       7239
947237  meter/sec      RA   =          292
08590  deg
 ZDOT =       2357
212940                 TA   =          241
99161
                                          MA   =          242
00610
                                          Ha   =            219
886  n
mi
                                          Hp   =            217
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15145259
15                 X    =         4603616
52
 Y    =       -3316906
71  feet           Y    =         -959442
04  meter
 Z    =       15953430
84                 Z    =         4884999
72
 XDOT =      -2948
909047                 XDOT =        -991
170005
 YDOT =      23753
107733  feet/sec       YDOT =        7229
379442  meter/sec
 ZDOT =       7733
638255                 ZDOT =        2352
622916

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13866943
85                 X    =         4226644
49
 Y    =        6704119
02  feet           Y    =         2043415
48  meter
 Z    =       16051646
55                 Z    =         4892541
87
 XDOT =     -16566
944797                 XDOT =       -5049
604774
 YDOT =      15791
699787  feet/sec       YDOT =        4813
310095  meter/sec
 ZDOT =       7712
148833                 ZDOT =        2350
662964


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   16338
74593645  
00016717  00000-0  10270-3 0  9113
2 25544  51
6441 292
5488 0006281 289
5502  70
4972 15
53784082 31353


Satellite: ISS
Catalog Number: 25544
Epoch time:      16338
74593645   =   yrday
fracday
Element set:     911
Inclination:       51
6441  deg
RA of node:       292
5488  deg
Eccentricity:     
0006281     
Arg of perigee:   289
5502  deg
Mean anomaly:      70
4972  deg
Mean motion:   15
53784082  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3135
Checksum:              330


Coasting Arc #13 (Orbit 3149)
---------------------------------------

Vector Time (GMT): 2016/339/16:38:45
000
Vector Time (MET): N/A
Weight (LBS)     : 911335
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4239019
02                 A    =         6778357
02  meter
 Y    =        -580859
21  meter          E    =           
0009587
 Z    =       -5265313
28                 I    =           51
27008
 XDOT =       1773
011039                 Wp   =           66
73096
 YDOT =      -7428
848616  meter/sec      RA   =          287
06620  deg
 ZDOT =       -605
046835                 TA   =          197
44231
                                          MA   =          197
47527
                                          Ha   =            220
146  n
mi
                                          Hp   =            217
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13907542
72                 X    =        -4206631
96
 Y    =       -1905706
08  feet           Y    =         -628081
33  meter
 Z    =      -17274649
86                 Z    =        -5285826
81
 XDOT =       5816
965352                 XDOT =        1858
889621
 YDOT =     -24372
862915  feet/sec       YDOT =       -7408
541399  meter/sec
 ZDOT =      -1985
061794                 ZDOT =        -596
225880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9827092
10                 X    =        -2995297
67
 Y    =       -9867789
05  feet           Y    =        -3007702
10  meter
 Z    =      -17364330
92                 Z    =        -5292648
06
 XDOT =      18672
821694                 XDOT =        5691
476052
 YDOT =     -15156
833394  feet/sec       YDOT =       -4619
802818  meter/sec
 ZDOT =      -1945
031487                 ZDOT =        -592
845597


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   16339
71067356  
00016717  00000-0  10270-3 0  9127
2 25544  51
6435 287
7424 0006377 293
9863  66
0622 15
53823722 31502


Satellite: ISS
Catalog Number: 25544
Epoch time:      16339
71067356   =   yrday
fracday
Element set:     912
Inclination:       51
6435  deg
RA of node:       287
7424  deg
Eccentricity:     
0006377     
Arg of perigee:   293
9863  deg
Mean anomaly:      66
0622  deg
Mean motion:   15
53823722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3150
Checksum:              323


Coasting Arc #14 (Orbit 3165)
---------------------------------------

Vector Time (GMT): 2016/340/16:38:45
000
Vector Time (MET): N/A
Weight (LBS)     : 911335
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3776911
29                 A    =         6778689
12  meter
 Y    =        2211244
07  meter          E    =           
0005708
 Z    =        5179471
18                 I    =           51
26202
 XDOT =      -2515
270496                 Wp   =          335
50832
 YDOT =       7139
572031  meter/sec      RA   =          282
04406  deg
 ZDOT =      -1209
279694                 TA   =          126
18623
                                          MA   =          126
13343
                                          Ha   =            220
266  n
mi
                                          Hp   =            217
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12391441
25                 X    =         3726744
20
 Y    =        7254737
75  feet           Y    =         2253199
24  meter
 Z    =       16993015
69                 Z    =         5197696
78
 XDOT =      -8252
199791                 XDOT =       -2589
045911
 YDOT =      23423
792753  feet/sec       YDOT =        7111
032149  meter/sec
 ZDOT =      -3967
453063                 ZDOT =       -1221
677075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5610645
94                 X    =         1710124
88
 Y    =       13114731
84  feet           Y    =         3997370
26  meter
 Z    =       17072377
67                 Z    =         5203660
71
 XDOT =     -19530
895794                 XDOT =       -5953
017038
 YDOT =      13612
334118  feet/sec       YDOT =        4149
039439  meter/sec
 ZDOT =      -4023
068097                 ZDOT =       -1226
231156


