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

 
Date: April 29th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 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


124/02:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 213 6

132/13:26:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 213 5

135/07:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 213 2

Coasting Arc #1 (Orbit 3739)
---------------------------------------

Vector Time (GMT): 2016/120/11:18:49
007
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         469015
10                 A    =         6784183
68  meter
 Y    =       -5942563
91  meter          E    =           
0006240
 Z    =       -3242781
01                 I    =           51
32926
 XDOT =       5636
199934                 Wp   =           77
56290
 YDOT =      -2133
220316  meter/sec      RA   =          300
32133  deg
 ZDOT =       4733
469161                 TA   =          244
69864
                                          MA   =          244
76330
                                          Ha   =            221
198  n
mi
                                          Hp   =            213
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1538763
44                 X    =          551183
63
 Y    =      -19496600
75  feet           Y    =        -5936859
67  meter
 Z    =      -10639045
31                 Z    =        -3240303
00
 XDOT =      18491
469599                 XDOT =        5636
641903
 YDOT =      -6998
754319  feet/sec       YDOT =       -2070
190065  meter/sec
 ZDOT =      15529
754464                 ZDOT =        4760
849720

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7325443
05                 X    =        -2232795
04
 Y    =      -18140461
19  feet           Y    =        -5529212
57  meter
 Z    =      -10627138
41                 Z    =        -3239151
79
 XDOT =      11962
775047                 XDOT =        3646
253834
 YDOT =     -13980
985634  feet/sec       YDOT =       -4261
404421  meter/sec
 ZDOT =      15649
061757                 ZDOT =        4769
834023


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   16120
47810519  
00016717  00000-0  10270-3 0  9002
2 25544  51
6400 301
0109 0001680  67
2165 292
9165 15
54367588 37404


Satellite: ISS
Catalog Number: 25544
Epoch time:      16120
47810519   =   yrday
fracday
Element set:     900
Inclination:       51
6400  deg
RA of node:       301
0109  deg
Eccentricity:     
0001680     
Arg of perigee:    67
2165  deg
Mean anomaly:     292
9165  deg
Mean motion:   15
54367588  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3740
Checksum:              290


Coasting Arc #2 (Orbit 3755)
---------------------------------------

Vector Time (GMT): 2016/121/11:18:49
007
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1571348
66                 A    =         6787342
80  meter
 Y    =        6389335
76  meter          E    =           
0014882
 Z    =        1639609
02                 I    =           51
32497
 XDOT =      -5137
916919                 Wp   =          111
27469
 YDOT =        206
405434  meter/sec      RA   =          295
32220  deg
 ZDOT =      -5691
859800                 TA   =           50
68313
                                          MA   =           50
55129
                                          Ha   =            221
053  n
mi
                                          Hp   =            213
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5155343
36                 X    =        -1650643
59
 Y    =       20962387
65  feet           Y    =         6371320
56  meter
 Z    =        5379294
69                 Z    =         1631783
03
 XDOT =     -16856
682805                 XDOT =       -5112
194332
 YDOT =        677
183183  feet/sec       YDOT =         149
093543  meter/sec
 ZDOT =     -18674
080709                 ZDOT =       -5716
756220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5144827
44                 X    =         1568143
40
 Y    =       20973972
38  feet           Y    =         6392866
78  meter
 Z    =        5344090
73                 Z    =         1628878
86
 XDOT =     -12976
475583                 XDOT =       -3955
229758
 YDOT =       7999
421457  feet/sec       YDOT =        2438
223660  meter/sec
 ZDOT =     -18782
229043                 ZDOT =       -5724
823412


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   16121
50677514  
00016717  00000-0  10270-3 0  9014
2 25544  51
6399 295
8814 0001595  60
7774 299
3538 15
54425857 37569


Satellite: ISS
Catalog Number: 25544
Epoch time:      16121
50677514   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:       295
8814  deg
Eccentricity:     
0001595     
Arg of perigee:    60
7774  deg
Mean anomaly:     299
3538  deg
Mean motion:   15
54425857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3756
Checksum:              347


