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

 
Date: February 2nd 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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 2371)
---------------------------------------

Vector Time (GMT): 2016/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2798716
06                 A    =         6781025
59  meter
 Y    =       -4507101
28  meter          E    =           
0014870
 Z    =       -4238856
09                 I    =           51
75893
 XDOT =       6689
969153                 Wp   =           67
32117
 YDOT =       -724
508453  meter/sec      RA   =           19
13639  deg
 ZDOT =      -3651
344455                 TA   =          165
31053
                                          MA   =          165
26727
                                          Ha   =            223
005  n
mi
                                          Hp   =            211
979

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9182139
29                 X    =        -2727518
19
 Y    =      -14787077
70  feet           Y    =        -4538000
41  meter
 Z    =      -13907008
17                 Z    =        -4252278
37
 XDOT =      21948
717693                 XDOT =        6715
310064
 YDOT =      -2376
996237  feet/sec       YDOT =        -649
555200  meter/sec
 ZDOT =     -11979
476558                 ZDOT =       -3618
785001

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5399836
08                 X    =         1645870
04
 Y    =      -16498929
02  feet           Y    =        -5028873
57  meter
 Z    =      -13964287
91                 Z    =        -4256314
95
 XDOT =      14854
116220                 XDOT =        4527
534624
 YDOT =      14868
212851  feet/sec       YDOT =        4531
831277  meter/sec
 ZDOT =     -11838
134551                 ZDOT =       -3608
263411


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   16032
52271268  
00016717  00000-0  10270-3 0  9002
2 25544  51
6398  19
5719 0006696  65
2884 294
8965 15
54349381 23726


Satellite: ISS
Catalog Number: 25544
Epoch time:      16032
52271268   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:        19
5719  deg
Eccentricity:     
0006696     
Arg of perigee:    65
2884  deg
Mean anomaly:     294
8965  deg
Mean motion:   15
54349381  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2372
Checksum:              342


Coasting Arc #2 (Orbit 2387)
---------------------------------------

Vector Time (GMT): 2016/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1056626
18                 A    =         6777703
15  meter
 Y    =        4380129
11  meter          E    =           
0010607
 Z    =        5054120
79                 I    =           51
71734
 XDOT =      -7438
410302                 Wp   =           92
65971
 YDOT =       -359
046003  meter/sec      RA   =           14
14745  deg
 ZDOT =       1862
407615                 TA   =          339
31524
                                          MA   =          339
35814
                                          Ha   =            222
938  n
mi
                                          Hp   =            211
988

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3466621
32                 X    =          983017
47
 Y    =       14370502
32  feet           Y    =         4391533
52  meter
 Z    =       16581761
11                 Z    =         5059074
70
 XDOT =     -24404
233275                 XDOT =       -7442
889208
 YDOT =      -1177
972452  feet/sec       YDOT =        -442
252247  meter/sec
 ZDOT =       6110
261204                 ZDOT =        1826
263172

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8584184
44                 X    =        -2616459
42
 Y    =       12006568
16  feet           Y    =         3659601
97  meter
 Z    =       16602340
21                 Z    =         5060393
30
 XDOT =     -14364
855756                 XDOT =       -4378
408035
 YDOT =     -18520
171692  feet/sec       YDOT =       -5644
948332  meter/sec
 ZDOT =       5953
602408                 ZDOT =        1814
658014


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   16033
55138459  
00016717  00000-0  10270-3 0  9011
2 25544  51
6396  14
4419 0006606  67
8033 292
3820 15
54379012 23884


Satellite: ISS
Catalog Number: 25544
Epoch time:      16033
55138459   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:        14
4419  deg
Eccentricity:     
0006606     
Arg of perigee:    67
8033  deg
Mean anomaly:     292
3820  deg
Mean motion:   15
54379012  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2388
Checksum:              309


Coasting Arc #3 (Orbit 2402)
---------------------------------------

Vector Time (GMT): 2016/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         842569
59                 A    =         6776644
74  meter
 Y    =       -4127647
05  meter          E    =           
0021253
 Z    =       -5326316
55                 I    =           51
68255
 XDOT =       7533
609929                 Wp   =           84
93478
 YDOT =       1338
682699  meter/sec      RA   =            9
14872  deg
 ZDOT =        156
693872                 TA   =          186
54664
                                          MA   =          186
57445
                                          Ha   =            222
996  n
mi
                                          Hp   =            211
931

