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

 
Date: March 7th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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


069/22:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 1
000/00:00:00 000 0 0 0 0 214 5

072/21:25:54 157 -0 5 0 7 0 7
N/A 0 4 -0 1 220 9
000/00:01:48 313 0 2 0 0 215 1

073/06:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 215 1

077/07:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 215 2

080/17:44:26 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 215 4

Coasting Arc #1 (Orbit 2269)
---------------------------------------

Vector Time (GMT): 2018/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3824391
42                 A    =         6783091
76  meter
 Y    =       -4141778
98  meter          E    =           
0012199
 Z    =        3760513
88                 I    =           51
73629
 XDOT =       6128
644521                 Wp   =           97
10633
 YDOT =       1782
668268  meter/sec      RA   =          164
46282  deg
 ZDOT =      -4258
984320                 TA   =           37
92138
                                          MA   =           37
83552
                                          Ha   =            221
343  n
mi
                                          Hp   =            214
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12547215
95                 X    =         3852155
19
 Y    =      -13588513
72  feet           Y    =        -4098856
40  meter
 Z    =       12337643
95                 Z    =         3779159
18
 XDOT =      20107
101447                 XDOT =        6128
942534
 YDOT =       5848
649173  feet/sec       YDOT =        1851
204227  meter/sec
 ZDOT =     -13973
045669                 ZDOT =       -4229
213116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15679698
28                 X    =         4779172
04
 Y    =       -9703472
33  feet           Y    =        -2957618
37  meter
 Z    =       12421251
07                 Z    =         3785997
32
 XDOT =      17152
550105                 XDOT =        5228
097272
 YDOT =       9956
366400  feet/sec       YDOT =        3034
700479  meter/sec
 ZDOT =     -13840
494126                 ZDOT =       -4218
582610


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   18066
54029919  
00016717  00000-0  10270-3 0  9007
2 25544  51
6405 165
4499 0002886 166
2198 193
9034 15
54180609 22707


Satellite: ISS
Catalog Number: 25544
Epoch time:      18066
54029919   =   yrday
fracday
Element set:     900
Inclination:       51
6405  deg
RA of node:       165
4499  deg
Eccentricity:     
0002886     
Arg of perigee:   166
2198  deg
Mean anomaly:     193
9034  deg
Mean motion:   15
54180609  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2270
Checksum:              328


Coasting Arc #2 (Orbit 2284)
---------------------------------------

Vector Time (GMT): 2018/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5047421
01                 A    =         6786760
80  meter
 Y    =        3874344
33  meter          E    =           
0004618
 Z    =       -2362378
37                 I    =           51
78015
 XDOT =      -4666
282939                 Wp   =           74
17316
 YDOT =      -2793
462744  meter/sec      RA   =          159
49047  deg
 ZDOT =       5398
576272                 TA   =          259
52996
                                          MA   =          259
58201
                                          Ha   =            221
257  n
mi
                                          Hp   =            214
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16559780
21                 X    =        -5078894
73
 Y    =       12711103
45  feet           Y    =         3817724
42  meter
 Z    =       -7750585
20                 Z    =        -2386973
60
 XDOT =     -15309
327228                 XDOT =       -4660
922142
 YDOT =      -9164
904017  feet/sec       YDOT =       -2845
613888  meter/sec
 ZDOT =      17711
864410                 ZDOT =        5375
922500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19197382
46                 X    =        -5851362
17
 Y    =        8095664
19  feet           Y    =         2467558
44  meter
 Z    =       -7860710
56                 Z    =        -2395944
58
 XDOT =     -11998
865591                 XDOT =       -3657
254232
 YDOT =     -11384
475659  feet/sec       YDOT =       -3469
988181  meter/sec
 ZDOT =      17611
153863                 ZDOT =        5367
879697


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   18067
50478685  
00016717  00000-0  10270-3 0  9013
2 25544  51
6408 160
6417 0002573 171
6850 188
4345 15
54173477 22850


Satellite: ISS
Catalog Number: 25544
Epoch time:      18067
50478685   =   yrday
fracday
Element set:     901
Inclination:       51
6408  deg
RA of node:       160
6417  deg
Eccentricity:     
0002573     
Arg of perigee:   171
6850  deg
Mean anomaly:     188
4345  deg
Mean motion:   15
54173477  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2285
Checksum:              327


