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

 
Date: August 8th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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


There are no maneuvers



Coasting Arc #1 (Orbit 1311)
---------------------------------------

Vector Time (GMT): 2016/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5543685
02                 A    =         6780847
38  meter
 Y    =         820471
74  meter          E    =           
0007750
 Z    =       -3825092
23                 I    =           51
78653
 XDOT =      -3668
711858                 Wp   =           82
66406
 YDOT =       5258
220109  meter/sec      RA   =          155
91338  deg
 ZDOT =      -4195
486353                 TA   =          143
18489
                                          MA   =          143
13165
                                          Ha   =            220
401  n
mi
                                          Hp   =            212
810

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18187942
97                 X    =         5552678
72
 Y    =        2691836
42  feet           Y    =          882515
12  meter
 Z    =      -12549515
18                 Z    =        -3798140
88
 XDOT =     -12036
456228                 XDOT =       -3706
858303
 YDOT =      17251
378310  feet/sec       YDOT =        5216
980717  meter/sec
 ZDOT =     -13764
719005                 ZDOT =       -4213
400630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11417918
80                 X    =        -3480181
65
 Y    =      -14512588
50  feet           Y    =        -4423436
98  meter
 Z    =      -12431954
36                 Z    =        -3789259
69
 XDOT =      19476
683238                 XDOT =        5936
493051
 YDOT =      -3482
349471  feet/sec       YDOT =       -1061
420119  meter/sec
 ZDOT =     -13843
788109                 ZDOT =       -4219
586616


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   16221
52406418  
00016717  00000-0  10270-3 0  9009
2 25544  51
6412 156
8898 0001851 100
7293 259
4068 15
54952217 13125


Satellite: ISS
Catalog Number: 25544
Epoch time:      16221
52406418   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:       156
8898  deg
Eccentricity:     
0001851     
Arg of perigee:   100
7293  deg
Mean anomaly:     259
4068  deg
Mean motion:   15
54952217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1312
Checksum:              298


Coasting Arc #2 (Orbit 1327)
---------------------------------------

Vector Time (GMT): 2016/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4169209
62                 A    =         6776723
30  meter
 Y    =       -2100222
63  meter          E    =           
0008466
 Z    =        4907472
38                 I    =           51
80221
 XDOT =       5293
199134                 Wp   =          119
63402
 YDOT =      -5042
235381  meter/sec      RA   =          150
92746  deg
 ZDOT =       2331
910586                 TA   =          307
57838
                                          MA   =          307
65523
                                          Ha   =            220
359  n
mi
                                          Hp   =            212
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13678509
24                 X    =        -4169252
70
 Y    =       -6890494
19  feet           Y    =        -2146845
66  meter
 Z    =       16100631
17                 Z    =         4887219
53
 XDOT =      17366
138892                 XDOT =        5337
861972
 YDOT =     -16542
766999  feet/sec       YDOT =       -4982
793517  meter/sec
 ZDOT =       7650
625282                 ZDOT =        2357
731968

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5521870
12                 X    =         1683066
01
 Y    =       14384680
08  feet           Y    =         4384450
49  meter
 Z    =       16012519
43                 Z    =         4880615
92
 XDOT =     -22893
126079                 XDOT =       -6977
824829
 YDOT =        119
101933  feet/sec       YDOT =          36
302269  meter/sec
 ZDOT =       7764
204168                 ZDOT =        2366
529431


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   16222
55235530  
00016717  00000-0  10270-3 0  9019
2 25544  51
6413 151
7586 0001659 111
9653 248
1677 15
54980985 13285


Satellite: ISS
Catalog Number: 25544
Epoch time:      16222
55235530   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:       151
7586  deg
Eccentricity:     
0001659     
Arg of perigee:   111
9653  deg
Mean anomaly:     248
1677  deg
Mean motion:   15
54980985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1328
Checksum:              318


