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

 
Date: September 9th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


254/00:50:05 163 3 7 3 8 3 8
N/A -0 3 -0 4 220 7
000/00:10:10 325 0 8 0 1 217 3

257/20:34:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 1
000/00:00:00 000 0 0 0 0 216 6

265/22:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 215 0

Coasting Arc #1 (Orbit 1809)
---------------------------------------

Vector Time (GMT): 2016/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893582
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6480302
65                 A    =         6787575
65  meter
 Y    =        1454900
31  meter          E    =           
0010839
 Z    =        1375998
93                 I    =           51
64464
 XDOT =      -2244
747498                 Wp   =          116
92155
 YDOT =      -4476
822344  meter/sec      RA   =          356
78222  deg
 ZDOT =      -5807
700770                 TA   =           48
08524
                                          MA   =           47
99286
                                          Ha   =            219
827  n
mi
                                          Hp   =            214
996

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21260835
47                 X    =        -6502774
10
 Y    =        4773294
97  feet           Y    =         1382307
67  meter
 Z    =        4514432
20                 Z    =         1344464
54
 XDOT =      -7364
657145                 XDOT =       -2166
308365
 YDOT =     -14687
737349  feet/sec       YDOT =       -4501
486448  meter/sec
 ZDOT =     -19054
136385                 ZDOT =       -5818
414362

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21816350
53                 X    =         6649623
64
 Y    =        -285818
72  feet           Y    =          -87117
54  meter
 Z    =        4376382
66                 Z    =         1333921
44
 XDOT =       4039
199351                 XDOT =        1231
147962
 YDOT =      14275
166439  feet/sec       YDOT =        4351
070730  meter/sec
 ZDOT =     -19100
072221                 ZDOT =       -5821
702013


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   16253
53476751  
00016717  00000-0  10270-3 0  9002
2 25544  51
6439 357
1826 0003028 310
6236  49
4654 15
54472553 18109


Satellite: ISS
Catalog Number: 25544
Epoch time:      16253
53476751   =   yrday
fracday
Element set:     900
Inclination:       51
6439  deg
RA of node:       357
1826  deg
Eccentricity:     
0003028     
Arg of perigee:   310
6236  deg
Mean anomaly:      49
4654  deg
Mean motion:   15
54472553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1810
Checksum:              305


Coasting Arc #2 (Orbit 1817)
---------------------------------------

Vector Time (GMT): 2016/254/00:55:10
325
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2930507
17                 A    =         6781380
35  meter
 Y    =       -3995590
57  meter          E    =           
0004420
 Z    =       -4633651
88                 I    =           51
59994
 XDOT =       6883
417321                 Wp   =           92
36816
 YDOT =       1634
805961  meter/sec      RA   =          354
08975  deg
 ZDOT =       2945
910305                 TA   =          206
99347
                                          MA   =          207
01647
                                          Ha   =            220
706  n
mi
                                          Hp   =            217
269

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9614524
83                 X    =         2997477
36
 Y    =      -13108892
95  feet           Y    =        -3962445
54  meter
 Z    =      -15202269
96                 Z    =        -4619253
29
 XDOT =      22583
390160                 XDOT =        6850
314954
 YDOT =       5363
536619  feet/sec       YDOT =        1711
596056  meter/sec
 ZDOT =       9665
060055                 ZDOT =        2979
267701

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9146655
96                 X    =         2787900
74
 Y    =      -13511214
22  feet           Y    =        -4118218
10  meter
 Z    =      -15138591
39                 Z    =        -4614242
66
 XDOT =      21742
797465                 XDOT =        6627
204667
 YDOT =       3735
378601  feet/sec       YDOT =        1138
543397  meter/sec
 ZDOT =       9810
470327                 ZDOT =        2990
231356


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   16254
04906591  
00016717  00000-0  10270-3 0  9010
2 25544  51
6442 354
6202 0006164 302
1508  57
9052 15
53759898 18188


Satellite: ISS
Catalog Number: 25544
Epoch time:      16254
04906591   =   yrday
fracday
Element set:     901
Inclination:       51
6442  deg
RA of node:       354
6202  deg
Eccentricity:     
0006164     
Arg of perigee:   302
1508  deg
Mean anomaly:      57
9052  deg
Mean motion:   15
53759898  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1818
Checksum:              312