Coasting Arc #3 (Orbit 3771)
---------------------------------------

Vector Time (GMT): 2016/122/11:18:49
007
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2442025
73                 A    =         6788574
53  meter
 Y    =       -6326441
63  meter          E    =           
0013810
 Z    =         115166
96                 I    =           51
31526
 XDOT =       4433
371861                 Wp   =           49
91274
 YDOT =       1828
771612  meter/sec      RA   =          290
32759  deg
 ZDOT =       5985
360405                 TA   =          311
33371
                                          MA   =          311
45246
                                          Ha   =            221
172  n
mi
                                          Hp   =            213
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8011895
43                 X    =         2512028
64
 Y    =      -20756042
08  feet           Y    =        -6298741
86  meter
 Z    =         377844
36                 Z    =          127200
03
 XDOT =      14545
183270                 XDOT =        4383
518048
 YDOT =       5999
906865  feet/sec       YDOT =        1878
069963  meter/sec
 ZDOT =      19637
009204                 ZDOT =        6006
775640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2931887
17                 X    =         -893639
21
 Y    =      -22053674
12  feet           Y    =        -6721959
87  meter
 Z    =         431292
16                 Z    =          131457
85
 XDOT =      13921
900948                 XDOT =        4243
395409
 YDOT =      -1438
676289  feet/sec       YDOT =        -438
508533  meter/sec
 ZDOT =      19729
655591                 ZDOT =        6013
599024


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   16122
53544190  
00016717  00000-0  10270-3 0  9022
2 25544  51
6393 290
7510 0001636  76
1971 283
9364 15
54386374 37720


Satellite: ISS
Catalog Number: 25544
Epoch time:      16122
53544190   =   yrday
fracday
Element set:     902
Inclination:       51
6393  deg
RA of node:       290
7510  deg
Eccentricity:     
0001636     
Arg of perigee:    76
1971  deg
Mean anomaly:     283
9364  deg
Mean motion:   15
54386374  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3772
Checksum:              316


Coasting Arc #4 (Orbit 3786)
---------------------------------------

Vector Time (GMT): 2016/123/11:18:49
007
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3143299
46                 A    =         6786890
42  meter
 Y    =        5704947
98  meter          E    =           
0007916
 Z    =       -1900976
73                 I    =           51
30010
 XDOT =      -3589
145674                 Wp   =          128
06674
 YDOT =      -3831
710699  meter/sec      RA   =          285
33209  deg
 ZDOT =      -5585
185512                 TA   =           72
97092
                                          MA   =           72
88420
                                          Ha   =            221
168  n
mi
                                          Hp   =            213
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10312662
25                 X    =        -3197625
77
 Y    =       18717020
92  feet           Y    =         5669493
68  meter
 Z    =       -6236800
30                 Z    =        -1916378
44
 XDOT =     -11775
412316                 XDOT =       -3518
901072
 YDOT =     -12571
229329  feet/sec       YDOT =       -3871
454385  meter/sec
 ZDOT =     -18324
099448                 ZDOT =       -5602
450084

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         335031
69                 X    =          102117
66
 Y    =       21347446
57  feet           Y    =         6506701
72  meter
 Z    =       -6304746
75                 Z    =        -1921686
81
 XDOT =     -14794
826901                 XDOT =       -4509
463239
 YDOT =      -5181
723633  feet/sec       YDOT =       -1579
389363  meter/sec
 ZDOT =     -18398
350571                 ZDOT =       -5607
817254


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   16123
49980749  
00016717  00000-0  10270-3 0  9033
2 25544  51
6396 285
9415 0001861  74
3744 285
7614 15
54427235 37877


Satellite: ISS
Catalog Number: 25544
Epoch time:      16123
49980749   =   yrday
fracday
Element set:     903
Inclination:       51
6396  deg
RA of node:       285
9415  deg
Eccentricity:     
0001861     
Arg of perigee:    74
3744  deg
Mean anomaly:     285
7614  deg
Mean motion:   15
54427235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3787
Checksum:              344