Coasting Arc #3 (Orbit 2300)
---------------------------------------

Vector Time (GMT): 2018/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5842520
33                 A    =         6788933
54  meter
 Y    =       -3373847
14  meter          E    =           
0015294
 Z    =         678167
71                 I    =           51
81687
 XDOT =       2910
362210                 Wp   =          135
16215
 YDOT =       3823
412860  meter/sec      RA   =          154
52920  deg
 ZDOT =      -5980
577175                 TA   =           37
52780
                                          MA   =           37
42114
                                          Ha   =            221
267  n
mi
                                          Hp   =            214
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19168373
80                 X    =         5876519
23
 Y    =      -11069052
30  feet           Y    =        -3308321
91  meter
 Z    =        2224959
68                 Z    =          706631
26
 XDOT =       9548
432449                 XDOT =        2896
441722
 YDOT =      12544
005446  feet/sec       YDOT =        3855
880225  meter/sec
 ZDOT =     -19621
316191                 ZDOT =       -5966
473874

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21234563
03                 X    =         6472294
81
 Y    =       -6201688
54  feet           Y    =        -1890274
67  meter
 Z    =        2352298
98                 Z    =          716980
73
 XDOT =       5968
687574                 XDOT =        1819
255973
 YDOT =      12934
086627  feet/sec       YDOT =        3942
309604  meter/sec
 ZDOT =     -19558
850032                 ZDOT =       -5961
537490


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   18068
53357286  
00016717  00000-0  10270-3 0  9021
2 25544  51
6398 155
5132 0002752 173
1869 186
9322 15
54190992 23019


Satellite: ISS
Catalog Number: 25544
Epoch time:      18068
53357286   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       155
5132  deg
Eccentricity:     
0002752     
Arg of perigee:   173
1869  deg
Mean anomaly:     186
9322  deg
Mean motion:   15
54190992  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2301
Checksum:              324


Coasting Arc #4 (Orbit 2316)
---------------------------------------

Vector Time (GMT): 2018/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6152223
48                 A    =         6788708
17  meter
 Y    =        2660207
38  meter          E    =           
0012402
 Z    =        1046347
91                 I    =           51
84585
 XDOT =      -1048
582093                 Wp   =           66
60707
 YDOT =      -4770
118667  meter/sec      RA   =          149
57182  deg
 ZDOT =       5911
411454                 TA   =          304
70461
                                          MA   =          304
82139
                                          Ha   =            221
168  n
mi
                                          Hp   =            214
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20184460
24                 X    =        -6186595
95
 Y    =        8727714
49  feet           Y    =         2591216
88  meter
 Z    =        3432899
96                 Z    =         1016379
16
 XDOT =      -3440
229964                 XDOT =       -1023
877628
 YDOT =     -15649
995626  feet/sec       YDOT =       -4781
706049  meter/sec
 ZDOT =      19394
394535                 ZDOT =        5906
378226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21635213
08                 X    =        -6594412
95
 Y    =        4050307
56  feet           Y    =         1234533
74  meter
 Z    =        3298909
09                 Z    =         1005507
49
 XDOT =        270
888558                 XDOT =          82
566833
 YDOT =     -14472
444852  feet/sec       YDOT =       -4411
201191  meter/sec
 ZDOT =      19372
492642                 ZDOT =        5904
735757


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   18069
56235518  
00016717  00000-0  10270-3 0  9039
2 25544  51
6403 150
3841 0002598 177
5577 182
5589 15
54195365 23171


Satellite: ISS
Catalog Number: 25544
Epoch time:      18069
56235518   =   yrday
fracday
Element set:     903
Inclination:       51
6403  deg
RA of node:       150
3841  deg
Eccentricity:     
0002598     
Arg of perigee:   177
5577  deg
Mean anomaly:     182
5589  deg
Mean motion:   15
54195365  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2317
Checksum:              334


Coasting Arc #5 (Orbit 2322)
---------------------------------------

Vector Time (GMT): 2018/069/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          43054
11                 A    =         6778619
13  meter
 Y    =        4616902
91  meter          E    =           
0013398
 Z    =       -4975437
08                 I    =           51
82431
 XDOT =      -6936
256078                 Wp   =          114
92518
 YDOT =       2409
267777  meter/sec      RA   =          147
38009  deg
 ZDOT =       2174
717034                 TA   =          176
25625
                                          MA   =          176
24621
                                          Ha   =            221
075  n
mi
                                          Hp   =            214
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         141253
63                 X    =           15591
23
 Y    =       15147319
24  feet           Y    =         4617230
43  meter
 Z    =      -16323612
48                 Z    =        -4975295
00
 XDOT =     -22756
745664                 XDOT =       -6973
245163
 YDOT =       7904
421842  feet/sec       YDOT =        2331
495143  meter/sec
 ZDOT =       7134
898405                 ZDOT =        2140
933460

