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

 
Date: December 9th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14100 72 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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


There are no maneuvers



Coasting Arc #1 (Orbit 1501)
---------------------------------------

Vector Time (GMT): 2015/341/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         779604
69                 A    =         6781271
19  meter
 Y    =        5395192
12  meter          E    =           
0002790
 Z    =        4031046
46                 I    =           51
31806
 XDOT =      -5489
201292                 Wp   =           93
11591
 YDOT =       3692
429525  meter/sec      RA   =          298
08020  deg
 ZDOT =      -3878
192874                 TA   =           37
27361
                                          MA   =           37
25425
                                          Ha   =            219
029  n
mi
                                          Hp   =            217
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2557758
17                 X    =          699634
80
 Y    =       17700761
54  feet           Y    =         5403462
87  meter
 Z    =       13225218
05                 Z    =         4034639
66
 XDOT =     -18009
190589                 XDOT =       -5511
243898
 YDOT =      12114
270095  feet/sec       YDOT =        3630
922559  meter/sec
 ZDOT =     -12723
729901                 ZDOT =       -3904
912118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17174173
86                 X    =        -5234688
19
 Y    =        4952265
32  feet           Y    =         1509450
47  meter
 Z    =       13239648
75                 Z    =         4035444
94
 XDOT =     -14166
093358                 XDOT =       -4317
825256
 YDOT =     -14781
254069  feet/sec       YDOT =       -4505
326240  meter/sec
 ZDOT =     -12839
895676                 ZDOT =       -3913
600202


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   15341
60477548  
00016717  00000-0  10270-3 0  9002
2 25544  51
6425 298
6048 0008104 253
1186 106
9079 15
54523176 15020


Satellite: ISS
Catalog Number: 25544
Epoch time:      15341
60477548   =   yrday
fracday
Element set:     900
Inclination:       51
6425  deg
RA of node:       298
6048  deg
Eccentricity:     
0008104     
Arg of perigee:   253
1186  deg
Mean anomaly:     106
9079  deg
Mean motion:   15
54523176  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1502
Checksum:              306


Coasting Arc #2 (Orbit 1516)
---------------------------------------

Vector Time (GMT): 2015/342/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         391780
83                 A    =         6785258
22  meter
 Y    =       -6249313
60  meter          E    =           
0004094
 Z    =       -2608567
37                 I    =           51
31719
 XDOT =       5316
745968                 Wp   =          287
75523
 YDOT =      -1842
659833  meter/sec      RA   =          293
07188  deg
 ZDOT =       5207
423839                 TA   =           42
73066
                                          MA   =           42
69884
                                          Ha   =            218
838  n
mi
                                          Hp   =            217
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1285370
18                 X    =          474304
69
 Y    =      -20502997
39  feet           Y    =        -6244470
89  meter
 Z    =       -8558291
91                 Z    =        -2606464
06
 XDOT =      17443
392284                 XDOT =        5311
659808
 YDOT =      -6045
471892  feet/sec       YDOT =       -1783
233201  meter/sec
 ZDOT =      17084
723880                 ZDOT =        5233
239476

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20457095
66                 X    =         6235322
76
 Y    =       -1925941
97  feet           Y    =         -587027
11  meter
 Z    =       -8547948
49                 Z    =        -2605414
70
 XDOT =       8573
818995                 XDOT =        2613
300030
 YDOT =      14665
153233  feet/sec       YDOT =        4469
938706  meter/sec
 ZDOT =      17196
610975                 ZDOT =        5241
527025


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   15342
56905285  
00016717  00000-0  10270-3 0  9013
2 25544  51
6424 293
7941 0008132 257
0879 102
9366 15
54538052 15170


Satellite: ISS
Catalog Number: 25544
Epoch time:      15342
56905285   =   yrday
fracday
Element set:     901
Inclination:       51
6424  deg
RA of node:       293
7941  deg
Eccentricity:     
0008132     
Arg of perigee:   257
0879  deg
Mean anomaly:     102
9366  deg
Mean motion:   15
54538052  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1517
Checksum:              317


