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

 
Date: January 14th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


016/05:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 216 2

018/18:05:10 698 3 0 3 2 3 2
N/A 0 8 0 0 220 9
000/00:08:17 397 -0 6 -0 0 218 0

020/01:03:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 217 9

025/12:55:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 217 5

026/08:59:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 217 4

Coasting Arc #1 (Orbit 3136)
---------------------------------------

Vector Time (GMT): 2019/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2829696
45                 A    =         6787626
57  meter
 Y    =       -5628335
52  meter          E    =           
0003091
 Z    =       -2524477
48                 I    =           51
92620
 XDOT =       5505
483972                 Wp   =          146
58238
 YDOT =       -385
072906  meter/sec      RA   =           45
01300  deg
 ZDOT =      -5318
198167                 TA   =           61
61581
                                          MA   =           61
58465
                                          Ha   =            220
719  n
mi
                                          Hp   =            216
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9283781
02                 X    =        -2754286
09
 Y    =      -18465667
70  feet           Y    =        -5659557
42  meter
 Z    =       -8282406
43                 Z    =        -2538040
02
 XDOT =      18062
611458                 XDOT =        5535
213467
 YDOT =      -1263
362551  feet/sec       YDOT =        -323
340344  meter/sec
 ZDOT =     -17448
156715                 ZDOT =       -5291
382574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13452162
09                 X    =         4100219
01
 Y    =      -15658974
03  feet           Y    =        -4772855
28  meter
 Z    =       -8342877
04                 Z    =        -2542908
92
 XDOT =       7063
413020                 XDOT =        2152
928288
 YDOT =      15289
851465  feet/sec       YDOT =        4660
346727  meter/sec
 ZDOT =     -17327
048985                 ZDOT =       -5281
284531


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   19014
52708432  
00016717  00000-0  10270-3 0  9003
2 25544  51
6422  45
5300 0002452 287
2155  72
8729 15
53770861 31374


Satellite: ISS
Catalog Number: 25544
Epoch time:      19014
52708432   =   yrday
fracday
Element set:     900
Inclination:       51
6422  deg
RA of node:        45
5300  deg
Eccentricity:     
0002452     
Arg of perigee:   287
2155  deg
Mean anomaly:      72
8729  deg
Mean motion:   15
53770861  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3137
Checksum:              291


Coasting Arc #2 (Orbit 3152)
---------------------------------------

Vector Time (GMT): 2019/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1735385
68                 A    =         6784308
64  meter
 Y    =        5345456
63  meter          E    =           
0009272
 Z    =        3792576
05                 I    =           51
88865
 XDOT =      -6317
419207                 Wp   =           92
76245
 YDOT =       -964
724541  meter/sec      RA   =           40
05289  deg
 ZDOT =       4241
062848                 TA   =          312
54859
                                          MA   =          312
62682
                                          Ha   =            220
859  n
mi
                                          Hp   =            216
036

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5693522
56                 X    =         1657060
17
 Y    =       17537587
36  feet           Y    =         5364424
80  meter
 Z    =       12442834
81                 Z    =         3800815
88
 XDOT =     -20726
440969                 XDOT =       -6326
762490
 YDOT =      -3165
106762  feet/sec       YDOT =       -1035
422762  meter/sec
 ZDOT =      13914
248189                 ZDOT =        4210
352606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13789876
04                 X    =        -4203154
22
 Y    =       12203015
80  feet           Y    =         3719479
22  meter
 Z    =       12479304
14                 Z    =         3803691
90
 XDOT =      -4605
049008                 XDOT =       -1403
618938
 YDOT =     -19322
838392  feet/sec       YDOT =       -5889
601142  meter/sec
 ZDOT =      13775
747544                 ZDOT =        4198
847851


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   19015
55616275  
00016717  00000-0  10270-3 0  9011
2 25544  51
6402  40
4028 0002312 294
1684  65
9227 15
53745097 31539


Satellite: ISS
Catalog Number: 25544
Epoch time:      19015
55616275   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:        40
4028  deg
Eccentricity:     
0002312     
Arg of perigee:   294
1684  deg
Mean anomaly:      65
9227  deg
Mean motion:   15
53745097  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3153
Checksum:              294