Coasting Arc #5 (Orbit 3796)
---------------------------------------

Vector Time (GMT): 2016/124/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4149651
46                 A    =         6776500
79  meter
 Y    =         865029
97  meter          E    =           
0004129
 Z    =        5283517
45                 I    =           51
26142
 XDOT =      -1599
043589                 Wp   =           81
48932
 YDOT =       7504
091398  meter/sec      RA   =          282
19622  deg
 ZDOT =         27
876616                 TA   =            8
24719
                                          MA   =            8
24040
                                          Ha   =            221
021  n
mi
                                          Hp   =            213
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13614342
05                 X    =         4114004
70
 Y    =        2838024
83  feet           Y    =          911235
06  meter
 Z    =       17334374
85                 Z    =         5303589
04
 XDOT =      -5246
206001                 XDOT =       -1682
972783
 YDOT =      24619
722436  feet/sec       YDOT =        7485
740554  meter/sec
 ZDOT =         91
458713                 ZDOT =          19
904572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6330029
44                 X    =        -1929392
97
 Y    =       12260172
00  feet           Y    =         3736900
43  meter
 Z    =       17421370
65                 Z    =         5310033
78
 XDOT =     -21442
115633                 XDOT =       -6535
556845
 YDOT =     -11146
829936  feet/sec       YDOT =       -3397
553765  meter/sec
 ZDOT =         55
446227                 ZDOT =          16
900010


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   16124
14271543  
00016717  00000-0  10270-3 0  9042
2 25544  51
6408 282
7390 0001797  69
3939 290
7406 15
54418028 37972


Satellite: ISS
Catalog Number: 25544
Epoch time:      16124
14271543   =   yrday
fracday
Element set:     904
Inclination:       51
6408  deg
RA of node:       282
7390  deg
Eccentricity:     
0001797     
Arg of perigee:    69
3939  deg
Mean anomaly:     290
7406  deg
Mean motion:   15
54418028  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3797
Checksum:              328


Coasting Arc #6 (Orbit 3811)
---------------------------------------

Vector Time (GMT): 2016/125/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3696714
72                 A    =         6777843
43  meter
 Y    =       -2728492
98  meter          E    =           
0014369
 Z    =       -4995953
26                 I    =           51
25992
 XDOT =       2475
796748                 Wp   =          101
11537
 YDOT =      -6971
499703  meter/sec      RA   =          277
16730  deg
 ZDOT =       1977
610918                 TA   =          188
20774
                                          MA   =          188
23127
                                          Ha   =            221
174  n
mi
                                          Hp   =            213
453

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12128329
12                 X    =        -3641660
69
 Y    =       -8951748
63  feet           Y    =        -2769524
51  meter
 Z    =      -16390922
76                 Z    =        -5013777
42
 XDOT =       8122
692743                 XDOT =        2543
963253
 YDOT =     -22872
374355  feet/sec       YDOT =       -6943
432467  meter/sec
 ZDOT =       6488
224796                 ZDOT =        1989
803794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11669372
72                 X    =         3556824
81
 Y    =       -9408999
31  feet           Y    =        -2867862
99  meter
 Z    =      -16467816
86                 Z    =        -5019390
58
 XDOT =      19446
717066                 XDOT =        5927
359362
 YDOT =      12679
985695  feet/sec       YDOT =        3864
859640  meter/sec
 ZDOT =       6542
454927                 ZDOT =        1994
140262


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   16125
10707196  
00016717  00000-0  10270-3 0  9058
2 25544  51
6407 277
9293 0001778  74
2200 285
9149 15
54413351 38126


Satellite: ISS
Catalog Number: 25544
Epoch time:      16125
10707196   =   yrday
fracday
Element set:     905
Inclination:       51
6407  deg
RA of node:       277
9293  deg
Eccentricity:     
0001778     
Arg of perigee:    74
2200  deg
Mean anomaly:     285
9149  deg
Mean motion:   15
54413351  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3812
Checksum:              308


Coasting Arc #7 (Orbit 3827)
---------------------------------------

Vector Time (GMT): 2016/126/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3126458
93                 A    =         6781236
22  meter
 Y    =        4396289
88  meter          E    =           
0012204
 Z    =        4100674
11                 I    =           51
26931
 XDOT =      -3246
519894                 Wp   =           76
07542
 YDOT =       5839
098557  meter/sec      RA   =          272
14571  deg
 ZDOT =      -3772
450634                 TA   =           53
05214
                                          MA   =           52
94045
                                          Ha   =            221
062  n
mi
                                          Hp   =            213
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10257411
18                 X    =         3057146
44
 Y    =       14423523
24  feet           Y    =         4430864
62  meter
 Z    =       13453655
21                 Z    =         4115693
47
 XDOT =     -10651
311988                 XDOT =       -3293
247553
 YDOT =      19157
147498  feet/sec       YDOT =        5802
532416  meter/sec
 ZDOT =     -12376
806541                 ZDOT =       -3788
335424

