[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: February 27th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10 7639 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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


062/01:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 214 4

064/09:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 214 6

065/04:04:36 465 -2 0 3 0 3 0
N/A -2 0 -0 3 220 5
000/00:09:12 930 1 1 0 0 216 2

067/19:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 216 4

070/23:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 216 4

Coasting Arc #1 (Orbit 2760)
---------------------------------------

Vector Time (GMT): 2016/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906097
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1469150
35                 A    =         6788790
05  meter
 Y    =        6601788
17  meter          E    =           
0013945
 Z    =        -496159
42                 I    =           51
30314
 XDOT =      -4787
376626                 Wp   =          146
08104
 YDOT =        624
330302  meter/sec      RA   =          254
08493  deg
 ZDOT =      -5960
932712                 TA   =           39
29801
                                          MA   =           39
19689
                                          Ha   =            221
243  n
mi
                                          Hp   =            214
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4820047
08                 X    =         1397628
43
 Y    =       21659410
01  feet           Y    =         6617817
22  meter
 Z    =       -1627819
63                 Z    =         -489197
34
 XDOT =     -15706
616226                 XDOT =       -4765
046899
 YDOT =       2048
327762  feet/sec       YDOT =         570
918726  meter/sec
 ZDOT =     -19556
865852                 ZDOT =       -5984
134184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4801329
10                 X    =        -1463445
11
 Y    =       21665730
05  feet           Y    =         6603714
52  meter
 Z    =       -1598772
27                 Z    =         -487305
79
 XDOT =     -13400
308534                 XDOT =       -4084
414041
 YDOT =      -4397
416329  feet/sec       YDOT =       -1340
332497  meter/sec
 ZDOT =     -19657
543280                 ZDOT =       -5991
619192


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   16057
53124938  
00016717  00000-0  10270-3 0  9001
2 25544  51
6390 254
8482 0003315 172
1707 187
9498 15
54279789 27615


Satellite: ISS
Catalog Number: 25544
Epoch time:      16057
53124938   =   yrday
fracday
Element set:     900
Inclination:       51
6390  deg
RA of node:       254
8482  deg
Eccentricity:     
0003315     
Arg of perigee:   172
1707  deg
Mean anomaly:     187
9498  deg
Mean motion:   15
54279789  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2761
Checksum:              340


Coasting Arc #2 (Orbit 2776)
---------------------------------------

Vector Time (GMT): 2016/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906097
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -573581
37                 A    =         6786800
42  meter
 Y    =       -6396394
71  meter          E    =           
0013368
 Z    =        2181349
26                 I    =           51
30505
 XDOT =       5209
193566                 Wp   =           85
49237
 YDOT =       1401
188985  meter/sec      RA   =          249
08813  deg
 ZDOT =       5450
566779                 TA   =          298
84287
                                          MA   =          298
97698
                                          Ha   =            221
182  n
mi
                                          Hp   =            214
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1881828
65                 X    =         -512608
64
 Y    =      -20985546
96  feet           Y    =        -6402467
68  meter
 Z    =        7156657
69                 Z    =         2178711
88
 XDOT =      17090
530073                 XDOT =        5166
661676
 YDOT =       4597
076721  feet/sec       YDOT =        1459
204531  meter/sec
 ZDOT =      17882
436938                 ZDOT =        5475
768043

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6802772
88                 X    =         2073485
18
 Y    =      -19945042
88  feet           Y    =        -6079249
07  meter
 Z    =        7146310
61                 Z    =         2178195
47
 XDOT =      12166
933426                 XDOT =        3708
481308
 YDOT =      10629
029812  feet/sec       YDOT =        3239
728287  meter/sec
 ZDOT =      17991
441840                 ZDOT =        5483
791473


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   16058
55997731  
00016717  00000-0  10270-3 0  9014
2 25544  51
6376 249
7179 0003500 176
8313 183
2863 15
54307526 27778


Satellite: ISS
Catalog Number: 25544
Epoch time:      16058
55997731   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       249
7179  deg
Eccentricity:     
0003500     
Arg of perigee:   176
8313  deg
Mean anomaly:     183
2863  deg
Mean motion:   15
54307526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2777
Checksum:              336