Coasting Arc #3 (Orbit 3163)
---------------------------------------

Vector Time (GMT): 2019/016/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5936183
90                 A    =         6787015
53  meter
 Y    =       -1566921
04  meter          E    =           
0010879
 Z    =        2881736
78                 I    =           51
87942
 XDOT =       -975
177622                 Wp   =           98
20537
 YDOT =      -5666
323504  meter/sec      RA   =           36
39803  deg
 ZDOT =      -5074
986258                 TA   =           49
10465
                                          MA   =           49
01047
                                          Ha   =            220
802  n
mi
                                          Hp   =            216
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19475668
98                 X    =        -5932218
78
 Y    =       -5140817
07  feet           Y    =        -1633281
59  meter
 Z    =        9454517
00                 Z    =         2852910
69
 XDOT =      -3199
401648                 XDOT =        -887
091372
 YDOT =     -18590
300210  feet/sec       YDOT =       -5676
735795  meter/sec
 ZDOT =     -16650
217381                 ZDOT =       -5079
509679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20200160
38                 X    =         6157008
88
 Y    =        -350365
99  feet           Y    =         -106791
55  meter
 Z    =        9324609
29                 Z    =         2842140
91
 XDOT =       7988
070137                 XDOT =        2434
763778
 YDOT =      15584
615103  feet/sec       YDOT =        4750
190683  meter/sec
 ZDOT =     -16669
858994                 ZDOT =       -5080
973021


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   19016
26365308  
00016717  00000-0  10270-3 0  9029
2 25544  51
6410  36
8752 0002482 283
3022  76
7854 15
53747168 31644


Satellite: ISS
Catalog Number: 25544
Epoch time:      19016
26365308   =   yrday
fracday
Element set:     902
Inclination:       51
6410  deg
RA of node:        36
8752  deg
Eccentricity:     
0002482     
Arg of perigee:   283
3022  deg
Mean anomaly:      76
7854  deg
Mean motion:   15
53747168  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3164
Checksum:              307


Coasting Arc #4 (Orbit 3178)
---------------------------------------

Vector Time (GMT): 2019/017/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6163261
66                 A    =         6789600
00  meter
 Y    =        2448057
32  meter          E    =           
0008332
 Z    =       -1434397
95                 I    =           51
86204
 XDOT =       -624
072454                 Wp   =           20
10035
 YDOT =       4964
754004  meter/sec      RA   =           31
44094  deg
 ZDOT =       5809
373304                 TA   =          324
30761
                                          MA   =          324
36329
                                          Ha   =            220
841  n
mi
                                          Hp   =            216
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20220674
74                 X    =         6142396
20
 Y    =        8031684
12  feet           Y    =         2516862
65  meter
 Z    =       -4706030
02                 Z    =        -1404509
78
 XDOT =      -2047
481803                 XDOT =        -707
761897
 YDOT =      16288
563005  feet/sec       YDOT =        4957
306791  meter/sec
 ZDOT =      19059
623701                 ZDOT =        5806
138942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21705992
01                 X    =        -6615986
36
 Y    =       -1866025
05  feet           Y    =         -568764
43  meter
 Z    =       -4571456
75                 Z    =        -1393380
02
 XDOT =      -2739
427061                 XDOT =        -834
977368
 YDOT =     -14644
144467  feet/sec       YDOT =       -4463
535234  meter/sec
 ZDOT =      19044
335112                 ZDOT =        5804
713342


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   19017
22841008  
00016717  00000-0  10270-3 0  9033
2 25544  51
6423  32
0688 0002536 292
9444  67
1441 15
53751354 31792


Satellite: ISS
Catalog Number: 25544
Epoch time:      19017
22841008   =   yrday
fracday
Element set:     903
Inclination:       51
6423  deg
RA of node:        32
0688  deg
Eccentricity:     
0002536     
Arg of perigee:   292
9444  deg
Mean anomaly:      67
1441  deg
Mean motion:   15
53751354  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3179
Checksum:              299