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2764335
93                 X    =          914535
98
 Y    =      -13542149
12  feet           Y    =        -4117822
52  meter
 Z    =      -17474791
82                 Z    =        -5322048
79
 XDOT =      24716
568009                 XDOT =        7517
319395
 YDOT =       4392
003606  feet/sec       YDOT =        1422
837431  meter/sec
 ZDOT =        514
087508                 ZDOT =         193
250254

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11957745
70                 X    =         3644720
89
 Y    =       -6979960
83  feet           Y    =        -2127492
06  meter
 Z    =      -17455433
82                 Z    =        -5320416
23
 XDOT =      12860
907674                 XDOT =        3920
004659
 YDOT =      20370
828963  feet/sec       YDOT =        6209
028668  meter/sec
 ZDOT =        672
324630                 ZDOT =         204
924547


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   16034
51575412  
00016717  00000-0  10270-3 0  9023
2 25544  51
6398   9
6317 0006680  71
5885 288
5994 15
54379800 24030


Satellite: ISS
Catalog Number: 25544
Epoch time:      16034
51575412   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:         9
6317  deg
Eccentricity:     
0006680     
Arg of perigee:    71
5885  deg
Mean anomaly:     288
5994  deg
Mean motion:   15
54379800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2403
Checksum:              327


Coasting Arc #4 (Orbit 2418)
---------------------------------------

Vector Time (GMT): 2016/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2722866
62                 A    =         6778142
13  meter
 Y    =        3730411
31  meter          E    =           
0012916
 Z    =        4952769
21                 I    =           51
65613
 XDOT =      -7017
073315                 Wp   =           65
73577
 YDOT =      -2229
214194  meter/sec      RA   =            4
14869  deg
 ZDOT =      -2169
065490                 TA   =           45
43643
                                          MA   =           45
33105
                                          Ha   =            223
022  n
mi
                                          Hp   =            211
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8933289
44                 X    =        -2788436
70
 Y    =       12238882
24  feet           Y    =         3699595
78  meter
 Z    =       16249242
81                 Z    =         4939383
14
 XDOT =     -23021
894077                 XDOT =       -6981
087940
 YDOT =      -7313
694863  feet/sec       YDOT =       -2307
482548  meter/sec
 ZDOT =      -7116
356593                 ZDOT =       -2203
064772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15107853
86                 X    =        -4604873
86
 Y    =        1804031
66  feet           Y    =          549868
85  meter
 Z    =       16190429
66                 Z    =         4934842
96
 XDOT =     -10283
058294                 XDOT =       -3134
276168
 YDOT =     -20645
050554  feet/sec       YDOT =       -6292
611409  meter/sec
 ZDOT =      -7263
317463                 ZDOT =       -2213
859163


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   16035
54440296  
00016717  00000-0  10270-3 0  9039
2 25544  51
6398   4
5012 0006616  74
5780 285
6103 15
54413483 24195


Satellite: ISS
Catalog Number: 25544
Epoch time:      16035
54440296   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:         4
5012  deg
Eccentricity:     
0006616     
Arg of perigee:    74
5780  deg
Mean anomaly:     285
6103  deg
Mean motion:   15
54413483  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2419
Checksum:              298