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8582434
38                 X    =         2615926
00
 Y    =      -12482239
20  feet           Y    =        -3804586
51  meter
 Z    =      -16323513
16                 Z    =        -4975406
81
 XDOT =      22250
333990                 XDOT =        6781
901800
 YDOT =       6161
640639  feet/sec       YDOT =        1878
068067  meter/sec
 ZDOT =       6983
910047                 ZDOT =        2128
695782


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   18069
94814856  
00016717  00000-0  10270-3 0  9040
2 25544  51
6399 148
4624 0002184 176
4177 183
6992 15
54210956 23238


Satellite: ISS
Catalog Number: 25544
Epoch time:      18069
94814856   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:       148
4624  deg
Eccentricity:     
0002184     
Arg of perigee:   176
4177  deg
Mean anomaly:     183
6992  deg
Mean motion:   15
54210956  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2323
Checksum:              342


Coasting Arc #6 (Orbit 2338)
---------------------------------------

Vector Time (GMT): 2018/070/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1504837
53                 A    =         6782015
92  meter
 Y    =       -5199362
57  meter          E    =           
0010396
 Z    =        4077437
31                 I    =           51
86287
 XDOT =       6513
238128                 Wp   =           89
22794
 YDOT =      -1167
161943  meter/sec      RA   =          142
40206  deg
 ZDOT =      -3883
449991                 TA   =           40
86652
                                          MA   =           40
78861
                                          Ha   =            221
057  n
mi
                                          Hp   =            214
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4937130
99                 X    =         1543060
58
 Y    =      -17058276
15  feet           Y    =        -5182320
39  meter
 Z    =       13377419
00                 Z    =         4084840
45
 XDOT =      21368
891495                 XDOT =        6544
669083
 YDOT =      -3829
271465  feet/sec       YDOT =       -1094
151011  meter/sec
 ZDOT =     -12740
977662                 ZDOT =       -3851
734922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13650866
33                 X    =        -4160784
06
 Y    =       11318694
15  feet           Y    =         3449937
98  meter
 Z    =       13411055
07                 Z    =         4087689
59
 XDOT =     -19028
792707                 XDOT =       -5799
976017
 YDOT =      -7987
550572  feet/sec       YDOT =       -2434
605414  meter/sec
 ZDOT =     -12599
342329                 ZDOT =       -3840
279542


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   18070
97692660  
00016717  00000-0  10270-3 0  9053
2 25544  51
6399 143
3341 0002164 177
9380 182
1782 15
54203509 23392


Satellite: ISS
Catalog Number: 25544
Epoch time:      18070
97692660   =   yrday
fracday
Element set:     905
Inclination:       51
6399  deg
RA of node:       143
3341  deg
Eccentricity:     
0002164     
Arg of perigee:   177
9380  deg
Mean anomaly:     182
1782  deg
Mean motion:   15
54203509  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2339
Checksum:              319


Coasting Arc #7 (Orbit 2353)
---------------------------------------

Vector Time (GMT): 2018/071/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2811524
08                 A    =         6785761
45  meter
 Y    =        5524464
89  meter          E    =           
0003978
 Z    =       -2763892
36                 I    =           51
90148
 XDOT =      -5656
110339                 Wp   =           86
36776
 YDOT =       -299
703229  meter/sec      RA   =          137
43516  deg
 ZDOT =       5161
177253                 TA   =          242
46876
                                          MA   =          242
50918
                                          Ha   =            220
955  n
mi
                                          Hp   =            214
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9224160
37                 X    =        -2859665
85
 Y    =       18124884
82  feet           Y    =         5492755
07  meter
 Z    =       -9067888
32                 Z    =        -2777667
00
 XDOT =     -18556
792451                 XDOT =       -5677
408519
 YDOT =       -983
278310  feet/sec       YDOT =        -363
072362  meter/sec
 ZDOT =      16932
996236                 ZDOT =        5133
650533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17642042
04                 X    =         5377294
41
 Y    =      -10061044
84  feet           Y    =        -3066606
47  meter
 Z    =       -9130000
66                 Z    =        -2782824
20
 XDOT =      14294
981389                 XDOT =        4357
110327
 YDOT =       9831
282748  feet/sec       YDOT =        2996
574982  meter/sec
 ZDOT =      16810
204875                 ZDOT =        5123
750446