Coasting Arc #5 (Orbit 3194)
---------------------------------------

Vector Time (GMT): 2019/018/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6011679
70                 A    =         6790369
24  meter
 Y    =       -3142412
48  meter          E    =           
0009430
 Z    =        -167195
90                 I    =           51
83495
 XDOT =       2322
870056                 Wp   =          141
26601
 YDOT =      -4133
385208  meter/sec      RA   =           26
48690  deg
 ZDOT =      -6025
324510                 TA   =           40
52991
                                          MA   =           40
45972
                                          Ha   =            220
793  n
mi
                                          Hp   =            216
078

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19723358
59                 X    =        -5975281
42
 Y    =      -10309752
24  feet           Y    =        -3209435
74  meter
 Z    =        -548542
98                 Z    =         -196310
04
 XDOT =       7620
964751                 XDOT =        2398
185518
 YDOT =     -13560
975091  feet/sec       YDOT =       -4106
987556  meter/sec
 ZDOT =     -19768
125034                 ZDOT =       -6013
858450

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21920578
10                 X    =         6681392
20
 Y    =        3824823
40  feet           Y    =         1165806
17  meter
 Z    =        -679519
52                 Z    =         -207117
55
 XDOT =      -2982
363790                 XDOT =        -909
024483
 YDOT =      13679
275511  feet/sec       YDOT =        4169
443176  meter/sec
 ZDOT =     -19715
790181                 ZDOT =       -6009
372847


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   19018
25748341  
00016717  00000-0  10270-3 0  9044
2 25544  51
6414  26
9420 0002471 294
9208  65
1687 15
53764139 31959


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
25748341   =   yrday
fracday
Element set:     904
Inclination:       51
6414  deg
RA of node:        26
9420  deg
Eccentricity:     
0002471     
Arg of perigee:   294
9208  deg
Mean anomaly:      65
1687  deg
Mean motion:   15
53764139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3195
Checksum:              317


Coasting Arc #6 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2019/018/18:09:19
397
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1978710
32                 A    =         6780178
40  meter
 Y    =       -3711628
21  meter          E    =           
0010205
 Z    =       -5326606
75                 I    =           51
77926
 XDOT =       6910
898202                 Wp   =           86
86691
 YDOT =       3291
485180  meter/sec      RA   =           23
84784  deg
 ZDOT =        274
698500                 TA   =          185
74362
                                          MA   =          185
75534
                                          Ha   =            220
947  n
mi
                                          Hp   =            217
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6491831
76                 X    =         2045941
14
 Y    =      -12177257
90  feet           Y    =        -3689124
43  meter
 Z    =      -17475743
95                 Z    =        -5316832
12
 XDOT =      22673
550533                 XDOT =        6872
243943
 YDOT =      10798
835894  feet/sec       YDOT =        3368
551498  meter/sec
 ZDOT =        901
241799                 ZDOT =         308
175143

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -198942
88                 X    =          -60637
79
 Y    =      -13854538
50  feet           Y    =        -4222863
34  meter
 Z    =      -17431101
53                 Z    =        -5312999
75
 XDOT =      24041
484986                 XDOT =        7327
844624
 YDOT =      -1664
524446  feet/sec       YDOT =        -507
347051  meter/sec
 ZDOT =       1051
886530                 ZDOT =         320
615014


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   19018
77202257  
00016717  00000-0  10270-3 0  9053
2 25544  51
6414  24
3821 0004744 283
7239  76
3385 15
53170510 32034


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
77202257   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:        24
3821  deg
Eccentricity:     
0004744     
Arg of perigee:   283
7239  deg
Mean anomaly:      76
3385  deg
Mean motion:   15
53170510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3203
Checksum:              291


Coasting Arc #7 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2019/019/18:09:19
397
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3247629
22                 A    =         6781237
02  meter
 Y    =        3116494
70  meter          E    =           
0004618
 Z    =        5073430
95                 I    =           51
75198
 XDOT =      -6443
508778                 Wp   =          358
22806
 YDOT =      -3727
145510  meter/sec      RA   =           18
86814  deg
 ZDOT =      -1830
686914                 TA   =          109
50062
                                          MA   =          109
45073
                                          Ha   =            221
058  n
mi
                                          Hp   =            217
907