Coasting Arc #3 (Orbit 1532)
---------------------------------------

Vector Time (GMT): 2015/343/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1421814
26                 A    =         6787761
02  meter
 Y    =        6574617
26  meter          E    =           
0009680
 Z    =         859261
20                 I    =           51
31518
 XDOT =      -4883
818317                 Wp   =          162
35129
 YDOT =       -282
923079  meter/sec      RA   =          288
07348  deg
 ZDOT =      -5907
987227                 TA   =            8
30677
                                          MA   =            8
29076
                                          Ha   =            218
531  n
mi
                                          Hp   =            217
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4664744
95                 X    =        -1499401
59
 Y    =       21570266
61  feet           Y    =         6558283
72  meter
 Z    =        2819098
43                 Z    =          852166
24
 XDOT =     -16023
025973                 XDOT =       -4851
592449
 YDOT =       -928
225326  feet/sec       YDOT =        -337
356537  meter/sec
 ZDOT =     -19383
160194                 ZDOT =       -5931
633938

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22057495
03                 X    =        -6723124
48
 Y    =        -826054
95  feet           Y    =         -251781
55  meter
 Z    =        2787132
84                 Z    =          849518
09
 XDOT =      -1933
612362                 XDOT =        -589
365048
 YDOT =     -14206
764240  feet/sec       YDOT =       -4330
221740  meter/sec
 ZDOT =     -19485
252744                 ZDOT =       -5939
105037


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   15343
59759878  
00016717  00000-0  10270-3 0  9023
2 25544  51
6434 288
6632 0008066 260
2791  99
7451 15
54563175 15336


Satellite: ISS
Catalog Number: 25544
Epoch time:      15343
59759878   =   yrday
fracday
Element set:     902
Inclination:       51
6434  deg
RA of node:       288
6632  deg
Eccentricity:     
0008066     
Arg of perigee:   260
2791  deg
Mean anomaly:      99
7451  deg
Mean motion:   15
54563175  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1533
Checksum:              343


Coasting Arc #4 (Orbit 1548)
---------------------------------------

Vector Time (GMT): 2015/344/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2288554
89                 A    =         6787543
28  meter
 Y    =       -6305761
42  meter          E    =           
0007525
 Z    =        1001710
91                 I    =           51
30560
 XDOT =       4256
751314                 Wp   =           25
07671
 YDOT =       2480
042860  meter/sec      RA   =          283
07787  deg
 ZDOT =       5877
119780                 TA   =          345
83085
                                          MA   =          345
85195
                                          Ha   =            218
173  n
mi
                                          Hp   =            217
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7508382
20                 X    =         2354031
38
 Y    =      -20688193
64  feet           Y    =        -6279803
28  meter
 Z    =        3286453
11                 Z    =         1012986
87
 XDOT =      13965
719535                 XDOT =        4200
153331
 YDOT =       8136
623556  feet/sec       YDOT =        2527
327682  meter/sec
 ZDOT =      19281
889042                 ZDOT =        5897
661234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21741666
32                 X    =         6626859
89
 Y    =        3368408
34  feet           Y    =         1026690
86  meter
 Z    =        3336420
88                 Z    =         1016941
08
 XDOT =      -5078
595865                 XDOT =       -1547
956020
 YDOT =      13563
426453  feet/sec       YDOT =        4134
132383  meter/sec
 ZDOT =      19370
133625                 ZDOT =        5904
016729


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   15344
62612666  
00016717  00000-0  10270-3 0  9032
2 25544  51
6433 283
5319 0008085 264
7331  95
2900 15
54592383 15491


Satellite: ISS
Catalog Number: 25544
Epoch time:      15344
62612666   =   yrday
fracday
Element set:     903
Inclination:       51
6433  deg
RA of node:       283
5319  deg
Eccentricity:     
0008085     
Arg of perigee:   264
7331  deg
Mean anomaly:      95
2900  deg
Mean motion:   15
54592383  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1549
Checksum:              317


Coasting Arc #5 (Orbit 1563)
---------------------------------------

Vector Time (GMT): 2015/345/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2994671
12                 A    =         6784628
23  meter
 Y    =        5428776
50  meter          E    =           
0004877
 Z    =       -2747835
27                 I    =           51
29090
 XDOT =      -3497
500228                 Wp   =          235
59902
 YDOT =      -4519
381736  meter/sec      RA   =          278
07752  deg
 ZDOT =      -5113
265368                 TA   =          335
68312
                                          MA   =          335
70613
                                          Ha   =            217
311  n
mi
                                          Hp   =            216
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9825036
48                 X    =        -3041806
40
 Y    =       17810946
54  feet           Y    =         5395024
84  meter
 Z    =       -9015207
57                 Z    =        -2762496
87
 XDOT =     -11474
738282                 XDOT =       -3421
864931
 YDOT =     -14827
367900  feet/sec       YDOT =       -4558
069688  meter/sec
 ZDOT =     -16775
805014                 ZDOT =       -5130
072413