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16395936
73                 X    =        -4997481
52
 Y    =        6533638
61  feet           Y    =         1991453
05  meter
 Z    =       13518068
30                 Z    =         4120307
22
 XDOT =     -15692
710581                 XDOT =       -4783
138185
 YDOT =     -13544
352597  feet/sec       YDOT =       -4128
318671  meter/sec
 ZDOT =     -12446
852123                 ZDOT =       -3793
800527


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   16126
13570986  
00016717  00000-0  10270-3 0  9068
2 25544  51
6417 272
7994 0001736  74
7116 285
4228 15
54432508 38288


Satellite: ISS
Catalog Number: 25544
Epoch time:      16126
13570986   =   yrday
fracday
Element set:     906
Inclination:       51
6417  deg
RA of node:       272
7994  deg
Eccentricity:     
0001736     
Arg of perigee:    74
7116  deg
Mean anomaly:     285
4228  deg
Mean motion:   15
54432508  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3828
Checksum:              330


Coasting Arc #8 (Orbit 3842)
---------------------------------------

Vector Time (GMT): 2016/127/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2494077
29                 A    =         6785187
75  meter
 Y    =       -5678314
08  meter          E    =           
0006526
 Z    =       -2753212
54                 I    =           51
28214
 XDOT =       3892
138403                 Wp   =           63
55150
 YDOT =      -4181
091046  meter/sec      RA   =          267
13507  deg
 ZDOT =       5109
692901                 TA   =          265
11425
                                          MA   =          265
18876
                                          Ha   =            221
147  n
mi
                                          Hp   =            213
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8182668
28                 X    =        -2417021
38
 Y    =      -18629639
38  feet           Y    =        -5705773
70  meter
 Z    =       -9032849
53                 Z    =        -2765141
18
 XDOT =      12769
482948                 XDOT =        3913
781885
 YDOT =     -13717
490307  feet/sec       YDOT =       -4137
445485  meter/sec
 ZDOT =      16764
084320                 ZDOT =        5128
652984

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19945550
46                 X    =         6079403
78
 Y    =       -3908308
52  feet           Y    =        -1191252
44  meter
 Z    =       -9083613
58                 Z    =        -2768685
42
 XDOT =      10372
244866                 XDOT =        3161
460235
 YDOT =      13870
674633  feet/sec       YDOT =        4227
781628  meter/sec
 ZDOT =      16847
177901                 ZDOT =        5135
019824


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   16127
10005055  
00016717  00000-0  10270-3 0  9077
2 25544  51
6415 267
9900 0001818  76
2190 283
9166 15
54433607 38431


Satellite: ISS
Catalog Number: 25544
Epoch time:      16127
10005055   =   yrday
fracday
Element set:     907
Inclination:       51
6415  deg
RA of node:       267
9900  deg
Eccentricity:     
0001818     
Arg of perigee:    76
2190  deg
Mean anomaly:     283
9166  deg
Mean motion:   15
54433607  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3843
Checksum:              302


Coasting Arc #9 (Orbit 3858)
---------------------------------------

Vector Time (GMT): 2016/128/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1737141
86                 A    =         6787952
77  meter
 Y    =        6471685
73  meter          E    =           
0014966
 Z    =        1042398
38                 I    =           51
29489
 XDOT =      -4449
245471                 Wp   =          118
96775
 YDOT =       2148
470212  meter/sec      RA   =          262
13545  deg
 ZDOT =      -5867
203663                 TA   =           49
67208
                                          MA   =           49
54143
                                          Ha   =            221
141  n
mi
                                          Hp   =            213
509