Coasting Arc #3 (Orbit 1833)
---------------------------------------

Vector Time (GMT): 2016/255/00:55:10
325
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4303840
28                 A    =         6784871
00  meter
 Y    =        3771465
83  meter          E    =           
0008148
 Z    =        3643265
54                 I    =           51
57934
 XDOT =      -5819
711578                 Wp   =           57
51075
 YDOT =      -2409
066465  meter/sec      RA   =          349
10197  deg
 ZDOT =      -4369
644811                 TA   =           79
21602
                                          MA   =           79
12430
                                          Ha   =            220
835  n
mi
                                          Hp   =            217
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14120210
88                 X    =        -4363391
26
 Y    =       12373575
55  feet           Y    =         3723004
67  meter
 Z    =       11952970
93                 Z    =         3622213
74
 XDOT =     -19093
541921                 XDOT =       -5771
114456
 YDOT =      -7903
761367  feet/sec       YDOT =       -2473
874936  meter/sec
 ZDOT =     -14336
105022                 ZDOT =       -4397
797242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13433376
68                 X    =        -4094493
21
 Y    =       13199905
28  feet           Y    =         4023331
13  meter
 Z    =       11860275
41                 Z    =         3615011
95
 XDOT =     -18475
774491                 XDOT =       -5631
416065
 YDOT =      -5777
374557  feet/sec       YDOT =       -1760
943765  meter/sec
 ZDOT =     -14458
621910                 ZDOT =       -4406
987958


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   16255
07814347  
00016717  00000-0  10270-3 0  9022
2 25544  51
6439 349
4943 0006160 305
4428  54
6149 15
53757875 18343


Satellite: ISS
Catalog Number: 25544
Epoch time:      16255
07814347   =   yrday
fracday
Element set:     902
Inclination:       51
6439  deg
RA of node:       349
4943  deg
Eccentricity:     
0006160     
Arg of perigee:   305
4428  deg
Mean anomaly:      54
6149  deg
Mean motion:   15
53757875  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1834
Checksum:              329


Coasting Arc #4 (Orbit 1848)
---------------------------------------

Vector Time (GMT): 2016/256/00:55:10
325
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5352930
84                 A    =         6788040
82  meter
 Y    =       -3449746
46  meter          E    =           
0008195
 Z    =       -2334954
02                 I    =           51
56032
 XDOT =       4411
993014                 Wp   =          354
09346
 YDOT =       3197
855368  meter/sec      RA   =          344
11897  deg
 ZDOT =       5396
246085                 TA   =          339
83446
                                          MA   =          339
86681
                                          Ha   =            220
993  n
mi
                                          Hp   =            216
943

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17562109
07                 X    =         5402451
08
 Y    =      -11318065
80  feet           Y    =        -3389609
68  meter
 Z    =       -7660610
30                 Z    =        -2308830
44
 XDOT =      14475
042697                 XDOT =        4349
693376
 YDOT =      10491
651470  feet/sec       YDOT =        3246
845269  meter/sec
 ZDOT =      17704
219438                 ZDOT =        5417
526784

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16689438
42                 X    =         5086940
83
 Y    =      -12638605
89  feet           Y    =        -3852247
08  meter
 Z    =       -7545828
32                 Z    =        -2299968
47
 XDOT =      14202
470917                 XDOT =        4328
913136
 YDOT =       8141
681451  feet/sec       YDOT =        2481
584506  meter/sec
 ZDOT =      17796
563071                 ZDOT =        5424
392424


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   16256
04289205  
00016717  00000-0  10270-3 0  9030
2 25544  51
6453 344
6871 0006304 309
2788  50
7805 15
53799495 18493


Satellite: ISS
Catalog Number: 25544
Epoch time:      16256
04289205   =   yrday
fracday
Element set:     903
Inclination:       51
6453  deg
RA of node:       344
6871  deg
Eccentricity:     
0006304     
Arg of perigee:   309
2788  deg
Mean anomaly:      50
7805  deg
Mean motion:   15
53799495  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1849
Checksum:              337