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19459194
54                 X    =        -5931162
50
 Y    =       -5825403
08  feet           Y    =        -1775582
86  meter
 Z    =       -9079622
92                 Z    =        -2767469
07
 XDOT =      11698
259020                 XDOT =        3565
629349
 YDOT =     -12798
632234  feet/sec       YDOT =       -3901
023105  meter/sec
 ZDOT =     -16847
520800                 ZDOT =       -5135
124340


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   15345
59035516  
00016717  00000-0  10270-3 0  9043
2 25544  51
6443 278
7219 0008106 268
1397  91
8828 15
54627716 15648


Satellite: ISS
Catalog Number: 25544
Epoch time:      15345
59035516   =   yrday
fracday
Element set:     904
Inclination:       51
6443  deg
RA of node:       278
7219  deg
Eccentricity:     
0008106     
Arg of perigee:   268
1397  deg
Mean anomaly:      91
8828  deg
Mean motion:   15
54627716  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1564
Checksum:              335


Coasting Arc #6 (Orbit 1579)
---------------------------------------

Vector Time (GMT): 2015/346/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3550119
06                 A    =         6780425
92  meter
 Y    =       -4015457
03  meter          E    =           
0003035
 Z    =        4152925
44                 I    =           51
27312
 XDOT =       2643
559269                 Wp   =          141
44902
 YDOT =       6171
237325  meter/sec      RA   =          273
06524  deg
 ZDOT =       3703
319070                 TA   =          270
28125
                                          MA   =          270
31603
                                          Ha   =            217
216  n
mi
                                          Hp   =            216
847

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11647372
25                 X    =         3574583
60
 Y    =      -13174071
62  feet           Y    =        -3975620
88  meter
 Z    =       13625083
46                 Z    =         4170230
32
 XDOT =       8673
094716                 XDOT =        2556
365100
 YDOT =      20246
841619  feet/sec       YDOT =        6200
311447  meter/sec
 ZDOT =      12149
996948                 ZDOT =        3715
949853

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15444283
26                 X    =         4707417
54
 Y    =        8284140
98  feet           Y    =         2525006
17  meter
 Z    =       13700637
41                 Z    =         4175954
28
 XDOT =     -17177
866891                 XDOT =       -5235
813828
 YDOT =      11822
132922  feet/sec       YDOT =        3603
386114  meter/sec
 ZDOT =      12203
357025                 ZDOT =        3719
583221


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   15346
61884961  
00016717  00000-0  10270-3 0  9054
2 25544  51
6440 273
5906 0008056 271
9682  88
0549 15
54646522 15806


Satellite: ISS
Catalog Number: 25544
Epoch time:      15346
61884961   =   yrday
fracday
Element set:     905
Inclination:       51
6440  deg
RA of node:       273
5906  deg
Eccentricity:     
0008056     
Arg of perigee:   271
9682  deg
Mean anomaly:      88
0549  deg
Mean motion:   15
54646522  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1580
Checksum:              334


Coasting Arc #7 (Orbit 1594)
---------------------------------------

Vector Time (GMT): 2015/347/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3968907
67                 A    =         6776796
22  meter
 Y    =        2200773
44  meter          E    =           
0006149
 Z    =       -5038025
99                 I    =           51
26117
 XDOT =      -1707
620596                 Wp   =           50
25832
 YDOT =      -7247
682317  meter/sec      RA   =          268
04076  deg
 ZDOT =      -1818
396283                 TA   =          202
02171
                                          MA   =          202
04814
                                          Ha   =            217
901  n
mi
                                          Hp   =            217
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13021350
63                 X    =        -3968749
44
 Y    =        7220385
29  feet           Y    =         2156391
86  meter
 Z    =      -16528956
66                 Z    =        -5057305
58
 XDOT =      -5602
429778                 XDOT =       -1617
615235
 YDOT =     -23778
485292  feet/sec       YDOT =       -7266
274633  meter/sec
 ZDOT =      -5965
867070                 ZDOT =       -1826
473656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10137488
35                 X    =        -3089906
45
 Y    =      -10777098
86  feet           Y    =        -3284859
73  meter
 Z    =      -16612688
35                 Z    =        -5063547
41
 XDOT =      20931
820443                 XDOT =        6380
018871
 YDOT =     -10429
665861  feet/sec       YDOT =       -3178
962154  meter/sec
 ZDOT =      -5999
358982                 ZDOT =       -1828
604618