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5699284
31                 X    =         1659581
10
 Y    =       21232564
73  feet           Y    =         6490677
92  meter
 Z    =        3419942
18                 Z    =         1050648
87
 XDOT =     -14597
262043                 XDOT =       -4444
438531
 YDOT =       7048
786785  feet/sec       YDOT =        2098
742747  meter/sec
 ZDOT =     -19249
355850                 ZDOT =       -5888
805767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21938209
76                 X    =        -6686766
34
 Y    =        1334303
56  feet           Y    =          406695
72  meter
 Z    =        3454596
59                 Z    =         1052961
04
 XDOT =      -3925
806639                 XDOT =       -1196
585864
 YDOT =     -13986
923267  feet/sec       YDOT =       -4263
214212  meter/sec
 ZDOT =     -19343
554382                 ZDOT =       -5895
915376


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   16128
12867404  
00016717  00000-0  10270-3 0  9085
2 25544  51
6424 262
8603 0001789  80
9589 279
1766 15
54441261 38591


Satellite: ISS
Catalog Number: 25544
Epoch time:      16128
12867404   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:       262
8603  deg
Eccentricity:     
0001789     
Arg of perigee:    80
9589  deg
Mean anomaly:     279
1766  deg
Mean motion:   15
54441261  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3859
Checksum:              340


Coasting Arc #10 (Orbit 3874)
---------------------------------------

Vector Time (GMT): 2016/129/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -904366
79                 A    =         6788149
68  meter
 Y    =       -6678306
48  meter          E    =           
0014854
 Z    =         754785
02                 I    =           51
30118
 XDOT =       4872
331815                 Wp   =           56
22358
 YDOT =         18
352381  meter/sec      RA   =          257
14029  deg
 ZDOT =       5924
275973                 TA   =          311
97557
                                          MA   =          312
10201
                                          Ha   =            221
103  n
mi
                                          Hp   =            213
521

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2967082
65                 X    =         -833287
58
 Y    =      -21910454
34  feet           Y    =        -6688022
31  meter
 Z    =        2476328
82                 Z    =          750564
14
 XDOT =      15985
340602                 XDOT =        4842
986316
 YDOT =         60
211225  feet/sec       YDOT =          72
673732  meter/sec
 ZDOT =      19436
600961                 ZDOT =        5947
873738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22086880
10                 X    =         6732081
05
 Y    =        1061054
70  feet           Y    =          323409
47  meter
 Z    =        2459203
81                 Z    =          749565
32
 XDOT =      -2874
719469                 XDOT =        -876
214494
 YDOT =      13972
264711  feet/sec       YDOT =        4258
746284  meter/sec
 ZDOT =      19539
080051                 ZDOT =        5955
511600


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   16129
15728903  
00016717  00000-0  10270-3 0  9090
2 25544  51
6427 257
7305 0001738  80
6646 279
4703 15
54453629 38754


Satellite: ISS
Catalog Number: 25544
Epoch time:      16129
15728903   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:       257
7305  deg
Eccentricity:     
0001738     
Arg of perigee:    80
6646  deg
Mean anomaly:     279
4703  deg
Mean motion:   15
54453629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3875
Checksum:              338


Coasting Arc #11 (Orbit 3889)
---------------------------------------

Vector Time (GMT): 2016/130/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -80088
82                 A    =         6785652
60  meter
 Y    =        6304378
04  meter          E    =           
0006610
 Z    =       -2508410
75                 I    =           51
30222
 XDOT =      -5130
232313                 Wp   =          119
51441
 YDOT =      -2156
583891  meter/sec      RA   =          252
14265  deg
 ZDOT =      -5270
035892                 TA   =           88
75767
                                          MA   =           88
68194
                                          Ha   =            221
082  n
mi
                                          Hp   =            213
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -262758
58                 X    =         -138395
02
 Y    =       20683654
99  feet           Y    =         6303156
56  meter
 Z    =       -8229694
07                 Z    =        -2508941
09
 XDOT =     -16831
470844                 XDOT =       -5080
135594
 YDOT =      -7075
406466  feet/sec       YDOT =       -2213
673169  meter/sec
 ZDOT =     -17290
144003                 ZDOT =       -5294
836109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20363502
08                 X    =        -6206795
43
 Y    =       -3626824
94  feet           Y    =        -1105456
24  meter
 Z    =       -8233129
07                 Z    =        -2509457
74
 XDOT =       9479
764451                 XDOT =        2889
432205
 YDOT =     -13834
558053  feet/sec       YDOT =       -4216
773295  meter/sec
 ZDOT =     -17397
471177                 ZDOT =       -5302
749215


