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

 
Date: October 3rd 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) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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


284/02:47:17 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 212 5

286/10:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 212 2

287/18:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 212 2

288/06:36:41 000 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 212 2

Coasting Arc #1 (Orbit 2182)
---------------------------------------

Vector Time (GMT): 2016/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -591198
10                 A    =         6782045
88  meter
 Y    =        5279295
36  meter          E    =           
0014199
 Z    =       -4231591
36                 I    =           51
32153
 XDOT =      -5759
400906                 Wp   =           52
09542
 YDOT =      -3531
324806  meter/sec      RA   =          236
77071  deg
 ZDOT =      -3600
739312                 TA   =          180
85444
                                          MA   =          180
85687
                                          Ha   =            223
193  n
mi
                                          Hp   =            213
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1939626
31                 X    =         -629632
99
 Y    =       17320522
83  feet           Y    =         5272468
75  meter
 Z    =      -13883173
76                 Z    =        -4234557
32
 XDOT =     -18895
672264                 XDOT =       -5701
993540
 YDOT =     -11585
711306  feet/sec       YDOT =       -3595
409759  meter/sec
 ZDOT =     -11813
449185                 ZDOT =       -3628
577628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1721141
11                 X    =         -524603
81
 Y    =      -17332548
78  feet           Y    =        -5282960
87  meter
 Z    =      -13896963
73                 Z    =        -4235794
54
 XDOT =      19522
358585                 XDOT =        5950
414897
 YDOT =       7630
970372  feet/sec       YDOT =        2325
919770  meter/sec
 ZDOT =     -11934
479859                 ZDOT =       -3637
629461


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   16277
52277146  
00016717  00000-0  10270-3 0  9004
2 25544  51
6402 237
6460 0006993  30
8589 329
2973 15
54025236 21830


Satellite: ISS
Catalog Number: 25544
Epoch time:      16277
52277146   =   yrday
fracday
Element set:     900
Inclination:       51
6402  deg
RA of node:       237
6460  deg
Eccentricity:     
0006993     
Arg of perigee:    30
8589  deg
Mean anomaly:     329
2973  deg
Mean motion:   15
54025236  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2183
Checksum:              318


Coasting Arc #2 (Orbit 2198)
---------------------------------------

Vector Time (GMT): 2016/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1794432
15                 A    =         6778795
75  meter
 Y    =       -4194670
22  meter          E    =           
0008894
 Z    =        5005520
55                 I    =           51
33052
 XDOT =       5711
336407                 Wp   =           74
23613
 YDOT =       4749
126396  meter/sec      RA   =          231
75763  deg
 ZDOT =       1931
858753                 TA   =          356
95383
                                          MA   =          356
95924
                                          Ha   =            223
019  n
mi
                                          Hp   =            213
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5887244
60                 X    =         1816889
55
 Y    =      -13762041
42  feet           Y    =        -4174477
55  meter
 Z    =       16422311
51                 Z    =         5014292
62
 XDOT =      18737
980338                 XDOT =        5648
421675
 YDOT =      15581
123345  feet/sec       YDOT =        4812
642830  meter/sec
 ZDOT =       6338
119270                 ZDOT =        1959
450149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2600660
41                 X    =         -792681
29
 Y    =       14697221
36  feet           Y    =         4479713
07  meter
 Z    =       16461287
86                 Z    =         5017400
54
 XDOT =     -20603
179199                 XDOT =       -6279
849020
 YDOT =     -10880
526486  feet/sec       YDOT =       -3316
384473  meter/sec
 ZDOT =       6457
891538                 ZDOT =        1968
365341


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   16278
55166946  
00016717  00000-0  10270-3 0  9014
2 25544  51
6411 232
5187 0006809  33
2940 326
8640 15
54069005 21997


Satellite: ISS
Catalog Number: 25544
Epoch time:      16278
55166946   =   yrday
fracday
Element set:     901
Inclination:       51
6411  deg
RA of node:       232
5187  deg
Eccentricity:     
0006809     
Arg of perigee:    33
2940  deg
Mean anomaly:     326
8640  deg
Mean motion:   15
54069005  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2199
Checksum:              315