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10654951
51                 X    =        -3306880
86
 Y    =       10224720
15  feet           Y    =         3079845
62  meter
 Z    =       16645114
67                 Z    =         5057511
87
 XDOT =     -21140
120663                 XDOT =       -6392
459589
 YDOT =     -12228
167683  feet/sec       YDOT =       -3798
915683  meter/sec
 ZDOT =      -6006
190662                 ZDOT =       -1861
862946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4137512
10                 X    =        -1261113
69
 Y    =       14260272
40  feet           Y    =         4346531
03  meter
 Z    =       16572819
95                 Z    =         5051395
52
 XDOT =     -23347
045175                 XDOT =       -7116
179369
 YDOT =        386
241740  feet/sec       YDOT =         117
726482  meter/sec
 ZDOT =      -6146
386608                 ZDOT =       -1873
418638


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   19019
80149679  
00016717  00000-0  10270-3 0  9067
2 25544  51
6413  19
2582 0004951 287
3682  72
6929 15
53193896 32194


Satellite: ISS
Catalog Number: 25544
Epoch time:      19019
80149679   =   yrday
fracday
Element set:     906
Inclination:       51
6413  deg
RA of node:        19
2582  deg
Eccentricity:     
0004951     
Arg of perigee:   287
3682  deg
Mean anomaly:      72
6929  deg
Mean motion:   15
53193896  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3219
Checksum:              345


Coasting Arc #8 (Orbit 3222)
---------------------------------------

Vector Time (GMT): 2019/020/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1820716
88                 A    =         6780253
91  meter
 Y    =       -3816708
92  meter          E    =           
0010188
 Z    =       -5308756
95                 I    =           51
73723
 XDOT =       7154
952543                 Wp   =           89
82382
 YDOT =       2683
196869  meter/sec      RA   =           17
44620  deg
 ZDOT =        525
726351                 TA   =          185
18580
                                          MA   =          185
19636
                                          Ha   =            220
985  n
mi
                                          Hp   =            217
886

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5973480
57                 X    =         1889047
58
 Y    =      -12522010
91  feet           Y    =        -3795965
79  meter
 Z    =      -17417181
61                 Z    =        -5299747
20
 XDOT =      23474
253749                 XDOT =        7121
862876
 YDOT =       8803
139334  feet/sec       YDOT =        2763
023459  meter/sec
 ZDOT =       1724
823987                 ZDOT =         560
401693

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13239044
54                 X    =        -4035260
78
 Y    =        4317942
42  feet           Y    =         1316108
85  meter
 Z    =      -17375975
24                 Z    =        -5296197
25
 XDOT =      -9649
252720                 XDOT =       -2941
092229
 YDOT =     -22027
834444  feet/sec       YDOT =       -6714
083939  meter/sec
 ZDOT =       1880
961847                 ZDOT =         573
317171


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   19020
05886592  
00016717  00000-0  10270-3 0  9079
2 25544  51
6391  17
9724 0004596 283
7195  76
3446 15
53170504 32237


Satellite: ISS
Catalog Number: 25544
Epoch time:      19020
05886592   =   yrday
fracday
Element set:     907
Inclination:       51
6391  deg
RA of node:        17
9724  deg
Eccentricity:     
0004596     
Arg of perigee:   283
7195  deg
Mean anomaly:      76
3446  deg
Mean motion:   15
53170504  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3223
Checksum:              320