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   18071
94140361  
00016717  00000-0  10270-3 0  9068
2 25544  51
6404 138
5255 0002149 183
0365 177
0775 15
54225575 23542


Satellite: ISS
Catalog Number: 25544
Epoch time:      18071
94140361   =   yrday
fracday
Element set:     906
Inclination:       51
6404  deg
RA of node:       138
5255  deg
Eccentricity:     
0002149     
Arg of perigee:   183
0365  deg
Mean anomaly:     177
0775  deg
Mean motion:   15
54225575  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2354
Checksum:              304


Coasting Arc #8 (Orbit 2368)
---------------------------------------

Vector Time (GMT): 2018/072/21:26:48
313
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1152542
14                 A    =         6779067
35  meter
 Y    =        4487276
21  meter          E    =           
0012252
 Z    =       -4960254
92                 I    =           51
90018
 XDOT =      -6110
054533                 Wp   =          115
98076
 YDOT =       4040
788025  meter/sec      RA   =          132
68183  deg
 ZDOT =       2234
835821                 TA   =          175
79003
                                          MA   =          175
77971
                                          Ha   =            220
888  n
mi
                                          Hp   =            215
055

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3781306
22                 X    =         1126372
47
 Y    =       14722034
80  feet           Y    =         4500017
89  meter
 Z    =      -16273802
23                 Z    =        -4954720
38
 XDOT =     -20046
110672                 XDOT =       -6165
641102
 YDOT =      13257
178561  feet/sec       YDOT =        3972
150621  meter/sec
 ZDOT =       7332
138521                 ZDOT =        2205
020329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8273402
77                 X    =         2521733
17
 Y    =      -12781760
49  feet           Y    =        -3895880
60  meter
 Z    =      -16249634
75                 Z    =        -4952888
67
 XDOT =      22396
142434                 XDOT =        6826
344214
 YDOT =       5340
982138  feet/sec       YDOT =        1627
931356  meter/sec
 ZDOT =       7198
608789                 ZDOT =        2194
135959


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   18072
90587913  
00016717  00000-0  10270-3 0  9074
2 25544  51
6403 133
7166 0002060 204
1582 155
9475 15
54088844 23691


Satellite: ISS
Catalog Number: 25544
Epoch time:      18072
90587913   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:       133
7166  deg
Eccentricity:     
0002060     
Arg of perigee:   204
1582  deg
Mean anomaly:     155
9475  deg
Mean motion:   15
54088844  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2369
Checksum:              319


Coasting Arc #9 (Orbit 2374)
---------------------------------------

Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -569422
49                 A    =         6782700
03  meter
 Y    =        5457769
45  meter          E    =           
0007195
 Z    =       -3994952
74                 I    =           51
92028
 XDOT =      -6115
021516                 Wp   =          128
33270
 YDOT =       2292
576821  meter/sec      RA   =          130
73631  deg
 ZDOT =       4004
183740                 TA   =          183
27422
                                          MA   =          183
27893
                                          Ha   =            220
950  n
mi
                                          Hp   =            215
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1868184
03                 X    =         -611005
35
 Y    =       17906067
76  feet           Y    =         5451168
84  meter
 Z    =      -13106800
33                 Z    =        -3997820
35
 XDOT =     -20062
406547                 XDOT =       -6159
653171
 YDOT =       7521
577497  feet/sec       YDOT =        2223
945331  meter/sec
 ZDOT =      13137
085762                 ZDOT =        3974
370896

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17971418
86                 X    =        -5477688
47
 Y    =        -890436
95  feet           Y    =         -271405
18  meter
 Z    =      -13120244
48                 Z    =        -3999050
52
 XDOT =      -8578
626266                 XDOT =       -2614
765286
 YDOT =     -18439
852889  feet/sec       YDOT =       -5620
467161  meter/sec
 ZDOT =      13003
769001                 ZDOT =        3963
548791


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   18073
29170115  
00016717  00000-0  10270-3 0  9080
2 25544  51
6396 131
7891 0002524 201
5186 158
5861 15
54079654 23755


Satellite: ISS
Catalog Number: 25544
Epoch time:      18073
29170115   =   yrday
fracday
Element set:     908
Inclination:       51
6396  deg
RA of node:       131
7891  deg
Eccentricity:     
0002524     
Arg of perigee:   201
5186  deg
Mean anomaly:     158
5861  deg
Mean motion:   15
54079654  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2375
Checksum:              319