Coasting Arc #5 (Orbit 1864)
---------------------------------------

Vector Time (GMT): 2016/257/00:55:10
325
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6046622
63                 A    =         6790127
47  meter
 Y    =        2978575
38  meter          E    =           
0007171
 Z    =         793733
34                 I    =           51
53584
 XDOT =      -2752
191834                 Wp   =          121
11450
 YDOT =      -3996
101898  meter/sec      RA   =          339
14282  deg
 ZDOT =      -5934
090006                 TA   =           50
29564
                                          MA   =           50
23244
                                          Ha   =            221
115  n
mi
                                          Hp   =            216
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19838000
74                 X    =        -6083336
00
 Y    =        9772228
95  feet           Y    =         2910752
79  meter
 Z    =        2604112
00                 Z    =          764271
16
 XDOT =      -9029
500767                 XDOT =       -2678
476821
 YDOT =     -13110
570530  feet/sec       YDOT =       -4026
467084  meter/sec
 ZDOT =     -19468
799233                 ZDOT =       -5947
279984

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18848097
81                 X    =        -5744900
21
 Y    =       11595192
07  feet           Y    =         3534214
54  meter
 Z    =        2474845
70                 Z    =          754332
97
 XDOT =      -9250
757699                 XDOT =       -2819
630947
 YDOT =     -10843
063797  feet/sec       YDOT =       -3304
965845  meter/sec
 ZDOT =     -19525
648096                 ZDOT =       -5951
417540


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   16257
07194931  
00016717  00000-0  10270-3 0  9046
2 25544  51
6448 339
5610 0006181 313
2525  46
8111 15
53770308 18654


Satellite: ISS
Catalog Number: 25544
Epoch time:      16257
07194931   =   yrday
fracday
Element set:     904
Inclination:       51
6448  deg
RA of node:       339
5610  deg
Eccentricity:     
0006181     
Arg of perigee:   313
2525  deg
Mean anomaly:      46
8111  deg
Mean motion:   15
53770308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1865
Checksum:              304


Coasting Arc #6 (Orbit 1877)
---------------------------------------

Vector Time (GMT): 2016/257/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3442275
79                 A    =         6779088
66  meter
 Y    =        2867246
39  meter          E    =           
0001717
 Z    =        5087639
53                 I    =           51
47285
 XDOT =      -6102
468867                 Wp   =          349
42495
 YDOT =       4323
206568  meter/sec      RA   =          335
07640  deg
 ZDOT =       1694
215911                 TA   =           84
18008
                                          MA   =           84
16051
                                          Ha   =            221
078  n
mi
                                          Hp   =            216
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11293555
73                 X    =         3385244
32
 Y    =        9406976
36  feet           Y    =         2905421
86  meter
 Z    =       16691730
74                 Z    =         5104222
29
 XDOT =     -20021
223316                 XDOT =       -6158
588216
 YDOT =      14183
748584  feet/sec       YDOT =        4254
651059  meter/sec
 ZDOT =       5558
451150                 ZDOT =        1664
435159

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2327260
44                 X    =         -709348
98
 Y    =       14429639
02  feet           Y    =         4398153
97  meter
 Z    =       16763617
06                 Z    =         5109550
48
 XDOT =     -21419
896924                 XDOT =       -6528
784582
 YDOT =      -9753
495242  feet/sec       YDOT =       -2972
865350  meter/sec
 ZDOT =       5427
545417                 ZDOT =        1654
315843


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   16257
90804893  
00016717  00000-0  10270-3 0  9054
2 25544  51
6423 335
3943 0006394 316
1378  43
9267 15
53840896 18788


Satellite: ISS
Catalog Number: 25544
Epoch time:      16257
90804893   =   yrday
fracday
Element set:     905
Inclination:       51
6423  deg
RA of node:       335
3943  deg
Eccentricity:     
0006394     
Arg of perigee:   316
1378  deg
Mean anomaly:      43
9267  deg
Mean motion:   15
53840896  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1878
Checksum:              346