Coasting Arc #9 (Orbit 3238)
---------------------------------------

Vector Time (GMT): 2019/021/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3133093
51                 A    =         6781742
52  meter
 Y    =        3348126
14  meter          E    =           
0004819
 Z    =        4997336
25                 I    =           51
70928
 XDOT =      -6675
471755                 Wp   =           10
30574
 YDOT =      -3149
235811  meter/sec      RA   =           12
46214  deg
 ZDOT =      -2070
332732                 TA   =           99
84792
                                          MA   =           99
79350
                                          Ha   =            221
258  n
mi
                                          Hp   =            217
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10279178
18                 X    =        -3194574
03
 Y    =       10984665
80  feet           Y    =         3312745
51  meter
 Z    =       16395460
13                 Z    =         4981968
20
 XDOT =     -21901
154051                 XDOT =       -6629
703706
 YDOT =     -10332
138487  feet/sec       YDOT =       -3223
629498  meter/sec
 ZDOT =      -6792
430223                 ZDOT =       -2102
647995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15114072
59                 X    =         4606769
33
 Y    =        -417587
45  feet           Y    =         -127280
65  meter
 Z    =       16325621
90                 Z    =         4976049
55
 XDOT =       8110
038362                 XDOT =        2471
939693
 YDOT =      21660
760474  feet/sec       YDOT =        6602
199792  meter/sec
 ZDOT =      -6937
848359                 ZDOT =       -2114
656180


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   19021
08833941  
00016717  00000-0  10270-3 0  9084
2 25544  51
6386  12
8464 0004509 287
8517  72
2143 15
53130165 32398


Satellite: ISS
Catalog Number: 25544
Epoch time:      19021
08833941   =   yrday
fracday
Element set:     908
Inclination:       51
6386  deg
RA of node:        12
8464  deg
Eccentricity:     
0004509     
Arg of perigee:   287
8517  deg
Mean anomaly:      72
2143  deg
Mean motion:   15
53130165  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3239
Checksum:              306


Coasting Arc #10 (Orbit 3253)
---------------------------------------

Vector Time (GMT): 2019/022/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4324456
33                 A    =         6784229
01  meter
 Y    =       -2900794
42  meter          E    =           
0003976
 Z    =       -4352625
85                 I    =           51
68592
 XDOT =       5852
664258                 Wp   =          108
79321
 YDOT =       3529
308393  meter/sec      RA   =            7
48243  deg
 ZDOT =       3464
030130                 TA   =          196
38349
                                          MA   =          196
39634
                                          Ha   =            221
253  n
mi
                                          Hp   =            217
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14187848
84                 X    =         4377714
47
 Y    =       -9517042
06  feet           Y    =        -2852137
29  meter
 Z    =      -14280268
55                 Z    =        -4331490
68
 XDOT =      19201
654390                 XDOT =        5795
937703
 YDOT =      11579
095779  feet/sec       YDOT =        3594
439579  meter/sec
 ZDOT =      11364
928249                 ZDOT =        3492
321814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16884341
14                 X    =        -5146347
18
 Y    =       -3084659
83  feet           Y    =         -940204
31  meter
 Z    =      -14184467
29                 Z    =        -4323425
63
 XDOT =      -5926
114396                 XDOT =       -1806
279668
 YDOT =     -20387
472132  feet/sec       YDOT =       -6214
101506  meter/sec
 ZDOT =      11492
130727                 ZDOT =        3502
801445


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   19022
05346789  
00016717  00000-0  10270-3 0  9092
2 25544  51
6394   8
0428 0004585 291
4174  68
6488 15
53161727 32544


Satellite: ISS
Catalog Number: 25544
Epoch time:      19022
05346789   =   yrday
fracday
Element set:     909
Inclination:       51
6394  deg
RA of node:         8
0428  deg
Eccentricity:     
0004585     
Arg of perigee:   291
4174  deg
Mean anomaly:      68
6488  deg
Mean motion:   15
53161727  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3254
Checksum:              330


Coasting Arc #11 (Orbit 3269)
---------------------------------------

Vector Time (GMT): 2019/023/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5338626
77                 A    =         6787398
38  meter
 Y    =        2452548
81  meter          E    =           
0008477
 Z    =        3393595
34                 I    =           51
66343
 XDOT =      -4728
357610                 Wp   =           78
08431
 YDOT =      -3871
168335  meter/sec      RA   =            2
50588  deg
 ZDOT =      -4629
215342                 TA   =           62
29682
                                          MA   =           62
21084
                                          Ha   =            221
350  n
mi
                                          Hp   =            217
803