Coasting Arc #3 (Orbit 1342)
---------------------------------------

Vector Time (GMT): 2016/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2465269
18                 A    =         6774937
83  meter
 Y    =        3395120
16  meter          E    =           
0016516
 Z    =       -5333573
13                 I    =           51
82452
 XDOT =      -6287
076683                 Wp   =           91
19968
 YDOT =       4370
103494  meter/sec      RA   =          145
93166  deg
 ZDOT =       -124
848039                 TA   =          177
61591
                                          MA   =          177
60803
                                          Ha   =            220
297  n
mi
                                          Hp   =            212
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8088153
48                 X    =         2453028
86
 Y    =       11138845
68  feet           Y    =         3422619
95  meter
 Z    =      -17498599
50                 Z    =        -5321627
33
 XDOT =     -20626
892005                 XDOT =       -6334
870565
 YDOT =      14337
609888  feet/sec       YDOT =        4299
529966  meter/sec
 ZDOT =       -409
606426                 ZDOT =        -155
504974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1226934
88                 X    =          373969
75
 Y    =      -13776459
77  feet           Y    =        -4199064
94  meter
 Z    =      -17446973
41                 Z    =        -5317837
50
 XDOT =      23944
326576                 XDOT =        7298
230741
 YDOT =       2818
904034  feet/sec       YDOT =         859
201950  meter/sec
 ZDOT =       -544
213754                 ZDOT =        -165
876352


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   16223
51637445  
00016717  00000-0  10270-3 0  9028
2 25544  51
6420 146
9465 0001743 109
0304 251
1038 15
54963261 13430


Satellite: ISS
Catalog Number: 25544
Epoch time:      16223
51637445   =   yrday
fracday
Element set:     902
Inclination:       51
6420  deg
RA of node:       146
9465  deg
Eccentricity:     
0001743     
Arg of perigee:   109
0304  deg
Mean anomaly:     251
1038  deg
Mean motion:   15
54963261  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1343
Checksum:              282


Coasting Arc #4 (Orbit 1358)
---------------------------------------

Vector Time (GMT): 2016/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -636158
05                 A    =         6776276
69  meter
 Y    =       -4532747
12  meter          E    =           
0007193
 Z    =        4991851
97                 I    =           51
85509
 XDOT =       6625
634446                 Wp   =           68
08669
 YDOT =      -3250
674158  meter/sec      RA   =          140
93885  deg
 ZDOT =      -2102
300639                 TA   =           42
32761
                                          MA   =           42
27213
                                          Ha   =            220
294  n
mi
                                          Hp   =            212
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2087132
72                 X    =         -609672
52
 Y    =      -14871217
57  feet           Y    =        -4539712
96  meter
 Z    =       16377467
10                 Z    =         4988826
03
 XDOT =      21737
645820                 XDOT =        6671
703866
 YDOT =     -10664
941462  feet/sec       YDOT =       -3176
324297  meter/sec
 ZDOT =      -6897
311808                 ZDOT =       -2070
003320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7982998
63                 X    =        -2433217
98
 Y    =       12735365
81  feet           Y    =         3881739
50  meter
 Z    =       16364988
67                 Z    =         4988048
55
 XDOT =     -22564
157434                 XDOT =       -6877
555186
 YDOT =      -5441
684060  feet/sec       YDOT =       -1658
625301  meter/sec
 ZDOT =      -6755
701893                 ZDOT =       -2059
137937


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   16224
54465331  
00016717  00000-0  10270-3 0  9036
2 25544  51
6416 141
8153 0001710 110
6256 249
5081 15
54978522 13593


Satellite: ISS
Catalog Number: 25544
Epoch time:      16224
54465331   =   yrday
fracday
Element set:     903
Inclination:       51
6416  deg
RA of node:       141
8153  deg
Eccentricity:     
0001710     
Arg of perigee:   110
6256  deg
Mean anomaly:     249
5081  deg
Mean motion:   15
54978522  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1359
Checksum:              293