Coasting Arc #5 (Orbit 2433)
---------------------------------------

Vector Time (GMT): 2016/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4370883
98                 A    =         6781694
92  meter
 Y    =       -3263663
04  meter          E    =           
0013156
 Z    =       -4041114
82                 I    =           51
63623
 XDOT =       5855
359762                 Wp   =           92
60295
 YDOT =       3010
630088  meter/sec      RA   =          359
15424  deg
 ZDOT =       3912
182136                 TA   =          218
00436
                                          MA   =          218
09726
                                          Ha   =            222
989  n
mi
                                          Hp   =            211
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14340170
52                 X    =         4426683
85
 Y    =      -10707555
90  feet           Y    =        -3214472
92  meter
 Z    =      -13258250
71                 Z    =        -4019747
01
 XDOT =      19210
497906                 XDOT =        5802
255625
 YDOT =       9877
395302  feet/sec       YDOT =        3075
811679  meter/sec
 ZDOT =      12835
243227                 ZDOT =        3940
496505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17735563
00                 X    =         5405799
60
 Y    =        2864948
88  feet           Y    =          873236
42  meter
 Z    =      -13164927
99                 Z    =        -4012670
05
 XDOT =       6474
436857                 XDOT =        1973
408354
 YDOT =      19302
791908  feet/sec       YDOT =        5883
490974  meter/sec
 ZDOT =      12957
390587                 ZDOT =        3949
412651


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   16036
50875035  
00016717  00000-0  10270-3 0  9040
2 25544  51
6401 359
6913 0006647  77
6908 282
4989 15
54409112 24342


Satellite: ISS
Catalog Number: 25544
Epoch time:      16036
50875035   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       359
6913  deg
Eccentricity:     
0006647     
Arg of perigee:    77
6908  deg
Mean anomaly:     282
4989  deg
Mean motion:   15
54409112  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2434
Checksum:              326


Coasting Arc #6 (Orbit 2449)
---------------------------------------

Vector Time (GMT): 2016/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5664176
29                 A    =         6785591
99  meter
 Y    =        2655365
92  meter          E    =           
0019945
 Z    =        2608514
08                 I    =           51
61828
 XDOT =      -4179
904860                 Wp   =           95
79390
 YDOT =      -3741
385613  meter/sec      RA   =          354
16853  deg
 ZDOT =      -5235
281003                 TA   =           54
80210
                                          MA   =           54
61549
                                          Ha   =            222
962  n
mi
                                          Hp   =            211
786

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18583255
55                 X    =        -5706119
04
 Y    =        8711830
44  feet           Y    =         2591790
86  meter
 Z    =        8558117
06                 Z    =         2580897
63
 XDOT =     -13713
598621                 XDOT =       -4112
326920
 YDOT =     -12274
887181  feet/sec       YDOT =       -3787
750285  meter/sec
 ZDOT =     -17176
118777                 ZDOT =       -5255
421316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19366496
83                 X    =        -5902908
23
 Y    =       -6943814
20  feet           Y    =        -2116474
57  meter
 Z    =        8437830
84                 Z    =         2571850
84
 XDOT =      -1514
684443                 XDOT =        -461
675818
 YDOT =     -16883
620848  feet/sec       YDOT =       -5146
127634  meter/sec
 ZDOT =     -17262
673739                 ZDOT =       -5261
662956


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   16037
53737590  
00016717  00000-0  10270-3 0  9058
2 25544  51
6407 354
5603 0006640  81
2756 278
9148 15
54450270 24509


Satellite: ISS
Catalog Number: 25544
Epoch time:      16037
53737590   =   yrday
fracday
Element set:     905
Inclination:       51
6407  deg
RA of node:       354
5603  deg
Eccentricity:     
0006640     
Arg of perigee:    81
2756  deg
Mean anomaly:     278
9148  deg
Mean motion:   15
54450270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2450
Checksum:              311


Coasting Arc #7 (Orbit 2464)
---------------------------------------

Vector Time (GMT): 2016/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6426185
77                 A    =         6788010
92  meter
 Y    =       -1969358
34  meter          E    =           
0015432
 Z    =        -919952
16                 I    =           51
59506
 XDOT =       2172
879777                 Wp   =           56
67924
 YDOT =       4362
489173  meter/sec      RA   =          349
19096  deg
 ZDOT =       5919
517015                 TA   =          293
35553
                                          MA   =          293
51780
                                          Ha   =            222
912  n
mi
                                          Hp   =            211
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21083286
65                 X    =         6452198
64
 Y    =       -6461149
42  feet           Y    =        -1897351
05  meter
 Z    =       -3018215
75                 Z    =         -888672
89
 XDOT =       7128
870661                 XDOT =        2095
182095
 YDOT =      14312
628519  feet/sec       YDOT =        4386
353490  meter/sec
 ZDOT =      19420
987581                 ZDOT =        5929
883223