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17515179
68                 X    =        -5382138
81
 Y    =        8046419
98  feet           Y    =         2392605
18  meter
 Z    =       11133842
99                 Z    =         3367557
43
 XDOT =     -15512
984284                 XDOT =       -4662
232189
 YDOT =     -12700
683514  feet/sec       YDOT =       -3923
674269  meter/sec
 ZDOT =     -15187
714378                 ZDOT =       -4652
022775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18347077
79                 X    =         5592189
31
 Y    =        6125494
48  feet           Y    =         1867050
72  meter
 Z    =       11015984
17                 Z    =         3357671
97
 XDOT =       3038
838668                 XDOT =         926
238026
 YDOT =      18464
125266  feet/sec       YDOT =        5627
865381  meter/sec
 ZDOT =     -15290
114605                 ZDOT =       -4660
426932


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   19023
08293871  
00016717  00000-0  10270-3 0  9101
2 25544  51
6395   2
9178 0004617 294
2978  65
7692 15
53151143 32703


Satellite: ISS
Catalog Number: 25544
Epoch time:      19023
08293871   =   yrday
fracday
Element set:     910
Inclination:       51
6395  deg
RA of node:         2
9178  deg
Eccentricity:     
0004617     
Arg of perigee:   294
2978  deg
Mean anomaly:      65
7692  deg
Mean motion:   15
53151143  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3270
Checksum:              318


Coasting Arc #12 (Orbit 3284)
---------------------------------------

Vector Time (GMT): 2019/024/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6088239
54                 A    =         6790110
59  meter
 Y    =       -2017584
53  meter          E    =           
0006900
 Z    =       -2216023
52                 I    =           51
64120
 XDOT =       3373
938490                 Wp   =             
63998
 YDOT =       4184
843322  meter/sec      RA   =          357
53442  deg
 ZDOT =       5466
265841                 TA   =          334
74862
                                          MA   =          334
78233
                                          Ha   =            221
514  n
mi
                                          Hp   =            217
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19974539
17                 X    =         6121112
18
 Y    =       -6619371
80  feet           Y    =        -1949317
78  meter
 Z    =       -7270418
37                 Z    =        -2186370
08
 XDOT =      11069
352000                 XDOT =        3300
340257
 YDOT =      13729
800925  feet/sec       YDOT =        4222
161540  meter/sec
 ZDOT =      17933
943048                 ZDOT =        5482
475985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19300214
19                 X    =        -5882705
28
 Y    =       -8498943
71  feet           Y    =        -2590478
04  meter
 Z    =       -7136313
45                 Z    =        -2175148
34
 XDOT =        450
035474                 XDOT =         137
170812
 YDOT =     -16122
151433  feet/sec       YDOT =       -4914
031757  meter/sec
 ZDOT =      18006
523706                 ZDOT =        5488
388426


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   19024
04806487  
00016717  00000-0  10270-3 0  9112
2 25544  51
6412 358
1137 0004659 299
7091  60
3597 15
53169889 32853


Satellite: ISS
Catalog Number: 25544
Epoch time:      19024
04806487   =   yrday
fracday
Element set:     911
Inclination:       51
6412  deg
RA of node:       358
1137  deg
Eccentricity:     
0004659     
Arg of perigee:   299
7091  deg
Mean anomaly:      60
3597  deg
Mean motion:   15
53169889  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3285
Checksum:              339