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   15347
58304658  
00016717  00000-0  10270-3 0  9062
2 25544  51
6444 268
7803 0008086 275
8979  84
1252 15
54699641 15951


Satellite: ISS
Catalog Number: 25544
Epoch time:      15347
58304658   =   yrday
fracday
Element set:     906
Inclination:       51
6444  deg
RA of node:       268
7803  deg
Eccentricity:     
0008086     
Arg of perigee:   275
8979  deg
Mean anomaly:      84
1252  deg
Mean motion:   15
54699641  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1595
Checksum:              357


Coasting Arc #8 (Orbit 1610)
---------------------------------------

Vector Time (GMT): 2015/348/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4247959
78                 A    =         6775618
26  meter
 Y    =        -169382
82  meter          E    =           
0005979
 Z    =        5280908
08                 I    =           51
25915
 XDOT =        687
544437                 Wp   =          288
74635
 YDOT =       7628
511855  meter/sec      RA   =          263
00845  deg
 ZDOT =       -306
776551                 TA   =          164
20405
                                          MA   =          164
18539
                                          Ha   =            218
309  n
mi
                                          Hp   =            217
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13936875
90                 X    =         4223885
56
 Y    =        -555717
91  feet           Y    =         -122014
39  meter
 Z    =       17325813
93                 Z    =         5301485
29
 XDOT =       2255
723219                 XDOT =         603
679648
 YDOT =      25027
926033  feet/sec       YDOT =        7635
731541  meter/sec
 ZDOT =      -1006
484748                 ZDOT =        -303
639645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4120782
66                 X    =         1256014
55
 Y    =       13208872
23  feet           Y    =         4026064
25  meter
 Z    =       17414764
01                 Z    =         5308020
07
 XDOT =     -22621
577061                 XDOT =       -6895
056688
 YDOT =       8375
195390  feet/sec       YDOT =        2552
759555  meter/sec
 ZDOT =       -994
396646                 ZDOT =        -303
092098


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   15348
61150656  
00016717  00000-0  10270-3 0  9075
2 25544  51
6440 263
6489 0008235 279
3095  80
7127 15
54734099 16114


Satellite: ISS
Catalog Number: 25544
Epoch time:      15348
61150656   =   yrday
fracday
Element set:     907
Inclination:       51
6440  deg
RA of node:       263
6489  deg
Eccentricity:     
0008235     
Arg of perigee:   279
3095  deg
Mean anomaly:      80
7127  deg
Mean motion:   15
54734099  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1611
Checksum:              323


Coasting Arc #9 (Orbit 1625)
---------------------------------------

Vector Time (GMT): 2015/349/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4366937
24                 A    =         6777491
07  meter
 Y    =       -1850787
17  meter          E    =           
0003722
 Z    =       -4844892
82                 I    =           51
27022
 XDOT =        419
015073                 Wp   =          116
47225
 YDOT =      -7268
991721  meter/sec      RA   =          257
97722  deg
 ZDOT =       2398
936745                 TA   =          177
17807
                                          MA   =          177
17597
                                          Ha   =            218
403  n
mi
                                          Hp   =            216
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14327221
91                 X    =        -4322382
19
 Y    =       -6072136
39  feet           Y    =        -1899371
68  meter
 Z    =      -15895317
66                 Z    =        -4865998
35
 XDOT =       1374
721367                 XDOT =         488
614510
 YDOT =     -23848
398035  feet/sec       YDOT =       -7263
917038  meter/sec
 ZDOT =       7870
527379                 ZDOT =        2401
140751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1912811
26                 X    =          583024
87
 Y    =      -15348767
72  feet           Y    =        -4678304
40  meter
 Z    =      -15986173
21                 Z    =        -4872585
59
 XDOT =      22168
022240                 XDOT =        6756
813179
 YDOT =      -5446
754600  feet/sec       YDOT =       -1660
170802  meter/sec
 ZDOT =       7881
433378                 ZDOT =        2402
260893