Coasting Arc #5 (Orbit 1373)
---------------------------------------

Vector Time (GMT): 2016/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1091509
95                 A    =         6780110
67  meter
 Y    =        5391087
05  meter          E    =           
0008531
 Z    =       -3973319
33                 I    =           51
89316
 XDOT =      -6293
462560                 Wp   =          109
59006
 YDOT =       1691
631356  meter/sec      RA   =          135
95511  deg
 ZDOT =       4028
361643                 TA   =          202
32153
                                          MA   =          202
35869
                                          Ha   =            220
216  n
mi
                                          Hp   =            212
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3581069
40                 X    =        -1132412
83
 Y    =       17687293
48  feet           Y    =         5378652
40  meter
 Z    =      -13035824
56                 Z    =        -3978720
86
 XDOT =     -20647
843043                 XDOT =       -6331
478937
 YDOT =       5549
971639  feet/sec       YDOT =        1621
041049  meter/sec
 ZDOT =      13216
409591                 ZDOT =        3997
697530

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13944868
63                 X    =         4250395
96
 Y    =      -11426553
02  feet           Y    =        -3482813
36  meter
 Z    =      -13060308
41                 Z    =        -3980782
00
 XDOT =      18698
075432                 XDOT =        5699
173392
 YDOT =       7882
208884  feet/sec       YDOT =        2402
497268  meter/sec
 ZDOT =      13082
171048                 ZDOT =        3987
445735


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   16225
50865923  
00016717  00000-0  10270-3 0  9045
2 25544  51
6423 137
0035 0001713 117
1570 242
9758 15
54989332 13747


Satellite: ISS
Catalog Number: 25544
Epoch time:      16225
50865923   =   yrday
fracday
Element set:     904
Inclination:       51
6423  deg
RA of node:       137
0035  deg
Eccentricity:     
0001713     
Arg of perigee:   117
1570  deg
Mean anomaly:     242
9758  deg
Mean motion:   15
54989332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1374
Checksum:              306


Coasting Arc #6 (Orbit 1389)
---------------------------------------

Vector Time (GMT): 2016/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2588554
53                 A    =         6784463
95  meter
 Y    =       -5800513
55  meter          E    =           
0015437
 Z    =        2362696
33                 I    =           51
93059
 XDOT =       5434
243896                 Wp   =          108
43086
 YDOT =        210
271888  meter/sec      RA   =          130
98757  deg
 ZDOT =      -5413
377786                 TA   =           45
28408
                                          MA   =           45
15848
                                          Ha   =            220
207  n
mi
                                          Hp   =            212
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8492632
98                 X    =         2641748
12
 Y    =      -19030556
27  feet           Y    =        -5771269
22  meter
 Z    =        7751628
40                 Z    =         2375399
84
 XDOT =      17828
884173                 XDOT =        5457
784264
 YDOT =        689
868399  feet/sec       YDOT =         271
172953  meter/sec
 ZDOT =     -17760
425806                 ZDOT =       -5386
922702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18453260
40                 X    =        -5624553
77
 Y    =        9637711
97  feet           Y    =         2937574
61  meter
 Z    =        7808093
10                 Z    =         2379906
78
 XDOT =     -12911
517121                 XDOT =       -3935
430419
 YDOT =     -10362
769899  feet/sec       YDOT =       -3158
572265  meter/sec
 ZDOT =     -17644
875011                 ZDOT =       -5378
157903


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   16226
53692488  
00016717  00000-0  10270-3 0  9054
2 25544  51
6428 131
8716 0001702 122
5224 237
6094 15
54976476 13901


Satellite: ISS
Catalog Number: 25544
Epoch time:      16226
53692488   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:       131
8716  deg
Eccentricity:     
0001702     
Arg of perigee:   122
5224  deg
Mean anomaly:     237
6094  deg
Mean motion:   15
54976476  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1390
Checksum:              319