Coasting Arc #3 (Orbit 2791)
---------------------------------------

Vector Time (GMT): 2016/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906097
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -496928
70                 A    =         6783089
79  meter
 Y    =        5689480
89  meter          E    =           
0006098
 Z    =       -3662301
83                 I    =           51
30492
 XDOT =      -5429
637110                 Wp   =          113
63345
 YDOT =      -3251
521740  meter/sec      RA   =          244
08422  deg
 ZDOT =      -4322
719921                 TA   =          110
12555
                                          MA   =          110
05993
                                          Ha   =            221
091  n
mi
                                          Hp   =            214
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1630343
51                 X    =         -542723
19
 Y    =       18666275
89  feet           Y    =         5683667
42  meter
 Z    =      -12015425
95                 Z    =        -3664827
67
 XDOT =     -17813
770046                 XDOT =       -5371
876473
 YDOT =     -10667
722244  feet/sec       YDOT =       -3311
917098  meter/sec
 ZDOT =     -14182
151971                 ZDOT =       -4348
954884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8750592
34                 X    =        -2667180
55
 Y    =       16559853
07  feet           Y    =         5047443
22  meter
 Z    =      -12027332
90                 Z    =        -3665931
07
 XDOT =     -10909
001096                 XDOT =       -3325
063534
 YDOT =     -16127
827139  feet/sec       YDOT =       -4915
761712  meter/sec
 ZDOT =     -14295
334003                 ZDOT =       -4357
217804


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   16059
52440408  
00016717  00000-0  10270-3 0  9027
2 25544  51
6375 244
9087 0003376 178
3122 181
8042 15
54314381 27925


Satellite: ISS
Catalog Number: 25544
Epoch time:      16059
52440408   =   yrday
fracday
Element set:     902
Inclination:       51
6375  deg
RA of node:       244
9087  deg
Eccentricity:     
0003376     
Arg of perigee:   178
3122  deg
Mean anomaly:     181
8042  deg
Mean motion:   15
54314381  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2792
Checksum:              306


Coasting Arc #4 (Orbit 2807)
---------------------------------------

Vector Time (GMT): 2016/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906097
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1644417
51                 A    =         6779365
94  meter
 Y    =       -4590524
11  meter          E    =           
0009666
 Z    =        4707100
86                 I    =           51
30763
 XDOT =       5383
018913                 Wp   =          135
89868
 YDOT =       4734
722375  meter/sec      RA   =          239
06981  deg
 ZDOT =       2726
704878                 TA   =          286
95314
                                          MA   =          287
05907
                                          Ha   =            220
983  n
mi
                                          Hp   =            214
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5395070
58                 X    =         1672762
75
 Y    =      -15060774
65  feet           Y    =        -4571976
16  meter
 Z    =       15443244
28                 Z    =         4715158
31
 XDOT =      17660
823207                 XDOT =        5316
428921
 YDOT =      15533
866059  feet/sec       YDOT =        4794
546831  meter/sec
 ZDOT =       8945
882145                 ZDOT =        2752
691827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10574611
29                 X    =         3223141
52
 Y    =      -11958572
58  feet           Y    =        -3644972
92  meter
 Z    =       15478942
20                 Z    =         4717981
58
 XDOT =       9589
172221                 XDOT =        2922
779693
 YDOT =      20246
850353  feet/sec       YDOT =        6171
239988  meter/sec
 ZDOT =       9057
753020                 ZDOT =        2760
803121


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   16060
55311616  
00016717  00000-0  10270-3 0  9031
2 25544  51
6379 239
7784 0003352 183
9262 176
1865 15
54305612 28081


Satellite: ISS
Catalog Number: 25544
Epoch time:      16060
55311616   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:       239
7784  deg
Eccentricity:     
0003352     
Arg of perigee:   183
9262  deg
Mean anomaly:     176
1865  deg
Mean motion:   15
54305612  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2808
Checksum:              316


Coasting Arc #5 (Orbit 2822)
---------------------------------------

Vector Time (GMT): 2016/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906097
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2869146
58                 A    =         6776988
54  meter
 Y    =        3203430
11  meter          E    =           
0014380
 Z    =       -5249866
33                 I    =           51
31713
 XDOT =      -4976
002245                 Wp   =           97
59219
 YDOT =      -5766
179107  meter/sec      RA   =          234
04791  deg
 ZDOT =       -802
764224                 TA   =          164
71275
                                          MA   =          164
66926
                                          Ha   =            220
996  n
mi
                                          Hp   =            214
191