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19703977
37                 X    =         6005772
30
 Y    =        9940185
10  feet           Y    =         3029768
42  meter
 Z    =       -2882195
34                 Z    =         -878493
14
 XDOT =      -4126
015483                 XDOT =       -1257
609519
 YDOT =      13743
026122  feet/sec       YDOT =        4188
874362  meter/sec
 ZDOT =      19465
039464                 ZDOT =        5932
944029


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   16038
50170087  
00016717  00000-0  10270-3 0  9069
2 25544  51
6409 349
7507 0006614  85
1190 275
0717 15
54467909 24659


Satellite: ISS
Catalog Number: 25544
Epoch time:      16038
50170087   =   yrday
fracday
Element set:     906
Inclination:       51
6409  deg
RA of node:       349
7507  deg
Eccentricity:     
0006614     
Arg of perigee:    85
1190  deg
Mean anomaly:     275
0717  deg
Mean motion:   15
54467909  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2465
Checksum:              322


Coasting Arc #8 (Orbit 2480)
---------------------------------------

Vector Time (GMT): 2016/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6628616
35                 A    =         6787879
69  meter
 Y    =        1096717
78  meter          E    =           
0014713
 Z    =        -942333
17                 I    =           51
56483
 XDOT =         21
899338                 Wp   =          119
96126
 YDOT =      -4881
645682  meter/sec      RA   =          344
21487  deg
 ZDOT =      -5911
861060                 TA   =           70
25231
                                          MA   =           70
09369
                                          Ha   =            222
809  n
mi
                                          Hp   =            211
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21747428
98                 X    =        -6635810
14
 Y    =        3598155
46  feet           Y    =         1022551
93  meter
 Z    =       -3091644
25                 Z    =         -974550
03
 XDOT =         71
848223                 XDOT =         105
202019
 YDOT =     -16015
897908  feet/sec       YDOT =       -4880
935312  meter/sec
 ZDOT =     -19395
869620                 ZDOT =       -5911
552111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18384556
53                 X    =        -5603612
83
 Y    =      -12125215
77  feet           Y    =        -3695765
77  meter
 Z    =       -3231544
20                 Z    =         -984974
67
 XDOT =      10144
724402                 XDOT =        3092
111998
 YDOT =     -10276
939453  feet/sec       YDOT =       -3132
411145  meter/sec
 ZDOT =     -19393
537901                 ZDOT =       -5911
150352


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   16039
53030266  
00016717  00000-0  10270-3 0  9078
2 25544  51
6421 344
6197 0006569  88
4515 271
7391 15
54484199 24817


Satellite: ISS
Catalog Number: 25544
Epoch time:      16039
53030266   =   yrday
fracday
Element set:     907
Inclination:       51
6421  deg
RA of node:       344
6197  deg
Eccentricity:     
0006569     
Arg of perigee:    88
4515  deg
Mean anomaly:     271
7391  deg
Mean motion:   15
54484199  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2481
Checksum:              329


Coasting Arc #9 (Orbit 2496)
---------------------------------------

Vector Time (GMT): 2016/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6241785
58                 A    =         6785201
34  meter
 Y    =        -126147
89  meter          E    =           
0019967
 Z    =        2636431
35                 I    =           51
52560
 XDOT =      -2107
667347                 Wp   =           82
17757
 YDOT =       5226
372030  meter/sec      RA   =          339
23299  deg
 ZDOT =       5208
841446                 TA   =          307
61882
                                          MA   =          307
79989
                                          Ha   =            222
741  n
mi
                                          Hp   =            211
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20478299
16                 X    =         6229925
97
 Y    =        -413871
02  feet           Y    =          -56414
23  meter
 Z    =        8649709
17                 Z    =         2666722
84
 XDOT =      -6914
919117                 XDOT =       -2191
254972
 YDOT =      17146
889861  feet/sec       YDOT =        5202
335698  meter/sec
 ZDOT =      17089
374823                 ZDOT =        5198
399790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15494344
59                 X    =         4722676
23
 Y    =       13310439
92  feet           Y    =         4057022
09  meter
 Z    =        8781057
40                 Z    =         2676466
30
 XDOT =     -15699
236832                 XDOT =       -4785
127386
 YDOT =       6965
141584  feet/sec       YDOT =        2122
975155  meter/sec
 ZDOT =      17043
052866                 ZDOT =        5194
722514