Coasting Arc #7 (Orbit 1404)
---------------------------------------

Vector Time (GMT): 2016/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3690898
88                 A    =         6786692
35  meter
 Y    =        5672142
95  meter          E    =           
0011468
 Z    =        -449547
22                 I    =           51
95942
 XDOT =      -4183
809116                 Wp   =           49
83689
 YDOT =      -2253
981440  meter/sec      RA   =          126
03167  deg
 ZDOT =       6018
808600                 TA   =          305
33529
                                          MA   =          305
44244
                                          Ha   =            220
129  n
mi
                                          Hp   =            212
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12109248
28                 X    =        -3751868
22
 Y    =       18609392
89  feet           Y    =         5630527
96  meter
 Z    =       -1474892
46                 Z    =         -467624
41
 XDOT =     -13726
407861                 XDOT =       -4187
529945
 YDOT =      -7394
952232  feet/sec       YDOT =       -2300
788507  meter/sec
 ZDOT =      19746
747376                 ZDOT =        5998
475909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20929485
08                 X    =         6379307
05
 Y    =       -7393095
69  feet           Y    =        -2253415
56  meter
 Z    =       -1554829
87                 Z    =         -473912
14
 XDOT =       5947
776725                 XDOT =        1812
882346
 YDOT =      12774
357357  feet/sec       YDOT =        3893
624122  meter/sec
 ZDOT =      19658
277697                 ZDOT =        5991
843042


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   16227
50091589  
00016717  00000-0  10270-3 0  9068
2 25544  51
6436 127
0600 0001586 122
2838 237
8469 15
55002172 14056


Satellite: ISS
Catalog Number: 25544
Epoch time:      16227
50091589   =   yrday
fracday
Element set:     906
Inclination:       51
6436  deg
RA of node:       127
0600  deg
Eccentricity:     
0001586     
Arg of perigee:   122
2838  deg
Mean anomaly:     237
8469  deg
Mean motion:   15
55002172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1405
Checksum:              298


Coasting Arc #8 (Orbit 1420)
---------------------------------------

Vector Time (GMT): 2016/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4398356
22                 A    =         6785835
69  meter
 Y    =       -4917870
81  meter          E    =           
0009759
 Z    =       -1570436
64                 I    =           51
97468
 XDOT =       2707
251910                 Wp   =          141
09569
 YDOT =       4256
939422  meter/sec      RA   =          121
08096  deg
 ZDOT =      -5775
255175                 TA   =           55
99884
                                          MA   =           55
90618
                                          Ha   =            220
162  n
mi
                                          Hp   =            212
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14430302
57                 X    =         4460650
58
 Y    =      -16134746
74  feet           Y    =        -4868337
12  meter
 Z    =       -5152351
18                 Z    =        -1548919
64
 XDOT =       8882
060073                 XDOT =        2687
501747
 YDOT =      13966
336686  feet/sec       YDOT =        4287
103354  meter/sec
 ZDOT =     -18947
687581                 ZDOT =       -5762
152173

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21226140
99                 X    =        -6469727
77
 Y    =        4356960
13  feet           Y    =         1328001
45  meter
 Z    =       -5057493
90                 Z    =        -1541524
14
 XDOT =       1394
042079                 XDOT =         424
904026
 YDOT =     -15033
199605  feet/sec       YDOT =       -4582
119239  meter/sec
 ZDOT =     -18891
141802                 ZDOT =       -5758
020021


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   16228
52916794  
00016717  00000-0  10270-3 0  9076
2 25544  51
6438 121
9286 0001614 133
3979 226
7309 15
54982634 14219


Satellite: ISS
Catalog Number: 25544
Epoch time:      16228
52916794   =   yrday
fracday
Element set:     907
Inclination:       51
6438  deg
RA of node:       121
9286  deg
Eccentricity:     
0001614     
Arg of perigee:   133
3979  deg
Mean anomaly:     226
7309  deg
Mean motion:   15
54982634  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1421
Checksum:              329