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   15349
57567413  
00016717  00000-0  10270-3 0  9085
2 25544  51
6439 258
8380 0008235 283
2273  76
7961 15
54735857 16260


Satellite: ISS
Catalog Number: 25544
Epoch time:      15349
57567413   =   yrday
fracday
Element set:     908
Inclination:       51
6439  deg
RA of node:       258
8380  deg
Eccentricity:     
0008235     
Arg of perigee:   283
2273  deg
Mean anomaly:      76
7961  deg
Mean motion:   15
54735857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1626
Checksum:              349


Coasting Arc #10 (Orbit 1641)
---------------------------------------

Vector Time (GMT): 2015/350/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4284740
22                 A    =         6781338
11  meter
 Y    =        3659550
80  meter          E    =           
0005271
 Z    =        3773200
17                 I    =           51
29063
 XDOT =      -1609
087184                 Wp   =           42
35525
 YDOT =       6213
905763  meter/sec      RA   =          252
95598  deg
 ZDOT =      -4192
250259                 TA   =           92
16266
                                          MA   =           92
10230
                                          Ha   =            218
747  n
mi
                                          Hp   =            216
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14057546
66                 X    =         4225171
10
 Y    =       12006400
27  feet           Y    =         3707132
32  meter
 Z    =       12379265
64                 Z    =         3793869
99
 XDOT =      -5279
157429                 XDOT =       -1658
088760
 YDOT =      20386
829931  feet/sec       YDOT =        6195
638137  meter/sec
 ZDOT =     -13754
101901                 ZDOT =       -4200
185516

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7395342
90                 X    =        -2254100
52
 Y    =       16878229
47  feet           Y    =         5144484
34  meter
 Z    =       12467909
07                 Z    =         3800218
69
 XDOT =     -19781
634883                 XDOT =       -6029
442312
 YDOT =       1536
286957  feet/sec       YDOT =         468
260264  meter/sec
 ZDOT =     -13789
563144                 ZDOT =       -4203
058846


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   15350
60410268  
00016717  00000-0  10270-3 0  9097
2 25544  51
6436 253
7064 0008229 287
6215  72
4039 15
54770617 16427


Satellite: ISS
Catalog Number: 25544
Epoch time:      15350
60410268   =   yrday
fracday
Element set:     909
Inclination:       51
6436  deg
RA of node:       253
7064  deg
Eccentricity:     
0008229     
Arg of perigee:   287
6215  deg
Mean anomaly:      72
4039  deg
Mean motion:   15
54770617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1642
Checksum:              308


Coasting Arc #11 (Orbit 1656)
---------------------------------------

Vector Time (GMT): 2015/351/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3950809
66                 A    =         6785334
40  meter
 Y    =       -5048915
66  meter          E    =           
0008248
 Z    =       -2205543
46                 I    =           51
31417
 XDOT =       2839
139491                 Wp   =          333
82467
 YDOT =      -4599
520878  meter/sec      RA   =          247
94708  deg
 ZDOT =       5442
893141                 TA   =            1
54535
                                          MA   =            1
54280
                                          Ha   =            218
851  n
mi
                                          Hp   =            216
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12961973
96                 X    =        -3883344
17
 Y    =      -16564683
94  feet           Y    =        -5092718
92  meter
 Z    =       -7236034
97                 Z    =        -2224571
97
 XDOT =       9314
762108                 XDOT =        2863
922047
 YDOT =     -15090
291593  feet/sec       YDOT =       -4567
633399  meter/sec
 ZDOT =      17857
260961                 ZDOT =        5456
745067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11767086
91                 X    =         3586608
09
 Y    =      -17399825
40  feet           Y    =        -5303466
78  meter
 Z    =       -7317340
15                 Z    =        -2230325
28
 XDOT =      15923
476185                 XDOT =        4853
475541
 YDOT =       3232
705131  feet/sec       YDOT =         985
328524  meter/sec
 ZDOT =      17917
983664                 ZDOT =        5461
401421