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9413210
57                 X    =        -2879253
48
 Y    =       10509941
31  feet           Y    =         3171288
40  meter
 Z    =      -17223970
91                 Z    =        -5263828
69
 XDOT =     -16325
466682                 XDOT =       -4907
254119
 YDOT =     -18917
910456  feet/sec       YDOT =       -5821
439751  meter/sec
 ZDOT =      -2633
740893                 ZDOT =        -826
768695

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12464487
43                 X    =        -3799175
77
 Y    =        6449542
86  feet           Y    =         1965820
66  meter
 Z    =      -17285037
56                 Z    =        -5268479
45
 XDOT =      -7923
696913                 XDOT =       -2415
142819
 YDOT =     -22615
425651  feet/sec       YDOT =       -6893
181738  meter/sec
 ZDOT =      -2736
860692                 ZDOT =        -834
195139


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   16061
51752507  
00016717  00000-0  10270-3 0  9047
2 25544  51
6378 234
9695 0003463 182
7513 177
3622 15
54333947 28230


Satellite: ISS
Catalog Number: 25544
Epoch time:      16061
51752507   =   yrday
fracday
Element set:     904
Inclination:       51
6378  deg
RA of node:       234
9695  deg
Eccentricity:     
0003463     
Arg of perigee:   182
7513  deg
Mean anomaly:     177
3622  deg
Mean motion:   15
54333947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2823
Checksum:              321


Coasting Arc #6 (Orbit 2831)
---------------------------------------

Vector Time (GMT): 2016/062/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2063637
29                 A    =         6777612
49  meter
 Y    =       -3954741
97  meter          E    =           
0007003
 Z    =        5100998
27                 I    =           51
32980
 XDOT =       5612
372664                 Wp   =          149
08250
 YDOT =       4982
153077  meter/sec      RA   =          231
32812  deg
 ZDOT =       1585
212517                 TA   =          285
52950
                                          MA   =          285
60680
                                          Ha   =            220
792  n
mi
                                          Hp   =            214
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6770463
54                 X    =         2082928
56
 Y    =      -12974875
22  feet           Y    =        -3931556
68  meter
 Z    =       16735558
62                 Z    =         5111070
03
 XDOT =      18413
296143                 XDOT =        5548
543652
 YDOT =      16345
646579  feet/sec       YDOT =        5044
557608  meter/sec
 ZDOT =       5200
828469                 ZDOT =        1612
320321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7624990
23                 X    =        -2324097
02
 Y    =       12432240
61  feet           Y    =         3789346
94  meter
 Z    =       16779880
91                 Z    =         5114507
70
 XDOT =     -16183
902572                 XDOT =       -4932
853504
 YDOT =     -17133
454879  feet/sec       YDOT =       -5222
277047  meter/sec
 ZDOT =       5317
542486                 ZDOT =        1620
786950


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   16062
09616651  
00016717  00000-0  10270-3 0  9051
2 25544  51
6379 232
0874 0003156 188
5293 171
5806 15
54337768 28322


Satellite: ISS
Catalog Number: 25544
Epoch time:      16062
09616651   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:       232
0874  deg
Eccentricity:     
0003156     
Arg of perigee:   188
5293  deg
Mean anomaly:     171
5806  deg
Mean motion:   15
54337768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2832
Checksum:              327


Coasting Arc #7 (Orbit 2846)
---------------------------------------

Vector Time (GMT): 2016/063/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3391662
71                 A    =         6776795
80  meter
 Y    =        2570402
66  meter          E    =           
0014652
 Z    =       -5286449
97                 I    =           51
34820
 XDOT =      -5031
206996                 Wp   =          105
65184
 YDOT =      -5758
118911  meter/sec      RA   =          226
30498  deg
 ZDOT =        425
274802                 TA   =          168
44255
                                          MA   =          168
40888
                                          Ha   =            220
768  n
mi
                                          Hp   =            214
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11127502
34                 X    =        -3394474
48
 Y    =        8433079
60  feet           Y    =         2532458
67  meter
 Z    =      -17343995
98                 Z    =        -5302932
70
 XDOT =     -16506
584632                 XDOT =       -4968
510135
 YDOT =     -18891
466244  feet/sec       YDOT =       -5814
030613  meter/sec
 ZDOT =       1395
258537                 ZDOT =         400
987469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11490017
05                 X    =         3502157
20
 Y    =       -7772939
79  feet           Y    =        -2369192
05  meter
 Z    =      -17415890
78                 Z    =        -5308363
51
 XDOT =      14815
483265                 XDOT =        4515
759299
 YDOT =      18986
871821  feet/sec       YDOT =        5787
198531  meter/sec
 ZDOT =       1290
883255                 ZDOT =         393
461216