Coasting Arc #7 (Orbit 1892)
---------------------------------------

Vector Time (GMT): 2016/258/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2008757
81                 A    =         6778262
99  meter
 Y    =       -3723158
16  meter          E    =           
0011740
 Z    =       -5305274
41                 I    =           51
44142
 XDOT =       6679
720008                 Wp   =           66
36805
 YDOT =      -3748
389452  meter/sec      RA   =          330
06745  deg
 ZDOT =        106
187921                 TA   =          204
61964
                                          MA   =          204
67573
                                          Ha   =            221
320  n
mi
                                          Hp   =            216
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6590412
76                 X    =        -1941204
68
 Y    =      -12215085
82  feet           Y    =        -3745244
36  meter
 Z    =      -17405755
92                 Z    =        -5314867
84
 XDOT =      21915
091890                 XDOT =        6720
623191
 YDOT =     -12297
865657  feet/sec       YDOT =       -3673
463629  meter/sec
 ZDOT =        348
385568                 ZDOT =         138
735866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6950134
34                 X    =         2118400
95
 Y    =      -11954147
49  feet           Y    =        -3643624
15  meter
 Z    =      -17446953
65                 Z    =        -5317831
47
 XDOT =      21146
505075                 XDOT =        6445
454747
 YDOT =      11600
499616  feet/sec       YDOT =        3535
832283  meter/sec
 ZDOT =        491
254743                 ZDOT =         149
734446


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   16258
87277498  
00016717  00000-0  10270-3 0  9067
2 25544  51
6428 330
5873 0006392 320
4690  39
5996 15
53818626 18938


Satellite: ISS
Catalog Number: 25544
Epoch time:      16258
87277498   =   yrday
fracday
Element set:     906
Inclination:       51
6428  deg
RA of node:       330
5873  deg
Eccentricity:     
0006392     
Arg of perigee:   320
4690  deg
Mean anomaly:      39
5996  deg
Mean motion:   15
53818626  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1893
Checksum:              359


Coasting Arc #8 (Orbit 1908)
---------------------------------------

Vector Time (GMT): 2016/259/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         517282
63                 A    =         6779494
02  meter
 Y    =        4526236
77  meter          E    =           
0008595
 Z    =        5022215
17                 I    =           51
41822
 XDOT =      -6829
658272                 Wp   =            7
28383
 YDOT =       2911
410737  meter/sec      RA   =          325
05783  deg
 ZDOT =      -1911
718217                 TA   =          101
36628
                                          MA   =          101
26971
                                          Ha   =            221
536  n
mi
                                          Hp   =            216
209

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1697121
50                 X    =          442235
03
 Y    =       14849858
17  feet           Y    =         4531602
44  meter
 Z    =       16477083
91                 Z    =         5024545
09
 XDOT =     -22407
015329                 XDOT =       -6852
420559
 YDOT =       9551
872496  feet/sec       YDOT =        2834
909385  meter/sec
 ZDOT =      -6272
041394                 ZDOT =       -1944
950486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11609173
52                 X    =        -3538476
09
 Y    =        9397772
20  feet           Y    =         2864440
97  meter
 Z    =       16486411
71                 Z    =         5025058
29
 XDOT =     -19477
549018                 XDOT =       -5936
756941
 YDOT =     -12752
105662  feet/sec       YDOT =       -3886
841806  meter/sec
 ZDOT =      -6417
727048                 ZDOT =       -1956
123204


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   16259
90180647  
00016717  00000-0  10270-3 0  9072
2 25544  51
6428 325
4609 0006433 325
3729  34
7004 15
53829371 19095


Satellite: ISS
Catalog Number: 25544
Epoch time:      16259
90180647   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       325
4609  deg
Eccentricity:     
0006433     
Arg of perigee:   325
3729  deg
Mean anomaly:      34
7004  deg
Mean motion:   15
53829371  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1909
Checksum:              321


Coasting Arc #9 (Orbit 1923)
---------------------------------------

Vector Time (GMT): 2016/260/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         864090
61                 A    =         6782400
54  meter
 Y    =       -5186714
57  meter          E    =           
0005199
 Z    =       -4286136
57                 I    =           51
40131
 XDOT =       6556
901951                 Wp   =           59
05570
 YDOT =      -1818
281573  meter/sec      RA   =          320
05149  deg
 ZDOT =       3528
015048                 TA   =          247
00080
                                          MA   =          247
05565
                                          Ha   =            221
644  n
mi
                                          Hp   =            216
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2834942
96                 X    =          942845
74
 Y    =      -17016780
08  feet           Y    =        -5176612
01  meter
 Z    =      -14062127
85                 Z    =        -4281747
00
 XDOT =      21512
145507                 XDOT =        6559
609557
 YDOT =      -5965
490725  feet/sec       YDOT =       -1744
942243  meter/sec
 ZDOT =      11574
852520                 ZDOT =        3559
873631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15761544
34                 X    =         4804118
71
 Y    =       -7053173
62  feet           Y    =        -2149807
32  meter
 Z    =      -14041994
44                 Z    =        -4279999
90
 XDOT =      16383
307623                 XDOT =        4993
632164
 YDOT =      13327
575345  feet/sec       YDOT =        4062
244965  meter/sec
 ZDOT =      11714
321228                 ZDOT =        3570
525110