Coasting Arc #3 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2016/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3041729
58                 A    =         6777614
62  meter
 Y    =        2956357
11  meter          E    =           
0019906
 Z    =       -5302825
57                 I    =           51
34739
 XDOT =      -5278
567297                 Wp   =           73
57312
 YDOT =      -5542
569080  meter/sec      RA   =          226
73799  deg
 ZDOT =        -56
861424                 TA   =          195
85063
                                          MA   =          195
91302
                                          Ha   =            223
249  n
mi
                                          Hp   =            212
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9979427
77                 X    =        -3048802
94
 Y    =        9699334
37  feet           Y    =         2922302
38  meter
 Z    =      -17397721
69                 Z    =        -5317619
27
 XDOT =     -17318
134176                 XDOT =       -5215
920347
 YDOT =     -18184
281760  feet/sec       YDOT =       -5601
247287  meter/sec
 ZDOT =       -186
553228                 ZDOT =         -82
351140

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7281219
21                 X    =         2219315
62
 Y    =      -11763543
21  feet           Y    =        -3585527
97  meter
 Z    =      -17462808
59                 Z    =        -5322664
06
 XDOT =      20281
892005                 XDOT =        6181
920683
 YDOT =      13020
628005  feet/sec       YDOT =        3968
687416  meter/sec
 ZDOT =       -297
034672                 ZDOT =         -90
536168


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   16279
51625459  
00016717  00000-0  10270-3 0  9021
2 25544  51
6415 227
7105 0006954  37
1395 323
0237 15
54042331 22147


Satellite: ISS
Catalog Number: 25544
Epoch time:      16279
51625459   =   yrday
fracday
Element set:     902
Inclination:       51
6415  deg
RA of node:       227
7105  deg
Eccentricity:     
0006954     
Arg of perigee:    37
1395  deg
Mean anomaly:     323
0237  deg
Mean motion:   15
54042331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2214
Checksum:              292


Coasting Arc #4 (Orbit 2229)
---------------------------------------

Vector Time (GMT): 2016/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4235259
01                 A    =         6778645
15  meter
 Y    =       -1613926
97  meter          E    =           
0012384
 Z    =        5035017
49                 I    =           51
37356
 XDOT =       4471
612753                 Wp   =           47
62761
 YDOT =       5957
470705  meter/sec      RA   =          221
72097  deg
 ZDOT =      -1840
633898                 TA   =           60
31611
                                          MA   =           60
19288
                                          Ha   =            223
197  n
mi
                                          Hp   =            212
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13895206
73                 X    =         4228533
20
 Y    =       -5295035
98  feet           Y    =        -1566602
63  meter
 Z    =       16519086
27                 Z    =         5055575
48
 XDOT =      14670
645516                 XDOT =        4413
603620
 YDOT =      19545
507563  feet/sec       YDOT =        6007
150772  meter/sec
 ZDOT =      -6038
825126                 ZDOT =       -1819
052956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11989789
68                 X    =        -3654487
89
 Y    =        8624119
04  feet           Y    =         2628631
48  meter
 Z    =       16609151
13                 Z    =         5062469
26
 XDOT =     -18565
108712                 XDOT =       -5658
645135
 YDOT =     -14290
263922  feet/sec       YDOT =       -4355
672444  meter/sec
 ZDOT =      -5945
469314                 ZDOT =       -1812
179047


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   16280
54513569  
00016717  00000-0  10270-3 0  9035
2 25544  51
6411 222
5831 0007033  41
1186 319
0496 15
54057571 22306


Satellite: ISS
Catalog Number: 25544
Epoch time:      16280
54513569   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:       222
5831  deg
Eccentricity:     
0007033     
Arg of perigee:    41
1186  deg
Mean anomaly:     319
0496  deg
Mean motion:   15
54057571  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2230
Checksum:              285


Coasting Arc #5 (Orbit 2244)
---------------------------------------

Vector Time (GMT): 2016/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5251108
14                 A    =         6781605
07  meter
 Y    =         351970
68  meter          E    =           
0012993
 Z    =       -4286875
32                 I    =           51
40816
 XDOT =      -3273
345988                 Wp   =           81
56273
 YDOT =      -5956
593250  meter/sec      RA   =          216
71106  deg
 ZDOT =       3531
609618                 TA   =          224
53527
                                          MA   =          224
63977
                                          Ha   =            223
266  n
mi
                                          Hp   =            212
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17228045
07                 X    =        -5233829
57
 Y    =        1154759
44  feet           Y    =          293345
55  meter
 Z    =      -14064551
57                 Z    =        -4312342
34
 XDOT =     -10739
324107                 XDOT =       -3223
649870
 YDOT =     -19542
628774  feet/sec       YDOT =       -5992
919864  meter/sec
 ZDOT =      11586
645729                 ZDOT =        3515
829435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16184206
47                 X    =         4932946
13
 Y    =       -5750351
75  feet           Y    =        -1752707
21  meter
 Z    =      -14175878
56                 Z    =        -4320807
79
 XDOT =      15281
942733                 XDOT =        4657
936145
 YDOT =      14703
451605  feet/sec       YDOT =        4481
612049  meter/sec
 ZDOT =      11518
619365                 ZDOT =        3510
875182