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   16040
55889203  
00016717  00000-0  10270-3 0  9086
2 25544  51
6421 339
4896 0006554  92
3547 267
8356 15
54504521 24974


Satellite: ISS
Catalog Number: 25544
Epoch time:      16040
55889203   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:       339
4896  deg
Eccentricity:     
0006554     
Arg of perigee:    92
3547  deg
Mean anomaly:     267
8356  deg
Mean motion:   15
54504521  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2497
Checksum:              334


Coasting Arc #10 (Orbit 2511)
---------------------------------------

Vector Time (GMT): 2016/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5335171
81                 A    =         6781016
47  meter
 Y    =       -1023510
78  meter          E    =           
0013684
 Z    =       -4071534
66                 I    =           51
48284
 XDOT =       3950
961124                 Wp   =           81
95059
 YDOT =      -5310
529081  meter/sec      RA   =          334
23788  deg
 ZDOT =      -3851
452101                 TA   =          148
09104
                                          MA   =          148
00808
                                          Ha   =            222
738  n
mi
                                          Hp   =            211
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17503844
53                 X    =        -5303552
81
 Y    =       -3357975
00  feet           Y    =        -1082995
77  meter
 Z    =      -13358053
33                 Z    =        -4097374
13
 XDOT =      12962
470878                 XDOT =        4028
759421
 YDOT =     -17422
995671  feet/sec       YDOT =       -5265
912153  meter/sec
 ZDOT =     -12635
997707                 ZDOT =       -3832
070319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10981060
27                 X    =        -3347027
17
 Y    =      -13931161
18  feet           Y    =        -4246217
93  meter
 Z    =      -13469863
46                 Z    =        -4105614
38
 XDOT =      20246
201205                 XDOT =        6171
042127
 YDOT =      -3852
578921  feet/sec       YDOT =       -1174
266055  meter/sec
 ZDOT =     -12550
914008                 ZDOT =       -3825
518590


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   16041
52318342  
00016717  00000-0  10270-3 0  9096
2 25544  51
6426 334
6793 0006570  95
2754 264
9149 15
54533311 25127


Satellite: ISS
Catalog Number: 25544
Epoch time:      16041
52318342   =   yrday
fracday
Element set:     909
Inclination:       51
6426  deg
RA of node:       334
6793  deg
Eccentricity:     
0006570     
Arg of perigee:    95
2754  deg
Mean anomaly:     264
9149  deg
Mean motion:   15
54533311  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2512
Checksum:              307


Coasting Arc #11 (Orbit 2527)
---------------------------------------

Vector Time (GMT): 2016/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4026479
06                 A    =         6777416
44  meter
 Y    =        2215598
50  meter          E    =           
0012134
 Z    =        4972706
72                 I    =           51
44247
 XDOT =      -5356
766216                 Wp   =          110
90720
 YDOT =       5098
262413  meter/sec      RA   =          329
22987  deg
 ZDOT =       2057
604772                 TA   =          319
00020
                                          MA   =          319
09136
                                          Ha   =            222
528  n
mi
                                          Hp   =            211
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13210233
15                 X    =         3977249
60
 Y    =        7269023
96  feet           Y    =         2260350
48  meter
 Z    =       16314654
58                 Z    =         4992146
21
 XDOT =     -17574
692309                 XDOT =       -5423
372903
 YDOT =      16726
582719  feet/sec       YDOT =        5037
987277  meter/sec
 ZDOT =       6750
671825                 ZDOT =        2031
421144

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5401952
26                 X    =         1646515
05
 Y    =       13979474
62  feet           Y    =         4260943
86  meter
 Z    =       16398479
33                 Z    =         4998256
50
 XDOT =     -23224
618797                 XDOT =       -7078
863809
 YDOT =       1158
154506  feet/sec       YDOT =         353
005494  meter/sec
 ZDOT =       6636
159052                 ZDOT =        2022
701279