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   16260
86651613  
00016717  00000-0  10270-3 0  9086
2 25544  51
6420 320
6545 0006466 328
8656  31
2113 15
53840844 19244


Satellite: ISS
Catalog Number: 25544
Epoch time:      16260
86651613   =   yrday
fracday
Element set:     908
Inclination:       51
6420  deg
RA of node:       320
6545  deg
Eccentricity:     
0006466     
Arg of perigee:   328
8656  deg
Mean anomaly:      31
2113  deg
Mean motion:   15
53840844  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1924
Checksum:              304


Coasting Arc #10 (Orbit 1939)
---------------------------------------

Vector Time (GMT): 2016/261/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2112296
93                 A    =         6785994
60  meter
 Y    =        5637823
26  meter          E    =           
0010903
 Z    =        3127950
97                 I    =           51
38988
 XDOT =      -5932
071114                 Wp   =           64
57109
 YDOT =        468
521900  meter/sec      RA   =          315
05220  deg
 ZDOT =      -4832
568942                 TA   =           79
27152
                                          MA   =           79
14878
                                          Ha   =            221
767  n
mi
                                          Hp   =            215
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6930108
05                 X    =        -2190377
81
 Y    =       18496795
47  feet           Y    =         5613766
02  meter
 Z    =       10262306
35                 Z    =         3117499
46
 XDOT =     -19462
175572                 XDOT =       -5913
394735
 YDOT =       1537
145341  feet/sec       YDOT =         402
289225  meter/sec
 ZDOT =     -15854
884981                 ZDOT =       -4861
340262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19178152
05                 X    =        -5845500
75
 Y    =        4828273
91  feet           Y    =         1471657
89  meter
 Z    =       10215626
59                 Z    =         3113722
99
 XDOT =     -11970
412702                 XDOT =       -3648
581791
 YDOT =     -13611
258357  feet/sec       YDOT =       -4148
711547  meter/sec
 ZDOT =     -15980
611073                 ZDOT =       -4870
890255


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   16261
89553240  
00016717  00000-0  10270-3 0  9098
2 25544  51
6424 315
5275 0006527 332
3312  27
7492 15
53863289 19404


Satellite: ISS
Catalog Number: 25544
Epoch time:      16261
89553240   =   yrday
fracday
Element set:     909
Inclination:       51
6424  deg
RA of node:       315
5275  deg
Eccentricity:     
0006527     
Arg of perigee:   332
3312  deg
Mean anomaly:      27
7492  deg
Mean motion:   15
53863289  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1940
Checksum:              316


Coasting Arc #11 (Orbit 1954)
---------------------------------------

Vector Time (GMT): 2016/262/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3096679
78                 A    =         6788911
64  meter
 Y    =       -5789609
60  meter          E    =           
0012313
 Z    =       -1697182
92                 I    =           51
37734
 XDOT =       5050
887216                 Wp   =            9
64137
 YDOT =       1042
247816  meter/sec      RA   =          310
05928  deg
 ZDOT =       5678
308974                 TA   =          331
67580
                                          MA   =          331
74269
                                          Ha   =            221
911  n
mi
                                          Hp   =            215
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10159710
56                 X    =         3169434
76
 Y    =      -18994782
15  feet           Y    =        -5754573
88  meter
 Z    =       -5568185
43                 Z    =        -1681962
41
 XDOT =      16571
152283                 XDOT =        5011
274143
 YDOT =       3419
448214  feet/sec       YDOT =        1098
509503  meter/sec
 ZDOT =      18629
622617                 ZDOT =        5702
748751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21368596
48                 X    =         6513148
21
 Y    =       -2855162
20  feet           Y    =         -870253
44  meter
 Z    =       -5500662
68                 Z    =        -1676601
98
 XDOT =       6649
083355                 XDOT =        2026
640607
 YDOT =      13781
036995  feet/sec       YDOT =        4200
460076  meter/sec
 ZDOT =      18736
149754                 ZDOT =        5710
778445