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   16130
12160514  
00016717  00000-0  10270-3 0  9109
2 25544  51
6438 252
9215 0001737  83
8053 276
3298 15
54473355 38909


Satellite: ISS
Catalog Number: 25544
Epoch time:      16130
12160514   =   yrday
fracday
Element set:     910
Inclination:       51
6438  deg
RA of node:       252
9215  deg
Eccentricity:     
0001737     
Arg of perigee:    83
8053  deg
Mean anomaly:     276
3298  deg
Mean motion:   15
54473355  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3890
Checksum:              302


Coasting Arc #12 (Orbit 3905)
---------------------------------------

Vector Time (GMT): 2016/131/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1138668
93                 A    =         6781709
72  meter
 Y    =       -5401827
57  meter          E    =           
0012846
 Z    =        3929299
70                 I    =           51
29895
 XDOT =       5172
415156                 Wp   =           98
07233
 YDOT =       4011
696535  meter/sec      RA   =          247
13569  deg
 ZDOT =       4003
166423                 TA   =          309
91790
                                          MA   =          310
03073
                                          Ha   =            221
065  n
mi
                                          Hp   =            213
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3735790
45                 X    =         1179901
82
 Y    =      -17722531
40  feet           Y    =        -5388863
90  meter
 Z    =       12891403
22                 Z    =         3934930
97
 XDOT =      16969
865999                 XDOT =        5107
725058
 YDOT =      13161
734039  feet/sec       YDOT =        4069
175981  meter/sec
 ZDOT =      13133
748106                 ZDOT =        4028
136122

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16983290
33                 X    =         5176506
89
 Y    =        6241472
47  feet           Y    =         1902400
81  meter
 Z    =       12916826
13                 Z    =         3937048
61
 XDOT =     -15067
236762                 XDOT =       -4592
493765
 YDOT =      13506
785662  feet/sec       YDOT =        4116
868270  meter/sec
 ZDOT =      13241
494859                 ZDOT =        4036
007633


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   16131
15020148  
00016717  00000-0  10270-3 0  9112
2 25544  51
6429 247
7918 0001825  85
8193 274
3168 15
54485550 39068


Satellite: ISS
Catalog Number: 25544
Epoch time:      16131
15020148   =   yrday
fracday
Element set:     911
Inclination:       51
6429  deg
RA of node:       247
7918  deg
Eccentricity:     
0001825     
Arg of perigee:    85
8193  deg
Mean anomaly:     274
3168  deg
Mean motion:   15
54485550  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3906
Checksum:              314


Coasting Arc #13 (Orbit 3920)
---------------------------------------

Vector Time (GMT): 2016/132/02:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2293985
59                 A    =         6777888
29  meter
 Y    =        4081650
45  meter          E    =           
0013820
 Z    =       -4913612
15                 I    =           51
30044
 XDOT =      -4903
437885                 Wp   =           75
28271
 YDOT =      -5442
123004  meter/sec      RA   =          242
11780  deg
 ZDOT =      -2233
277865                 TA   =          172
78558
                                          MA   =          172
76567
                                          Ha   =            220
965  n
mi
                                          Hp   =            213
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7526199
45                 X    =        -2315588
74
 Y    =       13391241
63  feet           Y    =         4055877
05  meter
 Z    =      -16120774
78                 Z    =        -4924808
10
 XDOT =     -16087
394636                 XDOT =       -4831
369885
 YDOT =     -17854
734265  feet/sec       YDOT =       -5496
553431  meter/sec
 ZDOT =      -7327
027115                 ZDOT =       -2256
922974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12299015
46                 X    =        -3748739
91
 Y    =       -9116438
24  feet           Y    =        -2778690
38  meter
 Z    =      -16170132
41                 Z    =        -4928656
36
 XDOT =      19142
493628                 XDOT =        5834
632058
 YDOT =     -12659
178943  feet/sec       YDOT =       -3858
517742  meter/sec
 ZDOT =      -7428
784928                 ZDOT =       -2264
293646