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   16042
55174791  
00016717  00000-0  10270-3 0  9100
2 25544  51
6423 329
5492 0006435 100
1758 260
0121 15
54569792 25289


Satellite: ISS
Catalog Number: 25544
Epoch time:      16042
55174791   =   yrday
fracday
Element set:     910
Inclination:       51
6423  deg
RA of node:       329
5492  deg
Eccentricity:     
0006435     
Arg of perigee:   100
1758  deg
Mean anomaly:     260
0121  deg
Mean motion:   15
54569792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2528
Checksum:              303


Coasting Arc #12 (Orbit 2542)
---------------------------------------

Vector Time (GMT): 2016/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2465970
84                 A    =         6776107
21  meter
 Y    =       -3443538
44  meter          E    =           
0021277
 Z    =       -5307718
06                 I    =           51
41105
 XDOT =       6213
411690                 Wp   =           93
71066
 YDOT =      -4468
615364  meter/sec      RA   =          324
21055  deg
 ZDOT =         11
079090                 TA   =          176
40311
                                          MA   =          176
38779
                                          Ha   =            222
676  n
mi
                                          Hp   =            211
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8090455
50                 X    =        -2401498
81
 Y    =      -11297698
28  feet           Y    =        -3470754
58  meter
 Z    =      -17413773
15                 Z    =        -5319540
04
 XDOT =      20385
208956                 XDOT =        6262
865243
 YDOT =     -14660
811561  feet/sec       YDOT =       -4398
856361  meter/sec
 ZDOT =         36
348721                 ZDOT =          41
382406

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         878192
23                 X    =          267672
99
 Y    =      -13804301
81  feet           Y    =        -4207551
19  meter
 Z    =      -17464334
57                 Z    =        -5323129
18
 XDOT =      24064
770594                 XDOT =        7334
942077
 YDOT =       1312
237128  feet/sec       YDOT =         399
969877  meter/sec
 ZDOT =        168
580486                 ZDOT =          51
383332


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   16043
51601831  
00016717  00000-0  10270-3 0  9118
2 25544  51
6426 324
7384 0006501 102
6326 257
5555 15
54559800 25439


Satellite: ISS
Catalog Number: 25544
Epoch time:      16043
51601831   =   yrday
fracday
Element set:     911
Inclination:       51
6426  deg
RA of node:       324
7384  deg
Eccentricity:     
0006501     
Arg of perigee:   102
6326  deg
Mean anomaly:     257
5555  deg
Mean motion:   15
54559800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2543
Checksum:              291


Coasting Arc #13 (Orbit 2558)
---------------------------------------

Vector Time (GMT): 2016/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         808925
14                 A    =         6777482
85  meter
 Y    =        4535908
90  meter          E    =           
0011495
 Z    =        4961136
20                 I    =           51
39006
 XDOT =      -6535
580015                 Wp   =           81
58061
 YDOT =       3447
810024  meter/sec      RA   =          319
19033  deg
 ZDOT =      -2080
863893                 TA   =           28
74820
                                          MA   =           28
68489
                                          Ha   =            222
547  n
mi
                                          Hp   =            211
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2653953
87                 X    =          734044
57
 Y    =       14881590
89  feet           Y    =         4544536
58  meter
 Z    =       16276693
56                 Z    =         4964883
45
 XDOT =     -21442
191649                 XDOT =       -6563
540713
 YDOT =      11311
712678  feet/sec       YDOT =        3374
568319  meter/sec
 ZDOT =      -6826
981276                 ZDOT =       -2112
679959

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7126257
11                 X    =        -2172083
17
 Y    =       13312466
47  feet           Y    =         4057639
78  meter
 Z    =       16292043
10                 Z    =         4965814
74
 XDOT =     -22863
649926                 XDOT =       -6968
840498
 YDOT =      -3691
282389  feet/sec       YDOT =       -1125
102872  meter/sec
 ZDOT =      -6965
557574                 ZDOT =       -2123
101948


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   16044
54455988  
00016717  00000-0  10270-3 0  9123
2 25544  51
6421 319
6077 0006420 106
0888 254
0972 15
54593194 25593