Coasting Arc #10 (Orbit 2390)
---------------------------------------

Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1747012
27                 A    =         6786452
31  meter
 Y    =       -5985742
26  meter          E    =           
0013318
 Z    =        2660224
16                 I    =           51
95333
 XDOT =       5562
439979                 Wp   =          113
11633
 YDOT =       -710
454551  meter/sec      RA   =          125
77484  deg
 ZDOT =      -5235
878872                 TA   =           36
99673
                                          MA   =           36
90496
                                          Ha   =            220
943  n
mi
                                          Hp   =            215
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5731667
57                 X    =         1800894
85
 Y    =      -19638262
01  feet           Y    =        -5965904
36  meter
 Z    =        8727769
55                 Z    =         2668842
03
 XDOT =      18249
474998                 XDOT =        5595
403841
 YDOT =      -2330
887634  feet/sec       YDOT =        -648
067859  meter/sec
 ZDOT =     -17178
080289                 ZDOT =       -5208
778711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19972834
02                 X    =         6087719
81
 Y    =        4349007
17  feet           Y    =         1325577
38  meter
 Z    =        8766946
27                 Z    =         2672165
22
 XDOT =       3871
166500                 XDOT =        1179
931549
 YDOT =      16709
152776  feet/sec       YDOT =        5092
949766  meter/sec
 ZDOT =     -17057
046610                 ZDOT =       -5198
987807


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   18074
32055946  
00016717  00000-0  10270-3 0  9090
2 25544  51
6395 126
6604 0002533 202
7268 157
3773 15
54076933 23917


Satellite: ISS
Catalog Number: 25544
Epoch time:      18074
32055946   =   yrday
fracday
Element set:     909
Inclination:       51
6395  deg
RA of node:       126
6604  deg
Eccentricity:     
0002533     
Arg of perigee:   202
7268  deg
Mean anomaly:     157
3773  deg
Mean motion:   15
54076933  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2391
Checksum:              321


Coasting Arc #11 (Orbit 2405)
---------------------------------------

Vector Time (GMT): 2018/075/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2682793
35                 A    =         6788932
54  meter
 Y    =        6139515
23  meter          E    =           
0007110
 Z    =       -1077005
86                 I    =           51
98015
 XDOT =      -4761
049779                 Wp   =           42
28210
 YDOT =      -1047
534045  meter/sec      RA   =          120
82385  deg
 ZDOT =       5915
879281                 TA   =          306
09568
                                          MA   =          306
16150
                                          Ha   =            220
838  n
mi
                                          Hp   =            215
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8801815
44                 X    =        -2746016
22
 Y    =       20142766
50  feet           Y    =         6109160
74  meter
 Z    =       -3533483
79                 Z    =        -1090192
17
 XDOT =     -15620
242056                 XDOT =       -4777
717997
 YDOT =      -3436
791485  feet/sec       YDOT =       -1100
867767  meter/sec
 ZDOT =      19409
052760                 ZDOT =        5892
711697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20808503
63                 X    =        -6342431
91
 Y    =       -7055811
10  feet           Y    =        -2150611
22  meter
 Z    =       -3593078
25                 Z    =        -1095170
25
 XDOT =       1586
189163                 XDOT =         483
470457
 YDOT =     -14463
512054  feet/sec       YDOT =       -4408
478474  meter/sec
 ZDOT =      19305
774896                 ZDOT =        5884
400188


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   18075
28511207  
00016717  00000-0  10270-3 0  9105
2 25544  51
6396 121
8528 0002429 207
2100 152
8925 15
54088442 24063


Satellite: ISS
Catalog Number: 25544
Epoch time:      18075
28511207   =   yrday
fracday
Element set:     910
Inclination:       51
6396  deg
RA of node:       121
8528  deg
Eccentricity:     
0002429     
Arg of perigee:   207
2100  deg
Mean anomaly:     152
8925  deg
Mean motion:   15
54088442  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2406
Checksum:              292