Coasting Arc #9 (Orbit 1436)
---------------------------------------

Vector Time (GMT): 2016/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4670410
09                 A    =         6782136
76  meter
 Y    =        3606045
11  meter          E    =           
0013778
 Z    =        3332584
28                 I    =           51
97892
 XDOT =      -1200
205485                 Wp   =           92
41145
 YDOT =      -5930
460286  meter/sec      RA   =          116
12209  deg
 ZDOT =       4717
752391                 TA   =          306
21603
                                          MA   =          306
34332
                                          Ha   =            220
132  n
mi
                                          Hp   =            212
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15322867
75                 X    =        -4726574
62
 Y    =       11830856
68  feet           Y    =         3553503
45  meter
 Z    =       10933675
47                 Z    =         3309760
62
 XDOT =      -3937
682039                 XDOT =       -1156
716731
 YDOT =     -19456
890701  feet/sec       YDOT =       -5943
638600  meter/sec
 ZDOT =      15478
190259                 ZDOT =        4712
027868

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19403158
69                 X    =         5914082
77
 Y    =        -679272
05  feet           Y    =         -207042
12  meter
 Z    =       10833315
63                 Z    =         3301994
60
 XDOT =      -8073
684104                 XDOT =       -2460
858915
 YDOT =      16762
883585  feet/sec       YDOT =        5109
326917  meter/sec
 ZDOT =      15454
173307                 ZDOT =        4710
432024


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   16229
55741219  
00016717  00000-0  10270-3 0  9089
2 25544  51
6443 116
7961 0001471 129
7532 230
3751 15
55011131 14377


Satellite: ISS
Catalog Number: 25544
Epoch time:      16229
55741219   =   yrday
fracday
Element set:     908
Inclination:       51
6443  deg
RA of node:       116
7961  deg
Eccentricity:     
0001471     
Arg of perigee:   129
7532  deg
Mean anomaly:     230
3751  deg
Mean motion:   15
55011131  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1437
Checksum:              290


Coasting Arc #10 (Orbit 1451)
---------------------------------------

Vector Time (GMT): 2016/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4597620
31                 A    =         6777601
28  meter
 Y    =       -1795624
31  meter          E    =           
0010983
 Z    =       -4655157
25                 I    =           51
97729
 XDOT =       -243
617600                 Wp   =           76
66934
 YDOT =       7058
778797  meter/sec      RA   =          111
15103  deg
 ZDOT =      -2966
778727                 TA   =          163
90211
                                          MA   =          163
86719
                                          Ha   =            219
961  n
mi
                                          Hp   =            212
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15084056
13                 X    =         4639970
00
 Y    =       -5891155
88  feet           Y    =        -1743973
98  meter
 Z    =      -15272825
62                 Z    =        -4632720
73
 XDOT =       -799
270341                 XDOT =        -308
121517
 YDOT =      23158
723088  feet/sec       YDOT =        7055
693762  meter/sec
 ZDOT =      -9733
526008                 ZDOT =       -2968
118987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15846134
55                 X    =        -4829901
81
 Y    =       -3758938
67  feet           Y    =        -1145724
51  meter
 Z    =      -15174454
50                 Z    =        -4625173
73
 XDOT =      13467
920604                 XDOT =        4105
022200
 YDOT =     -17498
826140  feet/sec       YDOT =       -5333
642208  meter/sec
 ZDOT =      -9740
582548                 ZDOT =       -2968
929561


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   16230
52138312  
00016717  00000-0  10270-3 0  9093
2 25544  51
6441 111
9848 0001360 134
1394 225
9871 15
55045546 14526


Satellite: ISS
Catalog Number: 25544
Epoch time:      16230
52138312   =   yrday
fracday
Element set:     909
Inclination:       51
6441  deg
RA of node:       111
9848  deg
Eccentricity:     
0001360     
Arg of perigee:   134
1394  deg
Mean anomaly:     225
9871  deg
Mean motion:   15
55045546  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1452
Checksum:              293