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   16281
50970331  
00016717  00000-0  10270-3 0  9047
2 25544  51
6410 217
7757 0006932  44
2131 315
9574 15
54066453 22456


Satellite: ISS
Catalog Number: 25544
Epoch time:      16281
50970331   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       217
7757  deg
Eccentricity:     
0006932     
Arg of perigee:    44
2131  deg
Mean anomaly:     315
9574  deg
Mean motion:   15
54066453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2245
Checksum:              297


Coasting Arc #6 (Orbit 2260)
---------------------------------------

Vector Time (GMT): 2016/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5994655
59                 A    =         6785355
70  meter
 Y    =         843941
48  meter          E    =           
0018418
 Z    =        3053204
11                 I    =           51
44823
 XDOT =       1714
290859                 Wp   =           79
45581
 YDOT =       5648
048135  meter/sec      RA   =          211
71188  deg
 ZDOT =      -4898
523315                 TA   =           65
38720
                                          MA   =           65
19544
                                          Ha   =            223
259  n
mi
                                          Hp   =            212
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19667505
21                 X    =         5969941
53
 Y    =        2768836
89  feet           Y    =          910839
78  meter
 Z    =       10017073
86                 Z    =         3082264
94
 XDOT =       5624
313843                 XDOT =        1674
800769
 YDOT =      18530
341649  feet/sec       YDOT =        5666
997334  meter/sec
 ZDOT =     -16071
270720                 ZDOT =       -4890
291930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19571638
50                 X    =        -5965435
41
 Y    =        2978348
31  feet           Y    =          907800
56  meter
 Z    =       10143933
93                 Z    =         3091871
06
 XDOT =     -10592
568939                 XDOT =       -3228
615013
 YDOT =     -14675
071060  feet/sec       YDOT =       -4472
961659  meter/sec
 ZDOT =     -16036
169844                 ZDOT =       -4887
824569


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   16282
53856425  
00016717  00000-0  10270-3 0  9059
2 25544  51
6417 212
6471 0006979  47
5332 312
6409 15
54102124 22615


Satellite: ISS
Catalog Number: 25544
Epoch time:      16282
53856425   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:       212
6471  deg
Eccentricity:     
0006979     
Arg of perigee:    47
5332  deg
Mean anomaly:     312
6409  deg
Mean motion:   15
54102124  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2261
Checksum:              298


Coasting Arc #7 (Orbit 2275)
---------------------------------------

Vector Time (GMT): 2016/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6349483
85                 A    =         6788330
06  meter
 Y    =       -1815718
14  meter          E    =           
0014931
 Z    =       -1550054
78                 I    =           51
48537
 XDOT =         62
977845                 Wp   =           44
43475
 YDOT =      -5083
521241  meter/sec      RA   =          206
72457  deg
 ZDOT =       5740
776857                 TA   =          298
58526
                                          MA   =          298
73542
                                          Ha   =            223
323  n
mi
                                          Hp   =            212
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20831639
92                 X    =        -6321178
54
 Y    =       -5957080
52  feet           Y    =        -1886564
18  meter
 Z    =       -5085481
57                 Z    =        -1580830
43
 XDOT =        206
620227                 XDOT =          91
931873
 YDOT =     -16678
219296  feet/sec       YDOT =       -5082
654669  meter/sec
 ZDOT =      18834
569741                 ZDOT =        5741
153489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21625228
01                 X    =         6591369
50
 Y    =        -640592
08  feet           Y    =         -195252
47  meter
 Z    =       -5219703
86                 Z    =        -1590965
74
 XDOT =       4937
495541                 XDOT =        1504
948641
 YDOT =      14337
588160  feet/sec       YDOT =        4370
096871  meter/sec
 ZDOT =      18836
992335                 ZDOT =        5741
515264


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   16283
50311060  
00016717  00000-0  10270-3 0  9069
2 25544  51
6410 207
8397 0007024  51
1484 309
0295 15
54101433 22763