Satellite: ISS
Catalog Number: 25544
Epoch time:      16044
54455988   =   yrday
fracday
Element set:     912
Inclination:       51
6421  deg
RA of node:       319
6077  deg
Eccentricity:     
0006420     
Arg of perigee:   106
0888  deg
Mean anomaly:     254
0972  deg
Mean motion:   15
54593194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2559
Checksum:              330


Coasting Arc #14 (Orbit 2573)
---------------------------------------

Vector Time (GMT): 2016/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         756652
05                 A    =         6781081
38  meter
 Y    =       -5406540
52  meter          E    =           
0013513
 Z    =       -4036724
52                 I    =           51
37904
 XDOT =       6284
083306                 Wp   =          108
45805
 YDOT =      -2015
350765  meter/sec      RA   =          314
17520  deg
 ZDOT =       3883
663917                 TA   =          201
99132
                                          MA   =          202
04936
                                          Ha   =            222
565  n
mi
                                          Hp   =            211
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2482454
24                 X    =          836661
57
 Y    =      -17737993
82  feet           Y    =        -5397632
06  meter
 Z    =      -13243846
85                 Z    =        -4032854
22
 XDOT =      20617
071213                 XDOT =        6287
287430
 YDOT =      -6612
043193  feet/sec       YDOT =       -1945
059790  meter/sec
 ZDOT =      12741
679518                 ZDOT =        3914
198041

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12703005
48                 X    =         3871876
07
 Y    =      -12645341
99  feet           Y    =        -3854300
24  meter
 Z    =      -13226014
56                 Z    =        -4031289
24
 XDOT =      19469
194344                 XDOT =        5934
210436
 YDOT =       6114
794414  feet/sec       YDOT =        1863
789337  meter/sec
 ZDOT =      12874
411267                 ZDOT =        3924
120554


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   16045
50880741  
00016717  00000-0  10270-3 0  9130
2 25544  51
6426 314
7967 0006454 109
6804 250
5046 15
54599406 25748


Satellite: ISS
Catalog Number: 25544
Epoch time:      16045
50880741   =   yrday
fracday
Element set:     913
Inclination:       51
6426  deg
RA of node:       314
7967  deg
Eccentricity:     
0006454     
Arg of perigee:   109
6804  deg
Mean anomaly:     250
5046  deg
Mean motion:   15
54599406  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2574
Checksum:              322


Coasting Arc #15 (Orbit 2589)
---------------------------------------

Vector Time (GMT): 2016/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2151878
42                 A    =         6785219
98  meter
 Y    =        5889358
50  meter          E    =           
0020089
 Z    =        2567395
76                 I    =           51
37090
 XDOT =      -5603
610944                 Wp   =          106
72633
 YDOT =        248
994424  meter/sec      RA   =          309
17099  deg
 ZDOT =      -5239
512355                 TA   =           44
25761
                                          MA   =           44
09713
                                          Ha   =            222
568  n
mi
                                          Hp   =            211
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7059968
57                 X    =        -2230045
92
 Y    =       19322042
32  feet           Y    =         5864857
85  meter
 Z    =        8423214
43                 Z    =         2556752
40
 XDOT =     -18384
550342                 XDOT =       -5580
527767
 YDOT =        816
910841  feet/sec       YDOT =         186
459907  meter/sec
 ZDOT =     -17190
001165                 ZDOT =       -5266
676950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17094794
67                 X    =        -5210493
42
 Y    =       11478094
32  feet           Y    =         3498523
15  meter
 Z    =        8375939
54                 Z    =         2552986
37
 XDOT =     -14441
979819                 XDOT =       -4401
915449
 YDOT =      -8810
703316  feet/sec       YDOT =       -2685
502371  meter/sec
 ZDOT =     -17307
781141                 ZDOT =       -5275
411692


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   16046
53732692  
00016717  00000-0  10270-3 0  9146
2 25544  51
6424 309
6653 0006494 113
9157 246
2677 15
54591885 25907


Satellite: ISS
Catalog Number: 25544
Epoch time:      16046
53732692   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       309
6653  deg
Eccentricity:     
0006494     
Arg of perigee:   113
9157  deg
Mean anomaly:     246
2677  deg
Mean motion:   15
54591885  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2590
Checksum:              337
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