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   15351
56823951  
00016717  00000-0  10270-3 0  9102
2 25544  51
6435 248
8945 0008354 290
9588  69
0671 15
54776213 16576


Satellite: ISS
Catalog Number: 25544
Epoch time:      15351
56823951   =   yrday
fracday
Element set:     910
Inclination:       51
6435  deg
RA of node:       248
8945  deg
Eccentricity:     
0008354     
Arg of perigee:   290
9588  deg
Mean anomaly:      69
0671  deg
Mean motion:   15
54776213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1657
Checksum:              342


Coasting Arc #12 (Orbit 1672)
---------------------------------------

Vector Time (GMT): 2015/352/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3316980
69                 A    =         6787433
34  meter
 Y    =        5908234
61  meter          E    =           
0005489
 Z    =         333996
99                 I    =           51
33369
 XDOT =      -4037
395992                 Wp   =          158
43193
 YDOT =       2605
900623  meter/sec      RA   =          242
94999  deg
 ZDOT =      -5974
642117                 TA   =           17
95283
                                          MA   =           17
93346
                                          Ha   =            219
070  n
mi
                                          Hp   =            216
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10882482
57                 X    =         3249044
41
 Y    =       19383971
82  feet           Y    =         5944947
42  meter
 Z    =        1095790
63                 Z    =          349945
38
 XDOT =     -13246
049842                 XDOT =       -4037
213236
 YDOT =       8549
542726  feet/sec       YDOT =        2560
753008  meter/sec
 ZDOT =     -19601
844216                 ZDOT =       -5994
254432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14794922
24                 X    =        -4509492
30
 Y    =       16586855
27  feet           Y    =         5055673
49  meter
 Z    =        1163639
04                 Z    =          354677
18
 XDOT =     -11139
608353                 XDOT =       -3395
352626
 YDOT =      -8549
317781  feet/sec       YDOT =       -2605
832060  meter/sec
 ZDOT =     -19687
094030                 ZDOT =       -6000
626260


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   15352
59663809  
00016717  00000-0  10270-3 0  9111
2 25544  51
6433 243
7629 0008241 293
5302  66
4984 15
54761801 16738


Satellite: ISS
Catalog Number: 25544
Epoch time:      15352
59663809   =   yrday
fracday
Element set:     911
Inclination:       51
6433  deg
RA of node:       243
7629  deg
Eccentricity:     
0008241     
Arg of perigee:   293
5302  deg
Mean anomaly:      66
4984  deg
Mean motion:   15
54761801  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1673
Checksum:              323


Coasting Arc #13 (Orbit 1688)
---------------------------------------

Vector Time (GMT): 2015/353/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2356520
58                 A    =         6786227
28  meter
 Y    =       -6154771
99  meter          E    =           
0011436
 Z    =        1585638
62                 I    =           51
34525
 XDOT =       5095
649007                 Wp   =           25
54033
 YDOT =       -476
954100  meter/sec      RA   =          237
95401  deg
 ZDOT =       5716
356960                 TA   =          351
88982
                                          MA   =          351
90829
                                          Ha   =            219
198  n
mi
                                          Hp   =            216
201

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7731366
72                 X    =        -2295223
71
 Y    =      -20192821
50  feet           Y    =        -6180781
49  meter
 Z    =        5202226
46                 Z    =         1574339
77
 XDOT =      16718
008552                 XDOT =        5072
835757
 YDOT =      -1564
810038  feet/sec       YDOT =        -420
098934  meter/sec
 ZDOT =      18754
451968                 ZDOT =        5741
055231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16328982
61                 X    =         4977073
90
 Y    =      -14190933
97  feet           Y    =        -4325396
68  meter
 Z    =        5154507
88                 Z    =         1571094
00
 XDOT =       6100
002527                 XDOT =        1859
280770
 YDOT =      13876
308234  feet/sec       YDOT =        4229
498750  meter/sec
 ZDOT =      18861
300060                 ZDOT =        5748
924258


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   15353
62501815  
00016717  00000-0  10270-3 0  9125
2 25544  51
6429 238
6296 0008458 298
1131  61
9167 15
54836527 16895