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   16063
06056284  
00016717  00000-0  10270-3 0  9060
2 25544  51
6382 227
2780 0003151 191
8472 168
2607 15
54339399 28479


Satellite: ISS
Catalog Number: 25544
Epoch time:      16063
06056284   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:       227
2780  deg
Eccentricity:     
0003151     
Arg of perigee:   191
8472  deg
Mean anomaly:     168
2607  deg
Mean motion:   15
54339399  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2847
Checksum:              323


Coasting Arc #8 (Orbit 2862)
---------------------------------------

Vector Time (GMT): 2016/064/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4590134
67                 A    =         6778495
76  meter
 Y    =       -1130358
54  meter          E    =           
0004977
 Z    =        4854010
96                 I    =           51
37766
 XDOT =       4026
712756                 Wp   =           83
32954
 YDOT =       6076
819669  meter/sec      RA   =          221
28541  deg
 ZDOT =      -2390
016390                 TA   =           30
18519
                                          MA   =           30
15652
                                          Ha   =            220
477  n
mi
                                          Hp   =            214
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15059496
95                 X    =         4578855
08
 Y    =       -3708525
39  feet           Y    =        -1079091
27  meter
 Z    =       15925232
80                 Z    =         4876281
09
 XDOT =      13210
999856                 XDOT =        3970
070501
 YDOT =      19937
072406  feet/sec       YDOT =        6121
532142  meter/sec
 ZDOT =      -7841
261122                 ZDOT =       -2370
593957

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15097186
26                 X    =        -4601622
37
 Y    =        3086296
63  feet           Y    =          940703
21  meter
 Z    =       16021997
03                 Z    =         4883504
70
 XDOT =     -12201
497294                 XDOT =       -3719
016375
 YDOT =     -19366
062128  feet/sec       YDOT =       -5902
775737  meter/sec
 ZDOT =      -7758
015472                 ZDOT =       -2364
643116


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   16064
08924174  
00016717  00000-0  10270-3 0  9076
2 25544  51
6388 222
1484 0003041 197
3349 162
7701 15
54369680 28630


Satellite: ISS
Catalog Number: 25544
Epoch time:      16064
08924174   =   yrday
fracday
Element set:     907
Inclination:       51
6388  deg
RA of node:       222
1484  deg
Eccentricity:     
0003041     
Arg of perigee:   197
3349  deg
Mean anomaly:     162
7701  deg
Mean motion:   15
54369680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2863
Checksum:              320


Coasting Arc #9 (Orbit 2867)
---------------------------------------

Vector Time (GMT): 2016/064/09:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 890369
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1034104
21                 A    =         6781126
37  meter
 Y    =        5219094
33  meter          E    =           
0006449
 Z    =       -4209648
12                 I    =           51
39351
 XDOT =      -6540
176833                 Wp   =           92
03659
 YDOT =      -1637
839370  meter/sec      RA   =          219
61278  deg
 ZDOT =      -3642
249630                 TA   =          140
52540
                                          MA   =          140
47840
                                          Ha   =            220
563  n
mi
                                          Hp   =            214
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3392730
33                 X    =          996114
52
 Y    =       17123012
91  feet           Y    =         5230445
61  meter
 Z    =      -13811181
49                 Z    =        -4204717
48
 XDOT =     -21457
273074                 XDOT =       -6503
683794
 YDOT =      -5373
488746  feet/sec       YDOT =       -1710
772230  meter/sec
 ZDOT =     -11949
637894                 ZDOT =       -3673
930955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12811626
80                 X    =        -3904983
85
 Y    =       11880124
64  feet           Y    =         3621061
99  meter
 Z    =      -13790641
08                 Z    =        -4203387
40
 XDOT =      -5665
641899                 XDOT =       -1726
887651
 YDOT =     -20121
075892  feet/sec       YDOT =       -6132
903932  meter/sec
 ZDOT =     -12086
773799                 ZDOT =       -3684
048654


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   16064
41070077  
00016717  00000-0  10270-3 0  9088
2 25544  51
6378 220
5441 0003053 199
4906 160
6130 15
54374273 28681


Satellite: ISS
Catalog Number: 25544
Epoch time:      16064
41070077   =   yrday
fracday
Element set:     908
Inclination:       51
6378  deg
RA of node:       220
5441  deg
Eccentricity:     
0003053     
Arg of perigee:   199
4906  deg
Mean anomaly:     160
6130  deg
Mean motion:   15
54374273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2868
Checksum:              303