Coasting Arc #13 (Orbit 3300)
---------------------------------------

Vector Time (GMT): 2019/025/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6552033
19                 A    =         6791807
87  meter
 Y    =        1546519
23  meter          E    =           
0008710
 Z    =         865714
30                 I    =           51
61316
 XDOT =      -1848
950872                 Wp   =          127
16501
 YDOT =      -4494
801544  meter/sec      RA   =          352
56636  deg
 ZDOT =      -5927
973487                 TA   =           43
47023
                                          MA   =           43
40160
                                          Ha   =            221
549  n
mi
                                          Hp   =            217
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21496171
88                 X    =        -6573044
91
 Y    =        5073881
98  feet           Y    =         1473132
35  meter
 Z    =        2840270
01                 Z    =          833836
64
 XDOT =      -6066
111785                 XDOT =       -1769
757163
 YDOT =     -14746
724226  feet/sec       YDOT =       -4515
035093  meter/sec
 ZDOT =     -19448
731913                 ZDOT =       -5936
762384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19552596
24                 X    =         5959631
34
 Y    =       10311317
77  feet           Y    =         3142889
66  meter
 Z    =        2696205
38                 Z    =          821803
40
 XDOT =      -4463
623998                 XDOT =       -1360
512595
 YDOT =      13592
238051  feet/sec       YDOT =        4142
914158  meter/sec
 ZDOT =     -19487
779015                 ZDOT =       -5939
875044


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   19025
07753157  
00016717  00000-0  10270-3 0  9122
2 25544  51
6405 352
9896 0004656 303
5351  56
5356 15
53177678 33013


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
07753157   =   yrday
fracday
Element set:     912
Inclination:       51
6405  deg
RA of node:       352
9896  deg
Eccentricity:     
0004656     
Arg of perigee:   303
5351  deg
Mean anomaly:      56
5356  deg
Mean motion:   15
53177678  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3301
Checksum:              319


Coasting Arc #14 (Orbit 3308)
---------------------------------------

Vector Time (GMT): 2019/025/12:55:30
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4060136
58                 A    =         6783115
20  meter
 Y    =        2960978
54  meter          E    =           
0003984
 Z    =        4552865
75                 I    =           51
56783
 XDOT =      -6055
953289                 Wp   =           94
17228
 YDOT =       3544
102569  meter/sec      RA   =          350
13646  deg
 ZDOT =       3093
009432                 TA   =          324
82304
                                          MA   =          324
84933
                                          Ha   =            221
599  n
mi
                                          Hp   =            217
517

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13320658
07                 X    =         4004609
48
 Y    =        9714496
52  feet           Y    =         3006071
43  meter
 Z    =       14937223
60                 Z    =         4572453
06
 XDOT =     -19868
613152                 XDOT =       -6110
158171
 YDOT =      11627
633100  feet/sec       YDOT =        3476
077655  meter/sec
 ZDOT =      10147
668739                 ZDOT =        3063
460765

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3193825
03                 X    =          973477
87
 Y    =       16092689
00  feet           Y    =         4905051
61  meter
 Z    =       15025207
66                 Z    =         4579683
29
 XDOT =     -21383
990261                 XDOT =       -6517
840231
 YDOT =      -5113
615911  feet/sec       YDOT =       -1558
630130  meter/sec
 ZDOT =      10013
848294                 ZDOT =        3052
220960


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   19025
59226340  
00016717  00000-0  10270-3 0  9139
2 25544  51
6400 350
4317 0004980 309
1721  50
8988 15
53207744 33096


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
59226340   =   yrday
fracday
Element set:     913
Inclination:       51
6400  deg
RA of node:       350
4317  deg
Eccentricity:     
0004980     
Arg of perigee:   309
1721  deg
Mean anomaly:      50
8988  deg
Mean motion:   15
53207744  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3309
Checksum:              299


Coasting Arc #15 (Orbit 3321)
---------------------------------------

Vector Time (GMT): 2019/026/08:59:00
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4592363
79                 A    =         6783957
71  meter
 Y    =        2422975
74  meter          E    =           
0005360
 Z    =        4361162
40                 I    =           51
54198
 XDOT =      -5452
809776                 Wp   =           87
45205
 YDOT =       4165
489121  meter/sec      RA   =          345
97313  deg
 ZDOT =       3424
212794                 TA   =          327
76632
                                          MA   =          327
79906
                                          Ha   =            221
794  n
mi
                                          Hp   =            217
436