Coasting Arc #12 (Orbit 2421)
---------------------------------------

Vector Time (GMT): 2018/076/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3393686
24                 A    =         6789231
07  meter
 Y    =       -5836936
72  meter          E    =           
0011716
 Z    =        -647391
58                 I    =           51
99722
 XDOT =       3814
535136                 Wp   =          151
15902
 YDOT =       2877
148404  meter/sec      RA   =          115
87774  deg
 ZDOT =      -5999
483624                 TA   =           35
79817
                                          MA   =           35
71970
                                          Ha   =            220
783  n
mi
                                          Hp   =            215
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11134141
19                 X    =         3461848
88
 Y    =      -19150054
85  feet           Y    =        -5798605
16  meter
 Z    =       -2123988
13                 Z    =         -630739
98
 XDOT =      12514
879055                 XDOT =        3811
220657
 YDOT =       9439
463267  feet/sec       YDOT =        2919
785764  meter/sec
 ZDOT =     -19683
345223                 ZDOT =       -5980
962564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20179182
90                 X    =         6150614
95
 Y    =        9154638
09  feet           Y    =         2790333
69  meter
 Z    =       -2048952
20                 Z    =         -624520
63
 XDOT =      -7443
604151                 XDOT =       -2268
810545
 YDOT =      12062
482911  feet/sec       YDOT =        3676
644791  meter/sec
 ZDOT =     -19601
026702                 ZDOT =       -5974
392939


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   18076
31396631  
00016717  00000-0  10270-3 0  9113
2 25544  51
6396 116
7241 0002475 211
8903 148
2101 15
54105473 24228


Satellite: ISS
Catalog Number: 25544
Epoch time:      18076
31396631   =   yrday
fracday
Element set:     911
Inclination:       51
6396  deg
RA of node:       116
7241  deg
Eccentricity:     
0002475     
Arg of perigee:   211
8903  deg
Mean anomaly:     148
2101  deg
Mean motion:   15
54105473  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2422
Checksum:              285


Coasting Arc #13 (Orbit 2437)
---------------------------------------

Vector Time (GMT): 2018/077/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3853342
92                 A    =         6787218
58  meter
 Y    =        5095756
02  meter          E    =           
0012095
 Z    =        2277084
15                 I    =           52
00471
 XDOT =      -2817
925550                 Wp   =           78
78152
 YDOT =      -4582
972886  meter/sec      RA   =          110
92997  deg
 ZDOT =       5465
192062                 TA   =          306
43433
                                          MA   =          306
54577
                                          Ha   =            220
729  n
mi
                                          Hp   =            215
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12642201
19                 X    =        -3921099
49
 Y    =       16718359
65  feet           Y    =         5052286
77  meter
 Z    =        7470748
52                 Z    =         2258200
73
 XDOT =      -9245
162565                 XDOT =       -2793
014974
 YDOT =     -15036
000282  feet/sec       YDOT =       -4614
344792  meter/sec
 ZDOT =      17930
420152                 ZDOT =        5451
564789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18101855
69                 X    =        -5517445
61
 Y    =      -10626063
44  feet           Y    =        -3238824
14  meter
 Z    =        7385829
69                 Z    =         2251200
89
 XDOT =      13047
587601                 XDOT =        3976
904701
 YDOT =      -9754
807632  feet/sec       YDOT =       -2973
265366  meter/sec
 ZDOT =      17870
158574                 ZDOT =        5446
824333


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   18077
34281744  
00016717  00000-0  10270-3 0  9126
2 25544  51
6403 111
5953 0002345 214
1368 145
9634 15
54116482 24381


Satellite: ISS
Catalog Number: 25544
Epoch time:      18077
34281744   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:       111
5953  deg
Eccentricity:     
0002345     
Arg of perigee:   214
1368  deg
Mean anomaly:     145
9634  deg
Mean motion:   15
54116482  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2438
Checksum:              301


Coasting Arc #14 (Orbit 2437)
---------------------------------------

Vector Time (GMT): 2018/077/07:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2754010
29                 A    =         6778956
88  meter
 Y    =        3711313
97  meter          E    =           
0011751
 Z    =       -4970257
90                 I    =           51
97796
 XDOT =      -4138
395576                 Wp   =          116
75508
 YDOT =       6049
349365  meter/sec      RA   =          110
65855  deg
 ZDOT =       2222
899011                 TA   =          174
86893
                                          MA   =          174
85688
                                          Ha   =            220
639  n
mi
                                          Hp   =            215
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9035466
83                 X    =         2736447
48
 Y    =       12176226
92  feet           Y    =         3742012
28  meter
 Z    =      -16306620
42                 Z    =        -4956923
13
 XDOT =     -13577
413307                 XDOT =       -4216
531098
 YDOT =      19846
946737  feet/sec       YDOT =        6002
634418  meter/sec
 ZDOT =       7292
975759                 ZDOT =        2202
605557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7412858
05                 X    =        -2259439
13
 Y    =       13299340
35  feet           Y    =         4053638
94  meter
 Z    =      -16247557
18                 Z    =        -4952255
43
 XDOT =     -22700
646598                 XDOT =       -6919
157083
 YDOT =      -3850
466776  feet/sec       YDOT =       -1173
622273  meter/sec
 ZDOT =       7201
644491                 ZDOT =        2195
061241