Satellite: ISS
Catalog Number: 25544
Epoch time:      15353
62501815   =   yrday
fracday
Element set:     912
Inclination:       51
6429  deg
RA of node:       238
6296  deg
Eccentricity:     
0008458     
Arg of perigee:   298
1131  deg
Mean anomaly:      61
9167  deg
Mean motion:   15
54836527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1689
Checksum:              334


Coasting Arc #14 (Orbit 1703)
---------------------------------------

Vector Time (GMT): 2015/354/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1088696
67                 A    =         6782684
49  meter
 Y    =        5825046
67  meter          E    =           
0004762
 Z    =       -3301817
27                 I    =           51
35037
 XDOT =      -5866
556775                 Wp   =          326
68309
 YDOT =      -1560
171440  meter/sec      RA   =          232
95289  deg
 ZDOT =      -4679
676446                 TA   =          251
86919
                                          MA   =          251
92106
                                          Ha   =            219
406  n
mi
                                          Hp   =            216
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3571839
48                 X    =         1039517
71
 Y    =       19111045
50  feet           Y    =         5836946
36  meter
 Z    =      -10832733
82                 Z    =        -3296647
76
 XDOT =     -19247
233513                 XDOT =       -5825
942345
 YDOT =      -5118
672703  feet/sec       YDOT =       -1625
547855  meter/sec
 ZDOT =     -15353
269179                 ZDOT =       -4708
076562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16545668
00                 X    =        -5043119
60
 Y    =       10231901
83  feet           Y    =         3118683
68  meter
 Z    =      -10811441
85                 Z    =        -3295327
47
 XDOT =      -1317
158108                 XDOT =        -401
469791
 YDOT =     -18507
005510  feet/sec       YDOT =       -5640
935279  meter/sec
 ZDOT =     -15475
758732                 ZDOT =       -4717
011261


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   15354
58911290  
00016717  00000-0  10270-3 0  9134
2 25544  51
6422 233
8185 0008513 301
3178  58
7141 15
54830461 17047


Satellite: ISS
Catalog Number: 25544
Epoch time:      15354
58911290   =   yrday
fracday
Element set:     913
Inclination:       51
6422  deg
RA of node:       233
8185  deg
Eccentricity:     
0008513     
Arg of perigee:   301
3178  deg
Mean anomaly:      58
7141  deg
Mean motion:   15
54830461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1704
Checksum:              295


Coasting Arc #15 (Orbit 1719)
---------------------------------------

Vector Time (GMT): 2015/355/13:31:53
160
Vector Time (MET): N/A
Weight (LBS)     : 906038
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         435262
51                 A    =         6778373
42  meter
 Y    =       -4979691
05  meter          E    =           
0001834
 Z    =        4576518
20                 I    =           51
35580
 XDOT =       6229
178040                 Wp   =           33
11890
 YDOT =       3310
351240  meter/sec      RA   =          227
93872  deg
 ZDOT =       3010
472735                 TA   =           26
71656
                                          MA   =           26
70711
                                          Ha   =            219
576  n
mi
                                          Hp   =            215
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1428026
60                 X    =          468683
18
 Y    =      -16337569
06  feet           Y    =        -4974637
08  meter
 Z    =       15014823
48                 Z    =         4578713
49
 XDOT =      20436
935828                 XDOT =        6177
074100
 YDOT =      10860
732415  feet/sec       YDOT =        3379
718506  meter/sec
 ZDOT =       9876
879052                 ZDOT =        3040
606660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15651405
29                 X    =         4770548
33
 Y    =       -4865884
85  feet           Y    =        -1483121
70  meter
 Z    =       15025212
95                 Z    =         4579684
91
 XDOT =      -2821
383887                 XDOT =        -859
957809
 YDOT =      21814
321621  feet/sec       YDOT =        6649
005230  meter/sec
 ZDOT =      10006
561502                 ZDOT =        3049
999946


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   15355
61746670  
00016717  00000-0  10270-3 0  9148
2 25544  51
6420 228
6853 0008476 306
4003  53
6368 15
54833283 17208


Satellite: ISS
Catalog Number: 25544
Epoch time:      15355
61746670   =   yrday
fracday
Element set:     914
Inclination:       51
6420  deg
RA of node:       228
6853  deg
Eccentricity:     
0008476     
Arg of perigee:   306
4003  deg
Mean anomaly:      53
6368  deg
Mean motion:   15
54833283  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1720
Checksum:              310
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