Satellite: ISS
Catalog Number: 25544
Epoch time:      16283
50311060   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:       207
8397  deg
Eccentricity:     
0007024     
Arg of perigee:    51
1484  deg
Mean anomaly:     309
0295  deg
Mean motion:   15
54101433  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2276
Checksum:              276


Coasting Arc #8 (Orbit 2285)
---------------------------------------

Vector Time (GMT): 2016/284/02:47:17
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5676767
60                 A    =         6788752
91  meter
 Y    =        3525232
05  meter          E    =           
0011884
 Z    =       -1193969
45                 I    =           51
50516
 XDOT =      -3435
763673                 Wp   =          107
44961
 YDOT =       3570
197860  meter/sec      RA   =          203
67062  deg
 ZDOT =      -5845
946758                 TA   =           85
53762
                                          MA   =           85
40186
                                          Ha   =            223
334  n
mi
                                          Hp   =            212
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18624565
61                 X    =         5642725
49
 Y    =       11565721
96  feet           Y    =         3588523
04  meter
 Z    =       -3917222
61                 Z    =        -1166475
84
 XDOT =     -11272
190528                 XDOT =       -3447
033821
 YDOT =      11713
247572  feet/sec       YDOT =        3531
713374  meter/sec
 ZDOT =     -19179
615348                 ZDOT =       -5862
664647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19320938
53                 X    =         5889022
06
 Y    =      -10405028
48  feet           Y    =        -3171452
68  meter
 Z    =       -3797593
73                 Z    =        -1157506
57
 XDOT =       3839
328507                 XDOT =        1170
227329
 YDOT =      14092
419551  feet/sec       YDOT =        4295
369479  meter/sec
 ZDOT =     -19253
226539                 ZDOT =       -5868
383449


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   16284
14613523  
00016717  00000-0  10270-3 0  9070
2 25544  51
6414 204
6332 0006814  55
7661 304
4137 15
54129102 22862


Satellite: ISS
Catalog Number: 25544
Epoch time:      16284
14613523   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:       204
6332  deg
Eccentricity:     
0006814     
Arg of perigee:    55
7661  deg
Mean anomaly:     304
4137  deg
Mean motion:   15
54129102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2286
Checksum:              286


Coasting Arc #9 (Orbit 2301)
---------------------------------------

Vector Time (GMT): 2016/285/02:47:17
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4781719
85                 A    =         6786173
06  meter
 Y    =       -3930337
10  meter          E    =           
0020031
 Z    =        2757057
71                 I    =           51
52636
 XDOT =       5093
215620                 Wp   =           72
74385
 YDOT =      -2580
605705  meter/sec      RA   =          198
68794  deg
 ZDOT =       5129
688502                 TA   =          318
56976
                                          MA   =          318
72148
                                          Ha   =            223
391  n
mi
                                          Hp   =            212
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15688057
24                 X    =        -4750807
14
 Y    =      -12894806
75  feet           Y    =        -3983636
40  meter
 Z    =        9045464
93                 Z    =         2733904
57
 XDOT =      16710
024999                 XDOT =        5096
776049
 YDOT =      -8466
554149  feet/sec       YDOT =       -2523
629574  meter/sec
 ZDOT =      16829
686686                 ZDOT =        5154
439151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18898876
45                 X    =        -5760377
54
 Y    =        7552066
38  feet           Y    =         2301869
83  meter
 Z    =        8944852
10                 Z    =         2726390
92
 XDOT =       1164
461230                 XDOT =         354
927783
 YDOT =     -17246
164954  feet/sec       YDOT =       -5256
631078  meter/sec
 ZDOT =      16938
265866                 ZDOT =        5162
783436


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   16285
17496648  
00016717  00000-0  10270-3 0  9082
2 25544  51
6414 199
5046 0006801  59
5409 300
6415 15
54130682 23025


Satellite: ISS
Catalog Number: 25544
Epoch time:      16285
17496648   =   yrday
fracday
Element set:     908
Inclination:       51
6414  deg
RA of node:       199
5046  deg
Eccentricity:     
0006801     
Arg of perigee:    59
5409  deg
Mean anomaly:     300
6415  deg
Mean motion:   15
54130682  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2302
Checksum:              311