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   16340
73972054  
00016717  00000-0  10270-3 0  9132
2 25544  51
6428 282
6156 0006429 296
9742  63
0754 15
53840281 31666


Satellite: ISS
Catalog Number: 25544
Epoch time:      16340
73972054   =   yrday
fracday
Element set:     913
Inclination:       51
6428  deg
RA of node:       282
6156  deg
Eccentricity:     
0006429     
Arg of perigee:   296
9742  deg
Mean anomaly:      63
0754  deg
Mean motion:   15
53840281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3166
Checksum:              322


Coasting Arc #15 (Orbit 3180)
---------------------------------------

Vector Time (GMT): 2016/341/16:38:45
000
Vector Time (MET): N/A
Weight (LBS)     : 911335
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3277955
01                 A    =         6781046
95  meter
 Y    =       -3727344
54  meter          E    =           
0004242
 Z    =       -4623801
30                 I    =           51
26372
 XDOT =       3134
026203                 Wp   =           92
95162
 YDOT =      -6360
754968  meter/sec      RA   =          277
02435  deg
 ZDOT =       2907
834730                 TA   =          206
14243
                                          MA   =          206
16386
                                          Ha   =            220
427  n
mi
                                          Hp   =            217
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10754445
57                 X    =        -3213570
77
 Y    =      -12228820
68  feet           Y    =        -3763640
65  meter
 Z    =      -15169951
78                 Z    =        -4639568
60
 XDOT =      10282
238200                 XDOT =        3190
795825
 YDOT =     -20868
618660  feet/sec       YDOT =       -6325
390883  meter/sec
 ZDOT =       9540
140190                 ZDOT =        2923
196710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1636197
23                 X    =         -498712
92
 Y    =      -16138381
77  feet           Y    =        -4918978
76  meter
 Z    =      -15238276
94                 Z    =        -4644626
81
 XDOT =      19218
002431                 XDOT =        5857
647141
 YDOT =     -11014
604025  feet/sec       YDOT =       -3357
251307  meter/sec
 ZDOT =       9608
572237                 ZDOT =        2928
692818


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   16341
70444770  
00016717  00000-0  10270-3 0  9140
2 25544  51
6425 277
8087 0006488 300
6187  59
4325 15
53833135 31813


Satellite: ISS
Catalog Number: 25544
Epoch time:      16341
70444770   =   yrday
fracday
Element set:     914
Inclination:       51
6425  deg
RA of node:       277
8087  deg
Eccentricity:     
0006488     
Arg of perigee:   300
6187  deg
Mean anomaly:      59
4325  deg
Mean motion:   15
53833135  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3181
Checksum:              317


Coasting Arc #16 (Orbit 3196)
---------------------------------------

Vector Time (GMT): 2016/342/16:38:45
000
Vector Time (MET): N/A
Weight (LBS)     : 911335
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2733887
00                 A    =         6784452
64  meter
 Y    =        5038447
13  meter          E    =           
0007999
 Z    =        3627607
67                 I    =           51
27284
 XDOT =      -3671
748194                 Wp   =           53
83900
 YDOT =       5133
225954  meter/sec      RA   =          272
01189  deg
 ZDOT =      -4351
096057                 TA   =           82
88951
                                          MA   =           82
79856
                                          Ha   =            220
706  n
mi
                                          Hp   =            216
986

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8969445
54                 X    =         2659721
17
 Y    =       16530338
36  feet           Y    =         5068604
49  meter
 Z    =       11901599
97                 Z    =         3640708
29
 XDOT =     -12046
417959                 XDOT =       -3707
740502
 YDOT =      16841
292500  feet/sec       YDOT =        5091
964889  meter/sec
 ZDOT =     -14275
249532                 ZDOT =       -4369
019838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1966873
28                 X    =         -599502
98
 Y    =       18667841
26  feet           Y    =         5689958
02  meter
 Z    =       11958019
62                 Z    =         3644804
38
 XDOT =     -18002
007967                 XDOT =       -5487
012028
 YDOT =       7322
210825  feet/sec       YDOT =        2231
809859  meter/sec
 ZDOT =     -14354
657306                 ZDOT =       -4375
299547