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   16132
11450067  
00016717  00000-0  10270-3 0  9127
2 25544  51
6434 242
9830 0001644  86
8755 273
2586 15
54528648 39213


Satellite: ISS
Catalog Number: 25544
Epoch time:      16132
11450067   =   yrday
fracday
Element set:     912
Inclination:       51
6434  deg
RA of node:       242
9830  deg
Eccentricity:     
0001644     
Arg of perigee:    86
8755  deg
Mean anomaly:     273
2586  deg
Mean motion:   15
54528648  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3921
Checksum:              314


Coasting Arc #14 (Orbit 3927)
---------------------------------------

Vector Time (GMT): 2016/132/13:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4693657
24                 A    =         6785846
96  meter
 Y    =       -4291994
05  meter          E    =           
0006602
 Z    =       -2364249
57                 I    =           51
33348
 XDOT =       1981
951874                 Wp   =           57
48093
 YDOT =      -5110
605957  meter/sec      RA   =          239
74529  deg
 ZDOT =       5357
401595                 TA   =          276
01547
                                          MA   =          276
09071
                                          Ha   =            220
949  n
mi
                                          Hp   =            213
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15399137
92                 X    =        -4633829
66
 Y    =      -14081345
31  feet           Y    =        -4344147
02  meter
 Z    =       -7756724
32                 Z    =        -2386905
23
 XDOT =       6502
466778                 XDOT =        2012
928527
 YDOT =     -16767
079913  feet/sec       YDOT =       -5088
269514  meter/sec
 ZDOT =      17576
776888                 ZDOT =        5367
104474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18412855
90                 X    =        -5612238
48
 Y    =        9739595
62  feet           Y    =         2968628
74  meter
 Z    =       -7854395
03                 Z    =        -2394019
61
 XDOT =     -12943
010903                 XDOT =       -3945
029723
 YDOT =     -10297
374205  feet/sec       YDOT =       -3138
639658  meter/sec
 ZDOT =      17619
827719                 ZDOT =        5370
523489


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   16132
56450341  
00016717  00000-0  10270-3 0  9132
2 25544  51
6430 240
7356 0001516 100
4191 259
7132 15
54488691 39289


Satellite: ISS
Catalog Number: 25544
Epoch time:      16132
56450341   =   yrday
fracday
Element set:     913
Inclination:       51
6430  deg
RA of node:       240
7356  deg
Eccentricity:     
0001516     
Arg of perigee:   100
4191  deg
Mean anomaly:     259
7132  deg
Mean motion:   15
54488691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3928
Checksum:              295


Coasting Arc #15 (Orbit 3943)
---------------------------------------

Vector Time (GMT): 2016/133/13:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4267648
80                 A    =         6788033
31  meter
 Y    =        5238277
87  meter          E    =           
0014675
 Z    =         577882
04                 I    =           51
35721
 XDOT =      -3400
161543                 Wp   =          126
03058
 YDOT =       3437
805431  meter/sec      RA   =          234
75112  deg
 ZDOT =      -5954
637088                 TA   =           47
70571
                                          MA   =           47
58141
                                          Ha   =            220
980  n
mi
                                          Hp   =            213
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14001472
44                 X    =         4205948
77
 Y    =       17185951
01  feet           Y    =         5285656
55  meter
 Z    =        1895938
44                 Z    =          598463
63
 XDOT =     -11155
385639                 XDOT =       -3409
426035
 YDOT =      11278
889210  feet/sec       YDOT =        3399
730971  meter/sec
 ZDOT =     -19536
210918                 ZDOT =       -5971
176683

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20750687
19                 X    =         6324809
46
 Y    =       -7775838
35  feet           Y    =        -2370075
53  meter
 Z    =        1984450
59                 Z    =          604860
54
 XDOT =       6602
570663                 XDOT =        2012
463538
 YDOT =      12537
333941  feet/sec       YDOT =        3821
379385  meter/sec
 ZDOT =     -19608
670036                 ZDOT =       -5976
722627


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   16133
59307640  
00016717  00000-0  10270-3 0  9140
2 25544  51
6422 235
6057 0001705 104
2392 255
8950 15
54521796 39443