Coasting Arc #10 (Orbit 2316)
---------------------------------------

Vector Time (GMT): 2016/286/02:47:17
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3457285
75                 A    =         6782278
36  meter
 Y    =        4181464
18  meter          E    =           
0014033
 Z    =       -4084721
99                 I    =           51
54546
 XDOT =      -6433
268286                 Wp   =           67
78329
 YDOT =       1571
892793  meter/sec      RA   =          193
69782  deg
 ZDOT =      -3841
370444                 TA   =          162
39561
                                          MA   =          162
34693
                                          Ha   =            223
370  n
mi
                                          Hp   =            212
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11342801
01                 X    =         3430112
58
 Y    =       13718714
51  feet           Y    =         4219973
50  meter
 Z    =      -13401318
85                 Z    =        -4067993
67
 XDOT =     -21106
523247                 XDOT =       -6431
707577
 YDOT =       5157
128585  feet/sec       YDOT =        1499
959980  meter/sec
 ZDOT =     -12602
921404                 ZDOT =       -3872
618284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17472483
48                 X    =         5325612
96
 Y    =       -3675949
46  feet           Y    =        -1120429
40  meter
 Z    =      -13328815
63                 Z    =        -4062623
00
 XDOT =      -5556
614203                 XDOT =       -1693
656009
 YDOT =      19717
420879  feet/sec       YDOT =        6009
869884  meter/sec
 ZDOT =     -12739
762253                 ZDOT =       -3883
079535


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   16286
13948439  
00016717  00000-0  10270-3 0  9090
2 25544  51
6424 194
6963 0006870  62
9434 297
2419 15
54152755 23178


Satellite: ISS
Catalog Number: 25544
Epoch time:      16286
13948439   =   yrday
fracday
Element set:     909
Inclination:       51
6424  deg
RA of node:       194
6963  deg
Eccentricity:     
0006870     
Arg of perigee:    62
9434  deg
Mean anomaly:     297
2419  deg
Mean motion:   15
54152755  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2317
Checksum:              342


Coasting Arc #11 (Orbit 2321)
---------------------------------------

Vector Time (GMT): 2016/286/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907704
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6002994
03                 A    =         6785427
63  meter
 Y    =        1127860
94  meter          E    =           
0011463
 Z    =       -2958071
25                 I    =           51
56640
 XDOT =      -3343
551583                 Wp   =           65
06385
 YDOT =      -4757
048496  meter/sec      RA   =          191
95993  deg
 ZDOT =       4991
408813                 TA   =          261
12685
                                          MA   =          261
25665
                                          Ha   =            223
320  n
mi
                                          Hp   =            212
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19694862
29                 X    =        -6000790
74
 Y    =        3700331
18  feet           Y    =         1060743
42  meter
 Z    =       -9704958
17                 Z    =        -2987227
32
 XDOT =     -10969
657423                 XDOT =       -3314
354880
 YDOT =     -15607
114487  feet/sec       YDOT =       -4794
274517  meter/sec
 ZDOT =      16376
013167                 ZDOT =        4975
237995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19295084
49                 X    =         5881141
75
 Y    =       -5175530
01  feet           Y    =        -1577501
55  meter
 Z    =       -9832592
15                 Z    =        -2996974
09
 XDOT =      11848
049803                 XDOT =        3611
285580
 YDOT =      13315
101645  feet/sec       YDOT =        4058
442981  meter/sec
 ZDOT =      16306
029395                 ZDOT =        4970
077760


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   16286
46098856  
00016717  00000-0  10270-3 0  9107
2 25544  51
6418 193
0950 0006956  61
5772 298
6080 15
54159193 23223


Satellite: ISS
Catalog Number: 25544
Epoch time:      16286
46098856   =   yrday
fracday
Element set:     910
Inclination:       51
6418  deg
RA of node:       193
0950  deg
Eccentricity:     
0006956     
Arg of perigee:    61
5772  deg
Mean anomaly:     298
6080  deg
Mean motion:   15
54159193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2322
Checksum:              334


Coasting Arc #12 (Orbit 2337)
---------------------------------------

Vector Time (GMT): 2016/287/10:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907704
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6640923
32                 A    =         6788384
55  meter
 Y    =        -266493
26  meter          E    =           
0018780
 Z    =        1352601
60                 I    =           51
60866
 XDOT =       1389
546052                 Wp   =          102
61361
 YDOT =       4808
703506  meter/sec      RA   =          186
98160  deg
 ZDOT =      -5810
793920                 TA   =           62
64612
                                          MA   =           62
45511
                                          Ha   =            223
365  n
mi
                                          Hp   =            212
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21787806
17                 X    =         6636839
32
 Y    =        -874321
73  feet           Y    =         -192252
66  meter
 Z    =        4437669
29                 Z    =         1384852
01
 XDOT =       4558
878125                 XDOT =        1363
897282
 YDOT =      15776
586307  feet/sec       YDOT =        4824
098190  meter/sec
 ZDOT =     -19064
284514                 ZDOT =       -5804
106691