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   16342
73348079  
00016717  00000-0  10270-3 0  9150
2 25544  51
6429 272
6810 0006626 305
6297  54
4238 15
53870122 31977


Satellite: ISS
Catalog Number: 25544
Epoch time:      16342
73348079   =   yrday
fracday
Element set:     915
Inclination:       51
6429  deg
RA of node:       272
6810  deg
Eccentricity:     
0006626     
Arg of perigee:   305
6297  deg
Mean anomaly:      54
4238  deg
Mean motion:   15
53870122  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3197
Checksum:              321


Coasting Arc #17 (Orbit 3211)
---------------------------------------

Vector Time (GMT): 2016/343/16:38:45
000
Vector Time (MET): N/A
Weight (LBS)     : 911335
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2164349
09                 A    =         6787909
26  meter
 Y    =       -6000334
56  meter          E    =           
0008253
 Z    =       -2305471
26                 I    =           51
28199
 XDOT =       4138
131577                 Wp   =          352
69041
 YDOT =      -3560
053378  meter/sec      RA   =          267
00817  deg
 ZDOT =       5386
652670                 TA   =          341
48285
                                          MA   =          341
51286
                                          Ha   =            220
816  n
mi
                                          Hp   =            216
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7100882
83                 X    =        -2085891
87
 Y    =      -19686137
01  feet           Y    =        -6024099
02  meter
 Z    =       -7563882
09                 Z    =        -2315794
81
 XDOT =      13576
547169                 XDOT =        4151
467212
 YDOT =     -11679
965150  feet/sec       YDOT =       -3513
703594  meter/sec
 ZDOT =      17672
744981                 ZDOT =        5406
787126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4916179
36                 X    =         1498451
47
 Y    =      -20325566
49  feet           Y    =        -6195232
67  meter
 Z    =       -7607980
45                 Z    =        -2318912
44
 XDOT =      16180
981371                 XDOT =        4931
963122
 YDOT =      -2727
312482  feet/sec       YDOT =        -831
284844  meter/sec
 ZDOT =      17761
535303                 ZDOT =        5413
715960


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   16343
69819516  
00016717  00000-0  10270-3 0  9166
2 25544  51
6410 267
8735 0006568 308
4488  51
6075 15
53831975 32126


Satellite: ISS
Catalog Number: 25544
Epoch time:      16343
69819516   =   yrday
fracday
Element set:     916
Inclination:       51
6410  deg
RA of node:       267
8735  deg
Eccentricity:     
0006568     
Arg of perigee:   308
4488  deg
Mean anomaly:      51
6075  deg
Mean motion:   15
53831975  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3212
Checksum:              336


Coasting Arc #18 (Orbit 3227)
---------------------------------------

Vector Time (GMT): 2016/344/16:38:45
000
Vector Time (MET): N/A
Weight (LBS)     : 911335
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1528391
57                 A    =         6789908
76  meter
 Y    =        6569939
21  meter          E    =           
0006842
 Z    =         749592
44                 I    =           51
29192
 XDOT =      -4547
593941                 Wp   =          122
24926
 YDOT =       1737
591332  meter/sec      RA   =          262
01323  deg
 ZDOT =      -5920
905944                 TA   =           49
61397
                                          MA   =           49
55427
                                          Ha   =            221
002  n
mi
                                          Hp   =            216
745

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5014408
02                 X    =         1451169
99
 Y    =       21554918
67  feet           Y    =         6586598
91  meter
 Z    =        2459292
79                 Z    =          756829
72
 XDOT =     -14919
927628                 XDOT =       -4537
924623
 YDOT =       5700
758962  feet/sec       YDOT =        1686
791343  meter/sec
 ZDOT =     -19425
544437                 ZDOT =       -5942
973715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7299903
66                 X    =        -2225010
63
 Y    =       20888257
18  feet           Y    =         6366740
79  meter
 Z    =        2489788
37                 Z    =          758887
49
 XDOT =     -14025
498905                 XDOT =       -4274
972066
 YDOT =      -2560
591431  feet/sec       YDOT =        -780
468268  meter/sec
 ZDOT =     -19522
466006                 ZDOT =       -5950
447639


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   16344
72721776  
00016717  00000-0  10270-3 0  9172
2 25544  51
6415 262
7467 0006496 311
9177  48
1421 15
53844474 32282


Satellite: ISS
Catalog Number: 25544
Epoch time:      16344
72721776   =   yrday
fracday
Element set:     917
Inclination:       51
6415  deg
RA of node:       262
7467  deg
Eccentricity:     
0006496     
Arg of perigee:   311
9177  deg
Mean anomaly:      48
1421  deg
Mean motion:   15
53844474  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3228
Checksum:              328
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