Coasting Arc #10 (Orbit 2879)
---------------------------------------

Vector Time (GMT): 2016/065/04:09:12
930
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5402071
41                 A    =         6782957
20  meter
 Y    =         157308
81  meter          E    =           
0005868
 Z    =       -4105445
81                 I    =           51
41753
 XDOT =      -3055
700006                 Wp   =          138
61164
 YDOT =      -5913
797323  meter/sec      RA   =          215
63598  deg
 ZDOT =       3792
981035                 TA   =          170
68962
                                          MA   =          170
67874
                                          Ha   =            220
513  n
mi
                                          Hp   =            216
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17723331
39                 X    =        -5383486
81
 Y    =         516105
02  feet           Y    =           97002
80  meter
 Z    =      -13469310
41                 Z    =        -4131642
18
 XDOT =     -10025
262487                 XDOT =       -3007
767729
 YDOT =     -19402
222189  feet/sec       YDOT =       -5947
699840  meter/sec
 ZDOT =      12444
163500                 ZDOT =        3778
254404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12151716
94                 X    =         3703843
32
 Y    =      -12792348
25  feet           Y    =        -3899107
75  meter
 Z    =      -13582958
61                 Z    =        -4140085
78
 XDOT =      19907
952671                 XDOT =        6067
943974
 YDOT =       5760
381840  feet/sec       YDOT =        1755
764385  meter/sec
 ZDOT =      12381
237099                 ZDOT =        3773
801068


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   16065
18220322  
00016717  00000-0  10270-3 0  9094
2 25544  51
6411 216
6980 0003760 240
2454 119
8324 15
53824211 28807


Satellite: ISS
Catalog Number: 25544
Epoch time:      16065
18220322   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:       216
6980  deg
Eccentricity:     
0003760     
Arg of perigee:   240
2454  deg
Mean anomaly:     119
8324  deg
Mean motion:   15
53824211  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2880
Checksum:              285


Coasting Arc #11 (Orbit 2895)
---------------------------------------

Vector Time (GMT): 2016/066/04:09:12
930
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6062109
48                 A    =         6786591
42  meter
 Y    =         905258
52  meter          E    =           
0010294
 Z    =        2900484
84                 I    =           51
45593
 XDOT =       1573
870847                 Wp   =          110
46708
 YDOT =       5581
162860  meter/sec      RA   =          210
64161  deg
 ZDOT =      -5020
416896                 TA   =           36
37895
                                          MA   =           36
30903
                                          Ha   =            220
343  n
mi
                                          Hp   =            216
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19888810
64                 X    =         6037447
06
 Y    =        2970008
26  feet           Y    =          972911
47  meter
 Z    =        9516026
37                 Z    =         2929872
52
 XDOT =       5163
618266                 XDOT =        1535
730519
 YDOT =      18310
901773  feet/sec       YDOT =        5598
549141  meter/sec
 ZDOT =     -16471
184043                 ZDOT =       -5012
864792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15955990
68                 X    =        -4863385
96
 Y    =       12138880
73  feet           Y    =         3699930
85  meter
 Z    =        9643362
05                 Z    =         2939296
75
 XDOT =     -15912
225490                 XDOT =       -4850
046329
 YDOT =      -7828
034248  feet/sec       YDOT =       -2385
984839  meter/sec
 ZDOT =     -16439
309519                 ZDOT =       -5010
701541


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   16066
21124100  
00016717  00000-0  10270-3 0  9108
2 25544  51
6409 211
5715 0003836 243
5958 116
4801 15
53810521 28962


Satellite: ISS
Catalog Number: 25544
Epoch time:      16066
21124100   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:       211
5715  deg
Eccentricity:     
0003836     
Arg of perigee:   243
5958  deg
Mean anomaly:     116
4801  deg
Mean motion:   15
53810521  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2896
Checksum:              284