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21583421
68                 X    =        -6578626
93
 Y    =        2890867
40  feet           Y    =          881136
38  meter
 Z    =        4578715
89                 Z    =         1395592
60
 XDOT =      -5916
189426                 XDOT =       -1803
254537
 YDOT =     -13698
003242  feet/sec       YDOT =       -4175
151388  meter/sec
 ZDOT =     -19035
762738                 ZDOT =       -5802
100483


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   16287
48979343  
00016717  00000-0  10270-3 0  9110
2 25544  51
6425 187
9665 0006931  65
7496 294
4380 15
54170664 23388


Satellite: ISS
Catalog Number: 25544
Epoch time:      16287
48979343   =   yrday
fracday
Element set:     911
Inclination:       51
6425  deg
RA of node:       187
9665  deg
Eccentricity:     
0006931     
Arg of perigee:    65
7496  deg
Mean anomaly:     294
4380  deg
Mean motion:   15
54170664  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2338
Checksum:              352


Coasting Arc #13 (Orbit 2342)
---------------------------------------

Vector Time (GMT): 2016/287/18:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907704
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5999663
36                 A    =         6787137
07  meter
 Y    =        2303968
14  meter          E    =           
0010862
 Z    =       -2186616
47                 I    =           51
61264
 XDOT =      -3533
411150                 Wp   =          102
50523
 YDOT =       4026
544189  meter/sec      RA   =          185
37056  deg
 ZDOT =      -5477
674632                 TA   =          101
75806
                                          MA   =          101
63618
                                          Ha   =            223
347  n
mi
                                          Hp   =            212
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19683934
89                 X    =         5984075
66
 Y    =        7558950
58  feet           Y    =         2370972
96  meter
 Z    =       -7173938
54                 Z    =        -2157509
41
 XDOT =     -11592
556267                 XDOT =       -3551
565866
 YDOT =      13210
446813  feet/sec       YDOT =        3986
928987  meter/sec
 ZDOT =     -17971
373464                 ZDOT =       -5494
883891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4731685
25                 X    =         1442217
66
 Y    =       20591531
38  feet           Y    =         6276298
77  meter
 Z    =       -7047014
33                 Z    =        -2147929
97
 XDOT =     -15862
706264                 XDOT =       -4834
952869
 YDOT =      -2502
298202  feet/sec       YDOT =        -762
700492  meter/sec
 ZDOT =     -18047
218266                 ZDOT =       -5500
792127


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   16287
81129154  
00016717  00000-0  10270-3 0  9125
2 25544  51
6399 186
3595 0006860  69
4374 290
7514 15
54207745 23435


Satellite: ISS
Catalog Number: 25544
Epoch time:      16287
81129154   =   yrday
fracday
Element set:     912
Inclination:       51
6399  deg
RA of node:       186
3595  deg
Eccentricity:     
0006860     
Arg of perigee:    69
4374  deg
Mean anomaly:     290
7514  deg
Mean motion:   15
54207745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2343
Checksum:              334


Coasting Arc #14 (Orbit 2350)
---------------------------------------

Vector Time (GMT): 2016/288/06:36:41
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1020639
24                 A    =         6777614
84  meter
 Y    =       -4193211
64  meter          E    =           
0009672
 Z    =        5217627
12                 I    =           51
59635
 XDOT =       7582
505888                 Wp   =           88
60715
 YDOT =       -482
685800  meter/sec      RA   =          182
91035  deg
 ZDOT =       1093
804248                 TA   =          350
90762
                                          MA   =          350
92512
                                          Ha   =            223
394  n
mi
                                          Hp   =            212
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3348553
94                 X    =         -999019
18
 Y    =      -13757256
02  feet           Y    =        -4204503
53  meter
 Z    =       17118199
22                 Z    =         5212722
11
 XDOT =      24876
987822                 XDOT =        7582
026546
 YDOT =      -1583
614831  feet/sec       YDOT =        -397
895663  meter/sec
 ZDOT =       3588
596613                 ZDOT =        1130
637590