Coasting Arc #11 (Orbit 1467)
---------------------------------------

Vector Time (GMT): 2016/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4223293
90                 A    =         6774901
07  meter
 Y    =        -279203
01  meter          E    =           
0004674
 Z    =        5287138
07                 I    =           51
97826
 XDOT =       1510
397579                 Wp   =          125
47836
 YDOT =      -7479
322175  meter/sec      RA   =          106
16855  deg
 ZDOT =        808
374650                 TA   =          316
81787
                                          MA   =          316
85451
                                          Ha   =            220
104  n
mi
                                          Hp   =            212
864

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13855951
13                 X    =        -4245540
01
 Y    =        -916020
36  feet           Y    =         -326554
84  meter
 Z    =       17346253
50                 Z    =         5266568
77
 XDOT =       4955
372635                 XDOT =        1589
994344
 YDOT =     -24538
458578  feet/sec       YDOT =       -7461
986809  meter/sec
 ZDOT =       2652
147802                 ZDOT =         815
905304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11132316
99                 X    =         3393130
22
 Y    =        8485721
90  feet           Y    =         2586448
04  meter
 Z    =       17256390
93                 Z    =         5259747
95
 XDOT =     -17064
571479                 XDOT =       -5201
281387
 YDOT =      16902
842606  feet/sec       YDOT =        5151
986426  meter/sec
 ZDOT =       2686
341092                 ZDOT =         818
796765


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   16231
54961509  
00016717  00000-0  10270-3 0  9100
2 25544  51
6433 106
8525 0001469 138
7704 221
3561 15
55044385 14680


Satellite: ISS
Catalog Number: 25544
Epoch time:      16231
54961509   =   yrday
fracday
Element set:     910
Inclination:       51
6433  deg
RA of node:       106
8525  deg
Eccentricity:     
0001469     
Arg of perigee:   138
7704  deg
Mean anomaly:     221
3561  deg
Mean motion:   15
55044385  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1468
Checksum:              304


Coasting Arc #12 (Orbit 1482)
---------------------------------------

Vector Time (GMT): 2016/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3653020
87                 A    =         6775335
41  meter
 Y    =        2413571
72  meter          E    =           
0014740
 Z    =       -5183695
62                 I    =           51
98773
 XDOT =      -2571
646104                 Wp   =          104
67978
 YDOT =       7061
678351  meter/sec      RA   =          101
18226  deg
 ZDOT =       1475
566501                 TA   =          179
47518
                                          MA   =          179
47363
                                          Ha   =            219
833  n
mi
                                          Hp   =            213
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11984976
62                 X    =         3650939
90
 Y    =        7918542
39  feet           Y    =         2454410
28  meter
 Z    =      -17006875
40                 Z    =        -5165955
70
 XDOT =      -8437
159133                 XDOT =       -2657
587985
 YDOT =      23168
236059  feet/sec       YDOT =        7032
440048  meter/sec
 ZDOT =       4841
097445                 ZDOT =        1462
865132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5927085
64                 X    =        -1806575
70
 Y    =      -13184468
90  feet           Y    =        -4018626
12  meter
 Z    =      -16929743
79                 Z    =        -5160185
91
 XDOT =      18651
496673                 XDOT =        5684
976186
 YDOT =     -14528
810553  feet/sec       YDOT =       -4428
381456  meter/sec
 ZDOT =       4784
364752                 ZDOT =        1458
274376


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   16232
51357708  
00016717  00000-0  10270-3 0  9119
2 25544  51
6431 102
0405 0001295 145
0026 215
1213 15
55065122 14832


Satellite: ISS
Catalog Number: 25544
Epoch time:      16232
51357708   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:       102
0405  deg
Eccentricity:     
0001295     
Arg of perigee:   145
0026  deg
Mean anomaly:     215
1213  deg
Mean motion:   15
55065122  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1483
Checksum:              255
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list