Coasting Arc #12 (Orbit 2910)
---------------------------------------

Vector Time (GMT): 2016/067/04:09:12
930
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6383801
29                 A    =         6789191
64  meter
 Y    =       -1797218
06  meter          E    =           
0005472
 Z    =       -1437804
95                 I    =           51
49452
 XDOT =        120
349262                 Wp   =           15
96347
 YDOT =      -5039
533171  meter/sec      RA   =          205
65566  deg
 ZDOT =       5775
326833                 TA   =          328
32746
                                          MA   =          328
36037
                                          Ha   =            220
217  n
mi
                                          Hp   =            216
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20944229
95                 X    =        -6356245
79
 Y    =       -5896384
71  feet           Y    =        -1868452
08  meter
 Z    =       -4717207
84                 Z    =        -1468748
14
 XDOT =        394
846661                 XDOT =         148
640080
 YDOT =     -16533
901481  feet/sec       YDOT =       -5038
028434  meter/sec
 ZDOT =      18947
922679                 ZDOT =        5775
980798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18620693
39                 X    =         5675587
35
 Y    =      -11198934
29  feet           Y    =        -3413435
17  meter
 Z    =       -4851166
78                 Z    =        -1478635
63
 XDOT =      11041
885563                 XDOT =        3365
566720
 YDOT =      10164
470527  feet/sec       YDOT =        3098
130617  meter/sec
 ZDOT =      18951
550635                 ZDOT =        5776
432634


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   16067
17595295  
00016717  00000-0  10270-3 0  9112
2 25544  51
6424 206
7636 0003871 249
7320 110
3417 15
53855856 29111


Satellite: ISS
Catalog Number: 25544
Epoch time:      16067
17595295   =   yrday
fracday
Element set:     911
Inclination:       51
6424  deg
RA of node:       206
7636  deg
Eccentricity:     
0003871     
Arg of perigee:   249
7320  deg
Mean anomaly:     110
3417  deg
Mean motion:   15
53855856  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2911
Checksum:              317


Coasting Arc #13 (Orbit 2921)
---------------------------------------

Vector Time (GMT): 2016/067/19:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6197138
26                 A    =         6790109
16  meter
 Y    =       -2753569
00  meter          E    =           
0009167
 Z    =         225412
93                 I    =           51
51531
 XDOT =       2124
492389                 Wp   =           38
75443
 YDOT =      -4280
224119  meter/sec      RA   =          202
44270  deg
 ZDOT =       5996
344908                 TA   =          323
67800
                                          MA   =          323
74018
                                          Ha   =            220
264  n
mi
                                          Hp   =            216
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20331818
42                 X    =        -6166981
52
 Y    =       -9034019
02  feet           Y    =        -2822700
87  meter
 Z    =         739543
73                 Z    =          195382
93
 XDOT =       6970
119385                 XDOT =        2143
069854
 YDOT =     -14042
730048  feet/sec       YDOT =       -4256
361926  meter/sec
 ZDOT =      19673
047599                 ZDOT =        6006
710700

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5326406
70                 X    =        -1623488
76
 Y    =       21605576
60  feet           Y    =         6585379
75  meter
 Z    =         609685
69                 Z    =          185832
20
 XDOT =     -13448
256271                 XDOT =       -4099
028511
 YDOT =      -3885
891024  feet/sec       YDOT =       -1184
419584  meter/sec
 ZDOT =      19718
687716                 ZDOT =        6010
256016


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   16067
88340302  
00016717  00000-0  10270-3 0  9128
2 25544  51
6415 203
2376 0003683 250
3330 109
7425 15
53855434 29229


Satellite: ISS
Catalog Number: 25544
Epoch time:      16067
88340302   =   yrday
fracday
Element set:     912
Inclination:       51
6415  deg
RA of node:       203
2376  deg
Eccentricity:     
0003683     
Arg of perigee:   250
3330  deg
Mean anomaly:     109
7425  deg
Mean motion:   15
53855434  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2922
Checksum:              291


Coasting Arc #14 (Orbit 2936)
---------------------------------------

Vector Time (GMT): 2016/068/19:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5638958
05                 A    =         6788779
14  meter
 Y    =        3298698
22  meter          E    =           
0006974
 Z    =       -1830749
37                 I    =           51
53939
 XDOT =      -3861
882525                 Wp   =          171
90875
 YDOT =       3478
588430  meter/sec      RA   =          197
46552  deg
 ZDOT =      -5636
675832                 TA   =           28
24898
                                          MA   =           28
21118
                                          Ha   =            220
274  n
mi
                                          Hp   =            216
441

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18500518
53                 X    =         5610544
96
 Y    =       10822500
74  feet           Y    =         3361597
65  meter
 Z    =       -6006395
57                 Z    =        -1803426
63
 XDOT =     -12670
218258                 XDOT =       -3873
113776
 YDOT =      11412
691698  feet/sec       YDOT =        3435
338618  meter/sec
 ZDOT =     -18493
030946                 ZDOT =       -5655
463446