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   16262
86022774  
00016717  00000-0  10270-3 0  9101
2 25544  51
6422 310
7203 0006579 336
3760  23
7090 15
53861741 19555


Satellite: ISS
Catalog Number: 25544
Epoch time:      16262
86022774   =   yrday
fracday
Element set:     910
Inclination:       51
6422  deg
RA of node:       310
7203  deg
Eccentricity:     
0006579     
Arg of perigee:   336
3760  deg
Mean anomaly:      23
7090  deg
Mean motion:   15
53861741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1955
Checksum:              300


Coasting Arc #12 (Orbit 1970)
---------------------------------------

Vector Time (GMT): 2016/263/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3849801
72                 A    =         6790076
89  meter
 Y    =        5590726
19  meter          E    =           
0006998
 Z    =          77004
90                 I    =           51
36176
 XDOT =      -3982
782317                 Wp   =          109
08784
 YDOT =      -2654
001777  meter/sec      RA   =          305
07108  deg
 ZDOT =      -5985
413502                 TA   =           70
08006
                                          MA   =           70
00468
                                          Ha   =            222
022  n
mi
                                          Hp   =            215
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12630583
08                 X    =        -3912406
58
 Y    =       18342277
53  feet           Y    =         5547325
09  meter
 Z    =         252640
73                 Z    =           58150
61
 XDOT =     -13066
871118                 XDOT =       -3923
733718
 YDOT =      -8707
354912  feet/sec       YDOT =       -2698
210469  meter/sec
 ZDOT =     -19637
183405                 ZDOT =       -6004
617322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22253775
80                 X    =        -6782950
86
 Y    =         880569
64  feet           Y    =          268397
63  meter
 Z    =         169296
03                 Z    =           51601
43
 XDOT =       -718
767399                 XDOT =        -219
080303
 YDOT =     -13954
999668  feet/sec       YDOT =       -4253
483899  meter/sec
 ZDOT =     -19720
550901                 ZDOT =       -6010
823915


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   16263
88922959  
00016717  00000-0  10270-3 0  9119
2 25544  51
6426 305
5928 0006528 340
5783  19
5120 15
53869316 19712


Satellite: ISS
Catalog Number: 25544
Epoch time:      16263
88922959   =   yrday
fracday
Element set:     911
Inclination:       51
6426  deg
RA of node:       305
5928  deg
Eccentricity:     
0006528     
Arg of perigee:   340
5783  deg
Mean anomaly:      19
5120  deg
Mean motion:   15
53869316  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1971
Checksum:              335


Coasting Arc #13 (Orbit 1986)
---------------------------------------

Vector Time (GMT): 2016/264/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4310056
35                 A    =         6789041
19  meter
 Y    =       -5004312
45  meter          E    =           
0016551
 Z    =        1526564
80                 I    =           51
34048
 XDOT =       2859
623340                 Wp   =           39
19392
 YDOT =       4219
470228  meter/sec      RA   =          300
08142  deg
 ZDOT =       5736
806444                 TA   =          337
56814
                                          MA   =          337
64043
                                          Ha   =            222
076  n
mi
                                          Hp   =            215
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14140604
83                 X    =         4358280
04
 Y    =      -16418347
94  feet           Y    =        -4955844
73  meter
 Z    =        5008414
69                 Z    =         1547619
82
 XDOT =       9381
966338                 XDOT =        2784
360380
 YDOT =      13843
406260  feet/sec       YDOT =        4251
028204  meter/sec
 ZDOT =      18821
543451                 ZDOT =        5750
514700

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21619629
70                 X    =         6589663
13
 Y    =        1082533
82  feet           Y    =          329956
31  meter
 Z    =        5101255
13                 Z    =         1554862
56
 XDOT =      -5183
658291                 XDOT =       -1579
979047
 YDOT =      14226
587456  feet/sec       YDOT =        4336
263856  meter/sec
 ZDOT =      18880
632487                 ZDOT =        5754
816782