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9910879
64                 X    =        -3020836
12
 Y    =       10147012
84  feet           Y    =         3092809
51  meter
 Z    =       17097375
42                 Z    =         5211280
03
 XDOT =     -13616
562279                 XDOT =       -4150
328183
 YDOT =     -19626
268135  feet/sec       YDOT =       -5982
086528  meter/sec
 ZDOT =       3749
724979                 ZDOT =        1142
916174


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   16288
32568863  
00016717  00000-0  10270-3 0  9137
2 25544  51
6398 183
7990 0006881  69
0889 291
1000 15
54182773 23511


Satellite: ISS
Catalog Number: 25544
Epoch time:      16288
32568863   =   yrday
fracday
Element set:     913
Inclination:       51
6398  deg
RA of node:       183
7990  deg
Eccentricity:     
0006881     
Arg of perigee:    69
0889  deg
Mean anomaly:     291
1000  deg
Mean motion:   15
54182773  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2351
Checksum:              342


Coasting Arc #15 (Orbit 2365)
---------------------------------------

Vector Time (GMT): 2016/289/06:36:41
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -829094
16                 A    =         6777408
49  meter
 Y    =        4204589
15  meter          E    =           
0021032
 Z    =       -5268605
25                 I    =           51
62886
 XDOT =      -7592
353383                 Wp   =           89
08846
 YDOT =       -411
663701  meter/sec      RA   =          177
90827  deg
 ZDOT =        869
577527                 TA   =          189
22531
                                          MA   =          189
26401
                                          Ha   =            223
388  n
mi
                                          Hp   =            212
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2720125
20                 X    =         -850456
22
 Y    =       13794583
82  feet           Y    =         4195197
53  meter
 Z    =      -17285450
29                 Z    =        -5272685
29
 XDOT =     -24909
295875                 XDOT =       -7591
409886
 YDOT =      -1350
602693  feet/sec       YDOT =        -496
561105  meter/sec
 ZDOT =       2852
944644                 ZDOT =         832
697415

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13030299
07                 X    =         3971635
16
 Y    =       -5221315
94  feet           Y    =        -1591457
10  meter
 Z    =      -17303918
10                 Z    =        -5274234
24
 XDOT =      11890
467246                 XDOT =        3624
214417
 YDOT =      20789
373848  feet/sec       YDOT =        6336
601149  meter/sec
 ZDOT =       2691
730653                 ZDOT =         820
439503


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   16289
29017511  
00016717  00000-0  10270-3 0  9144
2 25544  51
6406 178
9909 0006919  72
2967 287
8941 15
54188750 23665


Satellite: ISS
Catalog Number: 25544
Epoch time:      16289
29017511   =   yrday
fracday
Element set:     914
Inclination:       51
6406  deg
RA of node:       178
9909  deg
Eccentricity:     
0006919     
Arg of perigee:    72
2967  deg
Mean anomaly:     287
8941  deg
Mean motion:   15
54188750  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2366
Checksum:              353


Coasting Arc #16 (Orbit 2381)
---------------------------------------

Vector Time (GMT): 2016/290/06:36:41
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2626721
67                 A    =         6779511
71  meter
 Y    =       -4086802
04  meter          E    =           
0014486
 Z    =        4719319
07                 I    =           51
66777
 XDOT =       7038
545774                 Wp   =           68
77987
 YDOT =       1323
416709  meter/sec      RA   =          172
91120  deg
 ZDOT =      -2759
584367                 TA   =           48
56345
                                          MA   =           48
43909
                                          Ha   =            223
263  n
mi
                                          Hp   =            212
056

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8617853
24                 X    =         2649301
14
 Y    =      -13408143
16  feet           Y    =        -4057301
48  meter
 Z    =       15483330
28                 Z    =         4732134
64
 XDOT =      23092
341777                 XDOT =        7036
629057
 YDOT =       4341
918338  feet/sec       YDOT =        1402
115418  meter/sec
 ZDOT =      -9053
754485                 ZDOT =       -2725
396877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15880640
37                 X    =        -4840419
18
 Y    =         305338
13  feet           Y    =           93067
06  meter
 Z    =       15539988
55                 Z    =         4736588
51
 XDOT =      -9146
546335                 XDOT =       -2787
867323
 YDOT =     -20538
113572  feet/sec       YDOT =       -6260
017017  meter/sec
 ZDOT =      -8904
438035                 ZDOT =       -2714
072713


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   16290
31895165  
00016717  00000-0  10270-3 0  9159
2 25544  51
6398 173
8621 0006865  75
1302 285
0610 15
54224517 23828