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7054305
02                 X    =         2150152
17
 Y    =      -20274036
83  feet           Y    =        -6179526
43  meter
 Z    =       -5888353
49                 Z    =        -1794770
14
 XDOT =      12133
579118                 XDOT =        3698
314915
 YDOT =       9607
654097  feet/sec       YDOT =        2928
412969  meter/sec
 ZDOT =     -18575
087408                 ZDOT =       -5661
686642


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   16068
84810236  
00016717  00000-0  10270-3 0  9134
2 25544  51
6402 198
4309 0003729 252
5414 107
5331 15
53847440 29370


Satellite: ISS
Catalog Number: 25544
Epoch time:      16068
84810236   =   yrday
fracday
Element set:     913
Inclination:       51
6402  deg
RA of node:       198
4309  deg
Eccentricity:     
0003729     
Arg of perigee:   252
5414  deg
Mean anomaly:     107
5331  deg
Mean motion:   15
53847440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2937
Checksum:              308


Coasting Arc #15 (Orbit 2952)
---------------------------------------

Vector Time (GMT): 2016/069/19:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4680871
48                 A    =         6785644
85  meter
 Y    =       -3677794
12  meter          E    =           
0009068
 Z    =        3249213
38                 I    =           51
56010
 XDOT =       5398
862166                 Wp   =           90
22037
 YDOT =      -2665
464308  meter/sec      RA   =          192
48408  deg
 ZDOT =       4749
134126                 TA   =          307
49035
                                          MA   =          307
57277
                                          Ha   =            220
119  n
mi
                                          Hp   =            216
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15357189
91                 X    =        -4655180
72
 Y    =      -12066253
66  feet           Y    =        -3729994
56  meter
 Z    =       10660148
90                 Z    =         3226538
10
 XDOT =      17712
802383                 XDOT =        5405
197760
 YDOT =      -8744
961639  feet/sec       YDOT =       -2605
054444  meter/sec
 ZDOT =      15581
148708                 ZDOT =        4775
376021

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8571618
42                 X    =        -2612629
29
 Y    =       17607989
64  feet           Y    =         5366915
24  meter
 Z    =       10562319
46                 Z    =         3219394
97
 XDOT =     -10950
359472                 XDOT =       -3337
669567
 YDOT =     -14768
581507  feet/sec       YDOT =       -4501
463643  meter/sec
 ZDOT =      15695
430216                 ZDOT =        4783
967130


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   16069
87710352  
00016717  00000-0  10270-3 0  9147
2 25544  51
6403 193
3034 0003764 259
5112 100
5617 15
53884988 29537


Satellite: ISS
Catalog Number: 25544
Epoch time:      16069
87710352   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:       193
3034  deg
Eccentricity:     
0003764     
Arg of perigee:   259
5112  deg
Mean anomaly:     100
5617  deg
Mean motion:   15
53884988  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2953
Checksum:              318


Coasting Arc #16 (Orbit 2967)
---------------------------------------

Vector Time (GMT): 2016/070/19:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3354909
03                 A    =         6781952
57  meter
 Y    =        3947468
42  meter          E    =           
0005369
 Z    =       -4382487
60                 I    =           51
57939
 XDOT =      -6613
895821                 Wp   =           60
17357
 YDOT =       1848
620971  meter/sec      RA   =          187
49566  deg
 ZDOT =      -3398
506037                 TA   =          175
34900
                                          MA   =          175
34401
                                          Ha   =            220
074  n
mi
                                          Hp   =            216
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11006919
37                 X    =         3331806
25
 Y    =       12951011
87  feet           Y    =         3984855
37  meter
 Z    =      -14378240
15                 Z    =        -4366247
11
 XDOT =     -21699
133270                 XDOT =       -6617
567597
 YDOT =       6065
029434  feet/sec       YDOT =        1774
638920  meter/sec
 ZDOT =     -11149
954190                 ZDOT =       -3430
643745

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10106649
06                 X    =         3080506
63
 Y    =      -13738305
16  feet           Y    =        -4187435
41  meter
 Z    =      -14308367
78                 Z    =        -4361190
50
 XDOT =       9792
521668                 XDOT =        2984
760605
 YDOT =      18960
304525  feet/sec       YDOT =        5779
100819  meter/sec
 ZDOT =     -11289
704671                 ZDOT =       -3441
101984


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   16070
84178242  
00016717  00000-0  10270-3 0  9153
2 25544  51
6403 188
4965 0003601 264
2475  95
8267 15
53895248 29684