Satellite: ISS
Catalog Number: 25544
Epoch time:      16133
59307640   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       235
6057  deg
Eccentricity:     
0001705     
Arg of perigee:   104
2392  deg
Mean anomaly:     255
8950  deg
Mean motion:   15
54521796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3944
Checksum:              307


Coasting Arc #16 (Orbit 3959)
---------------------------------------

Vector Time (GMT): 2016/134/13:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3500049
42                 A    =         6787543
82  meter
 Y    =       -5673298
11  meter          E    =           
0014965
 Z    =        1242929
01                 I    =           51
37458
 XDOT =       4720
165124                 Wp   =           63
29155
 YDOT =      -1625
674576  meter/sec      RA   =          229
76028  deg
 ZDOT =       5823
781476                 TA   =          310
27777
                                          MA   =          310
40851
                                          Ha   =            220
972  n
mi
                                          Hp   =            213
453

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11483101
76                 X    =        -3442386
69
 Y    =      -18613182
78  feet           Y    =        -5712115
61  meter
 Z    =        4077851
08                 Z    =         1226066
50
 XDOT =      15486
106051                 XDOT =        4709
703459
 YDOT =      -5333
578006  feet/sec       YDOT =       -1572
949167  meter/sec
 ZDOT =      19106
894606                 ZDOT =        5846
685518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21223114
73                 X    =        -6468805
37
 Y    =        5336289
58  feet           Y    =         1626501
06  meter
 Z    =        4005556
59                 Z    =         1220893
65
 XDOT =        -43
152117                 XDOT =         -13
152765
 YDOT =     -14708
334805  feet/sec       YDOT =       -4483
100449  meter/sec
 ZDOT =      19206
697260                 ZDOT =        5854
201325


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   16134
62164042  
00016717  00000-0  10270-3 0  9153
2 25544  51
6419 230
4755 0001681 104
0276 256
1064 15
54526688 39602


Satellite: ISS
Catalog Number: 25544
Epoch time:      16134
62164042   =   yrday
fracday
Element set:     915
Inclination:       51
6419  deg
RA of node:       230
4755  deg
Eccentricity:     
0001681     
Arg of perigee:   104
0276  deg
Mean anomaly:     256
1064  deg
Mean motion:   15
54526688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3960
Checksum:              299


Coasting Arc #17 (Orbit 3970)
---------------------------------------

Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926503
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3607157
02                 A    =         6776275
57  meter
 Y    =        2321022
06  meter          E    =           
0016451
 Z    =       -5260265
09                 I    =           51
35113
 XDOT =      -4856
812643                 Wp   =           97
20040
 YDOT =      -5873
247428  meter/sec      RA   =          225
96422  deg
 ZDOT =        738
973550                 TA   =          179
89816
                                          MA   =          179
89782
                                          Ha   =            220
983  n
mi
                                          Hp   =            213
192

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11834504
67                 X    =        -3607290
94
 Y    =        7614901
78  feet           Y    =         2280683
75  meter
 Z    =      -17258087
57                 Z    =        -5277788
15
 XDOT =     -15934
424681                 XDOT =       -4794
365187
 YDOT =     -19269
184476  feet/sec       YDOT =       -5927
210384  meter/sec
 ZDOT =       2424
453903                 ZDOT =         715
531844

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13322012
29                 X    =        -4060549
35
 Y    =        4233010
91  feet           Y    =         1290221
73  meter
 Z    =      -17334630
76                 Z    =        -5283595
46
 XDOT =      -9962
012256                 XDOT =       -3036
421336
 YDOT =     -21836
419789  feet/sec       YDOT =       -6655
740752  meter/sec
 ZDOT =       2323
591921                 ZDOT =         708
230818


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   16135
32877328  
00016717  00000-0  10270-3 0  9160
2 25544  51
6398 226
9463 0001872 107
9203 252
2154 15
54557783 39717


Satellite: ISS
Catalog Number: 25544
Epoch time:      16135
32877328   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:       226
9463  deg
Eccentricity:     
0001872     
Arg of perigee:   107
9203  deg
Mean anomaly:     252
2154  deg
Mean motion:   15
54557783  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3971
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