Satellite: ISS
Catalog Number: 25544
Epoch time:      16290
31895165   =   yrday
fracday
Element set:     915
Inclination:       51
6398  deg
RA of node:       173
8621  deg
Eccentricity:     
0006865     
Arg of perigee:    75
1302  deg
Mean anomaly:     285
0610  deg
Mean motion:   15
54224517  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2382
Checksum:              311


Coasting Arc #17 (Orbit 2396)
---------------------------------------

Vector Time (GMT): 2016/291/06:36:41
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4167179
29                 A    =         6783203
04  meter
 Y    =        3877976
44  meter          E    =           
0012357
 Z    =       -3699462
44                 I    =           51
71151
 XDOT =      -5910
091964                 Wp   =           89
55179
 YDOT =      -2231
685812  meter/sec      RA   =          167
92522  deg
 ZDOT =       4330
526581                 TA   =          226
48021
                                          MA   =          226
58296
                                          Ha   =            223
323  n
mi
                                          Hp   =            211
996

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13671848
05                 X    =        -4192263
23
 Y    =       12723019
80  feet           Y    =         3831235
65  meter
 Z    =      -12137343
98                 Z    =        -3719767
37
 XDOT =     -19390
065498                 XDOT =       -5905
733813
 YDOT =      -7321
803846  feet/sec       YDOT =       -2297
751660  meter/sec
 ZDOT =      14207
764372                 ZDOT =        4301
826878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18184688
13                 X    =         5542692
94
 Y    =        3991712
80  feet           Y    =         1216674
06  meter
 Z    =      -12226738
22                 Z    =        -3726709
81
 XDOT =       5297
915278                 XDOT =        1614
804577
 YDOT =      18874
366324  feet/sec       YDOT =        5752
906856  meter/sec
 ZDOT =      14082
573222                 ZDOT =        4292
368318


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   16291
28342239  
00016717  00000-0  10270-3 0  9166
2 25544  51
6394 169
0541 0006832  78
5781 281
6139 15
54212029 23973


Satellite: ISS
Catalog Number: 25544
Epoch time:      16291
28342239   =   yrday
fracday
Element set:     916
Inclination:       51
6394  deg
RA of node:       169
0541  deg
Eccentricity:     
0006832     
Arg of perigee:    78
5781  deg
Mean anomaly:     281
6139  deg
Mean motion:   15
54212029  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2397
Checksum:              323


Coasting Arc #18 (Orbit 2412)
---------------------------------------

Vector Time (GMT): 2016/292/06:36:41
000
Vector Time (MET): N/A
Weight (LBS)     : 892578
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5373936
44                 A    =         6786827
84  meter
 Y    =       -3482179
86  meter          E    =           
0020195
 Z    =        2224894
08                 I    =           51
75613
 XDOT =       4340
474356                 Wp   =          100
00046
 YDOT =       3178
578955  meter/sec      RA   =          162
95107  deg
 ZDOT =      -5470
279596                 TA   =           55
29811
                                          MA   =           55
10802
                                          Ha   =            223
264  n
mi
                                          Hp   =            211
973

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17631025
07                 X    =         5401667
80
 Y    =      -11424474
60  feet           Y    =        -3421929
69  meter
 Z    =        7299521
27                 Z    =         2251067
59
 XDOT =      14240
401430                 XDOT =        4331
181029
 YDOT =      10428
408644  feet/sec       YDOT =        3227
064721  meter/sec
 ZDOT =     -17947
111534                 ZDOT =       -5449
216902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19511145
26                 X    =        -5946997
07
 Y    =       -7680784
23  feet           Y    =        -2341103
03  meter
 Z    =        7414542
47                 Z    =         2259952
55
 XDOT =       -408
465280                 XDOT =        -124
500217
 YDOT =     -16319
804623  feet/sec       YDOT =       -4974
276449  meter/sec
 ZDOT =     -17855
459209                 ZDOT =       -5442
343967


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   16292
31218134  
00016717  00000-0  10270-3 0  9178
2 25544  51
6403 163
9243 0006811  82
0799 278
1127 15
54245568 24133


Satellite: ISS
Catalog Number: 25544
Epoch time:      16292
31218134   =   yrday
fracday
Element set:     917
Inclination:       51
6403  deg
RA of node:       163
9243  deg
Eccentricity:     
0006811     
Arg of perigee:    82
0799  deg
Mean anomaly:     278
1127  deg
Mean motion:   15
54245568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2413
Checksum:              305
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