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   18077
34281726  
00016717  00000-0  10270-3 0  9137
2 25544  51
6404 111
5968 0002292 216
9212 143
1783 15
54127115 24387


Satellite: ISS
Catalog Number: 25544
Epoch time:      18077
34281726   =   yrday
fracday
Element set:     913
Inclination:       51
6404  deg
RA of node:       111
5968  deg
Eccentricity:     
0002292     
Arg of perigee:   216
9212  deg
Mean anomaly:     143
1783  deg
Mean motion:   15
54127115  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2438
Checksum:              298


Coasting Arc #15 (Orbit 2453)
---------------------------------------

Vector Time (GMT): 2018/078/07:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1891111
55                 A    =         6782344
62  meter
 Y    =       -5067788
61  meter          E    =           
0008930
 Z    =        4084415
80                 I    =           51
99934
 XDOT =       4514
981321                 Wp   =           85
96427
 YDOT =      -4828
169596  meter/sec      RA   =          105
69039  deg
 ZDOT =      -3892
230212                 TA   =           44
15397
                                          MA   =           44
08272
                                          Ha   =            220
687  n
mi
                                          Hp   =            215
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6204434
21                 X    =        -1854141
55
 Y    =      -16626603
05  feet           Y    =        -5088729
04  meter
 Z    =       13400314
31                 Z    =         4075319
94
 XDOT =      14812
930843                 XDOT =        4587
542068
 YDOT =     -15840
451432  feet/sec       YDOT =       -4777
274799  meter/sec
 ZDOT =     -12769
784160                 ZDOT =       -3870
121093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12420470
55                 X    =         3785759
42
 Y    =      -12717717
48  feet           Y    =        -3876360
29  meter
 Z    =       13360349
17                 Z    =         4072234
43
 XDOT =      19719
087851                 XDOT =        6010
377977
 YDOT =       5920
111203  feet/sec       YDOT =        1804
449895  meter/sec
 ZDOT =     -12670
486698                 ZDOT =       -3861
964346


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   18078
37166752  
00016717  00000-0  10270-3 0  9143
2 25544  51
6400 106
4680 0002229 221
4533 138
6450 15
54109871 24541


Satellite: ISS
Catalog Number: 25544
Epoch time:      18078
37166752   =   yrday
fracday
Element set:     914
Inclination:       51
6400  deg
RA of node:       106
4680  deg
Eccentricity:     
0002229     
Arg of perigee:   221
4533  deg
Mean anomaly:     138
6450  deg
Mean motion:   15
54109871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2454
Checksum:              298


Coasting Arc #16 (Orbit 2468)
---------------------------------------

Vector Time (GMT): 2018/079/07:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1068300
10                 A    =         6786134
68  meter
 Y    =        6090246
07  meter          E    =           
0002475
 Z    =       -2797107
62                 I    =           52
01937
 XDOT =      -4696
305970                 Wp   =           69
99966
 YDOT =       3186
886569  meter/sec      RA   =          100
73305  deg
 ZDOT =       5149
773782                 TA   =          258
47337
                                          MA   =          258
50116
                                          Ha   =            220
526  n
mi
                                          Hp   =            215
390

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3504921
57                 X    =         1013704
83
 Y    =       19981122
27  feet           Y    =         6101886
92  meter
 Z    =       -9176862
28                 Z    =        -2792051
55
 XDOT =     -15407
827984                 XDOT =       -4756
608539
 YDOT =      10455
664598  feet/sec       YDOT =        3134
032728  meter/sec
 ZDOT =      16895
583275                 ZDOT =        5126
813810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16409594
30                 X    =        -5001644
34
 Y    =       11943801
29  feet           Y    =         3640470
63  meter
 Z    =       -9155072
33                 Z    =        -2790466
05
 XDOT =     -15319
586526                 XDOT =       -4669
409973
 YDOT =      -8187
152431  feet/sec       YDOT =       -2495
444061  meter/sec
 ZDOT =      16792
683785                 ZDOT =        5118
410018


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   18079
33621247  
00016717  00000-0  10270-3 0  9156
2 25544  51
6396 101
6601 0002341 228
7909 131
3042 15
54091145 24694