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   16264
91822539  
00016717  00000-0  10270-3 0  9128
2 25544  51
6424 300
4652 0006617 344
2847  15
8100 15
53877054 19871


Satellite: ISS
Catalog Number: 25544
Epoch time:      16264
91822539   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:       300
4652  deg
Eccentricity:     
0006617     
Arg of perigee:   344
2847  deg
Mean anomaly:      15
8100  deg
Mean motion:   15
53877054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1987
Checksum:              313


Coasting Arc #14 (Orbit 2001)
---------------------------------------

Vector Time (GMT): 2016/265/20:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4552391
29                 A    =         6786081
56  meter
 Y    =        4039251
69  meter          E    =           
0005713
 Z    =       -3010552
10                 I    =           51
31691
 XDOT =      -1723
663114                 Wp   =           28
60608
 YDOT =      -5611
106298  meter/sec      RA   =          295
08572  deg
 ZDOT =      -4920
948522                 TA   =          186
00436
                                          MA   =          186
01121
                                          Ha   =            222
200  n
mi
                                          Hp   =            215
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14935666
97                 X    =        -4582596
79
 Y    =       13252138
09  feet           Y    =         3988174
66  meter
 Z    =       -9877139
44                 Z    =        -3032740
38
 XDOT =      -5655
062711                 XDOT =       -1636
886122
 YDOT =     -18409
141396  feet/sec       YDOT =       -5629
896666  meter/sec
 ZDOT =     -16144
844231                 ZDOT =       -4929
110480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19645226
05                 X    =        -5987864
90
 Y    =       -3289480
30  feet           Y    =        -1002633
60  meter
 Z    =       -9974748
51                 Z    =        -3040303
35
 XDOT =      10632
567501                 XDOT =        3240
806574
 YDOT =     -14427
680828  feet/sec       YDOT =       -4397
557116  meter/sec
 ZDOT =     -16179
470305                 ZDOT =       -4931
502549


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   16265
88290044  
00016717  00000-0  10270-3 0  9136
2 25544  51
6438 295
6584 0006625 346
7830  13
3148 15
53899050 20027


Satellite: ISS
Catalog Number: 25544
Epoch time:      16265
88290044   =   yrday
fracday
Element set:     913
Inclination:       51
6438  deg
RA of node:       295
6584  deg
Eccentricity:     
0006625     
Arg of perigee:   346
7830  deg
Mean anomaly:      13
3148  deg
Mean motion:   15
53899050  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2002
Checksum:              317


Coasting Arc #15 (Orbit 2002)
---------------------------------------

Vector Time (GMT): 2016/265/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2925936
30                 A    =         6778891
14  meter
 Y    =       -3402766
28  meter          E    =           
0012091
 Z    =       -5089804
36                 I    =           51
29173
 XDOT =       4275
361528                 Wp   =           72
50600
 YDOT =      -6137
792463  meter/sec      RA   =          294
66224  deg
 ZDOT =       1652
473097                 TA   =          213
50348
                                          MA   =          213
58001
                                          Ha   =            222
131  n
mi
                                          Hp   =            215
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9599528
53                 X    =        -2862943
94
 Y    =      -11163931
36  feet           Y    =        -3435134
27  meter
 Z    =      -16698833
22                 Z    =        -5103864
67
 XDOT =      14026
776668                 XDOT =        4335
651055
 YDOT =     -20137
114381  feet/sec       YDOT =       -6089
645270  meter/sec
 ZDOT =       5421
499663                 ZDOT =        1673
388861

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4280633
85                 X    =        -1304737
20
 Y    =      -14015239
02  feet           Y    =        -4271844
85  meter
 Z    =      -16759611
91                 Z    =        -5108329
71
 XDOT =      19811
925618                 XDOT =        6038
674929
 YDOT =     -12618
060352  feet/sec       YDOT =       -3845
984795  meter/sec
 ZDOT =       5513
930252                 ZDOT =        1680
645941


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   16265
94721086  
00016717  00000-0  10270-3 0  9149
2 25544  51
6436 295
3381 0006712 346
7322  13
3653 15
53919592 20036