Satellite: ISS
Catalog Number: 25544
Epoch time:      16070
84178242   =   yrday
fracday
Element set:     915
Inclination:       51
6403  deg
RA of node:       188
4965  deg
Eccentricity:     
0003601     
Arg of perigee:   264
2475  deg
Mean anomaly:      95
8267  deg
Mean motion:   15
53895248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2968
Checksum:              341


Coasting Arc #17 (Orbit 2969)
---------------------------------------

Vector Time (GMT): 2016/070/23:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6171658
92                 A    =         6787275
40  meter
 Y    =        1278472
54  meter          E    =           
0003151
 Z    =       -2513729
13                 I    =           51
60213
 XDOT =      -3106
097660                 Wp   =            4
57253
 YDOT =      -4591
236007  meter/sec      RA   =          186
72311  deg
 ZDOT =       5294
475705                 TA   =          327
21822
                                          MA   =          327
23777
                                          Ha   =            219
957  n
mi
                                          Hp   =            216
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20248224
80                 X    =        -6173285
86
 Y    =        4194463
70  feet           Y    =         1209447
45  meter
 Z    =       -8247142
81                 Z    =        -2543713
53
 XDOT =     -10190
609121                 XDOT =       -3080
244650
 YDOT =     -15063
110260  feet/sec       YDOT =       -4625
825065  meter/sec
 ZDOT =      17370
327115                 ZDOT =        5279
450644

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20131700
42                 X    =         6136142
29
 Y    =        4486897
86  feet           Y    =         1367606
47  meter
 Z    =       -8377462
85                 Z    =        -2553450
68
 XDOT =       3519
675355                 XDOT =        1072
797048
 YDOT =      16498
343253  feet/sec       YDOT =        5028
695024  meter/sec
 ZDOT =      17305
827133                 ZDOT =        5274
816110


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   16070
97040635  
00016717  00000-0  10270-3 0  9162
2 25544  51
6405 187
8555 0003807 268
0605  92
0112 15
53883471 29705


Satellite: ISS
Catalog Number: 25544
Epoch time:      16070
97040635   =   yrday
fracday
Element set:     916
Inclination:       51
6405  deg
RA of node:       187
8555  deg
Eccentricity:     
0003807     
Arg of perigee:   268
0605  deg
Mean anomaly:      92
0112  deg
Mean motion:   15
53883471  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2970
Checksum:              311


Coasting Arc #18 (Orbit 2985)
---------------------------------------

Vector Time (GMT): 2016/071/23:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 890060
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6693728
75                 A    =         6789544
39  meter
 Y    =        -550144
89  meter          E    =           
0010555
 Z    =         953183
13                 I    =           51
64185
 XDOT =       1234
995870                 Wp   =          135
69954
 YDOT =       4721
477522  meter/sec      RA   =          181
75040  deg
 ZDOT =      -5915
517247                 TA   =           33
97776
                                          MA   =           33
91021
                                          Ha   =            219
956  n
mi
                                          Hp   =            216
355

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21961052
34                 X    =         6694752
97
 Y    =       -1804937
29  feet           Y    =         -475285
30  meter
 Z    =        3127241
23                 Z    =          985702
12
 XDOT =       4051
823722                 XDOT =        1210
842361
 YDOT =      15490
411819  feet/sec       YDOT =        4735
152166  meter/sec
 ZDOT =     -19407
864983                 ZDOT =       -5909
577298

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20863716
13                 X    =        -6359260
67
 Y    =       -7024796
18  feet           Y    =        -2141157
88  meter
 Z    =        3268462
05                 Z    =          996227
23
 XDOT =       1781
260530                 XDOT =         542
928209
 YDOT =     -14355
677717  feet/sec       YDOT =       -4375
610568  meter/sec
 ZDOT =     -19382
810530                 ZDOT =       -5907
880650


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   16071
99938468  
00016717  00000-0  10270-3 0  9176
2 25544  51
6406 182
7283 0003768 272
0060  88
0661 15
53910241 29861


Satellite: ISS
Catalog Number: 25544
Epoch time:      16071
99938468   =   yrday
fracday
Element set:     917
Inclination:       51
6406  deg
RA of node:       182
7283  deg
Eccentricity:     
0003768     
Arg of perigee:   272
0060  deg
Mean anomaly:      88
0661  deg
Mean motion:   15
53910241  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2986
Checksum:              331
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