Satellite: ISS
Catalog Number: 25544
Epoch time:      18079
33621247   =   yrday
fracday
Element set:     915
Inclination:       51
6396  deg
RA of node:       101
6601  deg
Eccentricity:     
0002341     
Arg of perigee:   228
7909  deg
Mean anomaly:     131
3042  deg
Mean motion:   15
54091145  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2469
Checksum:              294


Coasting Arc #17 (Orbit 2484)
---------------------------------------

Vector Time (GMT): 2018/080/07:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -262950
78                 A    =         6788777
53  meter
 Y    =       -6669921
79  meter          E    =           
0013176
 Z    =        1196830
89                 I    =           52
03378
 XDOT =       4748
666616                 Wp   =          130
93328
 YDOT =      -1250
658949  meter/sec      RA   =           95
78516  deg
 ZDOT =      -5892
862810                 TA   =           36
13101
                                          MA   =           36
04206
                                          Ha   =            220
521  n
mi
                                          Hp   =            215
308

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -862699
42                 X    =         -194159
97
 Y    =      -21882945
51  feet           Y    =        -6672477
53  meter
 Z    =        3926610
52                 Z    =         1195721
37
 XDOT =      15579
614881                 XDOT =        4790
923474
 YDOT =      -4103
211776  feet/sec       YDOT =       -1197
320464  meter/sec
 ZDOT =     -19333
539402                 ZDOT =       -5869
692539

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19109663
22                 X    =         5824625
35
 Y    =      -10698614
96  feet           Y    =        -3260937
84  meter
 Z    =        3922529
09                 Z    =         1195586
87
 XDOT =       9990
383895                 XDOT =        3045
069011
 YDOT =      10753
570106  feet/sec       YDOT =        3277
688168  meter/sec
 ZDOT =     -19229
942752                 ZDOT =       -5861
286551


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   18080
36505853  
00016717  00000-0  10270-3 0  9166
2 25544  51
6399  96
5313 0002171 230
7774 129
3186 15
54110799 24854


Satellite: ISS
Catalog Number: 25544
Epoch time:      18080
36505853   =   yrday
fracday
Element set:     916
Inclination:       51
6399  deg
RA of node:        96
5313  deg
Eccentricity:     
0002171     
Arg of perigee:   230
7774  deg
Mean anomaly:     129
3186  deg
Mean motion:   15
54110799  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2485
Checksum:              324


Coasting Arc #18 (Orbit 2490)
---------------------------------------

Vector Time (GMT): 2018/080/17:44:26
000
Vector Time (MET): N/A
Weight (LBS)     : 904719
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3602233
88                 A    =         6779472
39  meter
 Y    =        3077450
54  meter          E    =           
0010460
 Z    =       -4859078
93                 I    =           52
00335
 XDOT =      -2421
024468                 Wp   =          115
34314
 YDOT =       6815
589536  meter/sec      RA   =           93
75151  deg
 ZDOT =       2521
656110                 TA   =          179
35020
                                          MA   =          179
34884
                                          Ha   =            220
472  n
mi
                                          Hp   =            215
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11818352
62                 X    =         3591156
24
 Y    =       10096622
52  feet           Y    =         3117670
77  meter
 Z    =      -15941860
00                 Z    =        -4841607
64
 XDOT =      -7942
993663                 XDOT =       -2509
307254
 YDOT =      22360
858058  feet/sec       YDOT =        6788
022610  meter/sec
 ZDOT =       8273
149968                 ZDOT =        2509
680436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11205373
55                 X    =         3415397
86
 Y    =      -10886809
80  feet           Y    =        -3318299
63  meter
 Z    =      -15864271
84                 Z    =        -4835430
06
 XDOT =      20685
463838                 XDOT =        6304
929378
 YDOT =       9313
707942  feet/sec       YDOT =        2838
818181  meter/sec
 ZDOT =       8218
791211                 ZDOT =        2505
087561


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   18080
75087600  
00016717  00000-0  10270-3 0  9175
2 25544  51
6393  94
6091 0001839 240
3695 119
7274 15
54115334 24917


Satellite: ISS
Catalog Number: 25544
Epoch time:      18080
75087600   =   yrday
fracday
Element set:     917
Inclination:       51
6393  deg
RA of node:        94
6091  deg
Eccentricity:     
0001839     
Arg of perigee:   240
3695  deg
Mean anomaly:     119
7274  deg
Mean motion:   15
54115334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2491
Checksum:              316
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