Satellite: ISS
Catalog Number: 25544
Epoch time:      16265
94721086   =   yrday
fracday
Element set:     914
Inclination:       51
6436  deg
RA of node:       295
3381  deg
Eccentricity:     
0006712     
Arg of perigee:   346
7322  deg
Mean anomaly:      13
3653  deg
Mean motion:   15
53919592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2003
Checksum:              309


Coasting Arc #16 (Orbit 2018)
---------------------------------------

Vector Time (GMT): 2016/266/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2033591
55                 A    =         6781623
55  meter
 Y    =        4756269
96  meter          E    =           
0012555
 Z    =        4384669
40                 I    =           51
28835
 XDOT =      -4660
959869                 Wp   =           37
68771
 YDOT =       5088
044517  meter/sec      RA   =          289
64509  deg
 ZDOT =      -3342
665763                 TA   =           86
35120
                                          MA   =           86
20763
                                          Ha   =            222
251  n
mi
                                          Hp   =            214
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6671888
29                 X    =         1958955
63
 Y    =       15604560
25  feet           Y    =         4778593
96  meter
 Z    =       14385398
31                 Z    =         4394366
50
 XDOT =     -15291
863087                 XDOT =       -4701
271936
 YDOT =      16693
059439  feet/sec       YDOT =        5035
696892  meter/sec
 ZDOT =     -10966
751190                 ZDOT =       -3365
405964

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         136287
11                 X    =           41540
31
 Y    =       16935240
19  feet           Y    =         5161861
21  meter
 Z    =       14426889
61                 Z    =         4397315
95
 XDOT =     -19197
512073                 XDOT =       -5851
401680
 YDOT =       9623
675143  feet/sec       YDOT =        2933
296184  meter/sec
 ZDOT =     -11066
953130                 ZDOT =       -3373
207314


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   16266
97618975  
00016717  00000-0  10270-3 0  9156
2 25544  51
6433 290
2103 0006859 350
4105   9
6915 15
53959847 20195


Satellite: ISS
Catalog Number: 25544
Epoch time:      16266
97618975   =   yrday
fracday
Element set:     915
Inclination:       51
6433  deg
RA of node:       290
2103  deg
Eccentricity:     
0006859     
Arg of perigee:   350
4105  deg
Mean anomaly:       9
6915  deg
Mean motion:   15
53959847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2019
Checksum:              335


Coasting Arc #17 (Orbit 2033)
---------------------------------------

Vector Time (GMT): 2016/267/22:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893178
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1201695
60                 A    =         6785334
68  meter
 Y    =       -5812628
89  meter          E    =           
0008169
 Z    =       -3283343
00                 I    =           51
28942
 XDOT =       4841
538856                 Wp   =           28
44562
 YDOT =      -3646
406472  meter/sec      RA   =          284
63630  deg
 ZDOT =       4695
270597                 TA   =          293
21494
                                          MA   =          293
30095
                                          Ha   =            222
361  n
mi
                                          Hp   =            214
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3942570
86                 X    =        -1120658
89
 Y    =      -19070304
74  feet           Y    =        -5825614
20  meter
 Z    =      -10772122
70                 Z    =        -3288983
28
 XDOT =      15884
313831                 XDOT =        4859
146407
 YDOT =     -11963
275827  feet/sec       YDOT =       -3592
166335  meter/sec
 ZDOT =      15404
431094                 ZDOT =        4718
832679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3356642
77                 X    =         1023104
72
 Y    =      -19168837
66  feet           Y    =        -5842661
72  meter
 Z    =      -10795722
65                 Z    =        -3290536
26
 XDOT =      17663
918832                 XDOT =        5383
962460
 YDOT =      -5618
913140  feet/sec       YDOT =       -1712
644725  meter/sec
 ZDOT =      15507
960289                 ZDOT =        4726
826296


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   16267
94085419  
00016717  00000-0  10270-3 0  9166
2 25544  51
6422 285
4032 0006751 353
7854   6
3214 15
53921886 20343


Satellite: ISS
Catalog Number: 25544
Epoch time:      16267
94085419   =   yrday
fracday
Element set:     916
Inclination:       51
6422  deg
RA of node:       285
4032  deg
Eccentricity:     
0006751     
Arg of perigee:   353
7854  deg
Mean anomaly:       6
3214  deg
Mean motion:   15
53921886  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2034
Checksum:              313
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