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15066810
34                 X    =         4543744
34
 Y    =        7949395
49  feet           Y    =         2474058
98  meter
 Z    =       14308275
59                 Z    =         4383351
88
 XDOT =     -17889
795853                 XDOT =       -5515
616828
 YDOT =      13666
302890  feet/sec       YDOT =        4104
160880  meter/sec
 ZDOT =      11234
293943                 ZDOT =        3397
572928

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10606641
65                 X    =        -3232904
38
 Y    =       13222522
19  feet           Y    =         4030224
76  meter
 Z    =       14408069
70                 Z    =         4391579
64
 XDOT =      -9107
163589                 XDOT =       -2775
863462
 YDOT =     -19427
520206  feet/sec       YDOT =       -5921
508159  meter/sec
 ZDOT =      11113
525881                 ZDOT =        3387
402689


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   19026
42870485  
00016717  00000-0  10270-3 0  9148
2 25544  51
6390 346
2679 0004860 313
5493  46
5255 15
53164039 33223


Satellite: ISS
Catalog Number: 25544
Epoch time:      19026
42870485   =   yrday
fracday
Element set:     914
Inclination:       51
6390  deg
RA of node:       346
2679  deg
Eccentricity:     
0004860     
Arg of perigee:   313
5493  deg
Mean anomaly:      46
5255  deg
Mean motion:   15
53164039  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3322
Checksum:              315


Coasting Arc #16 (Orbit 3336)
---------------------------------------

Vector Time (GMT): 2019/027/08:59:00
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3453483
88                 A    =         6781419
20  meter
 Y    =       -3019730
07  meter          E    =           
0011479
 Z    =       -5004320
10                 I    =           51
50199
 XDOT =       6298
732230                 Wp   =           53
15425
 YDOT =      -3863
732097  meter/sec      RA   =          340
98049  deg
 ZDOT =      -2011
753922                 TA   =          197
21423
                                          MA   =          197
25319
                                          Ha   =            222
025  n
mi
                                          Hp   =            217
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11330327
67                 X    =        -3395151
87
 Y    =       -9907250
89  feet           Y    =        -3058023
21  meter
 Z    =      -16418373
03                 Z    =        -5020953
90
 XDOT =      20665
131989                 XDOT =        6351
241285
 YDOT =     -12676
286408  feet/sec       YDOT =       -3793
001698  meter/sec
 ZDOT =      -6600
242527                 ZDOT =       -1981
029916

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11670180
98                 X    =         3557071
16
 Y    =       -9374447
78  feet           Y    =        -2857331
68  meter
 Z    =      -16493014
37                 Z    =        -5027070
78
 XDOT =       8291
698191                 XDOT =        2527
309609
 YDOT =      21709
967819  feet/sec       YDOT =        6617
198191  meter/sec
 ZDOT =      -6461
100172                 ZDOT =       -1969
343333


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   19027
39382636  
00016717  00000-0  10270-3 0  9152
2 25544  51
6394 341
4639 0004780 318
2479  41
8308 15
53175743 33374


Satellite: ISS
Catalog Number: 25544
Epoch time:      19027
39382636   =   yrday
fracday
Element set:     915
Inclination:       51
6394  deg
RA of node:       341
4639  deg
Eccentricity:     
0004780     
Arg of perigee:   318
2479  deg
Mean anomaly:      41
8308  deg
Mean motion:   15
53175743  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3337
Checksum:              330


Coasting Arc #17 (Orbit 3352)
---------------------------------------

Vector Time (GMT): 2019/028/08:59:00
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2188289
78                 A    =         6780191
07  meter
 Y    =        3635818
79  meter          E    =           
0003094
 Z    =        5288322
67                 I    =           51
46553
 XDOT =      -6833
149168                 Wp   =          349
22462
 YDOT =       3446
840031  meter/sec      RA   =          335
98074  deg
 ZDOT =        460
791105                 TA   =           96
38658
                                          MA   =           96
35134
                                          Ha   =            222
125  n
mi
                                          Hp   =            217
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7179428
40                 X    =         2121782
98
 Y    =       11928539
34  feet           Y    =         3659917
87  meter
 Z    =       17350139
99                 Z    =         5298790
92
 XDOT =     -22418
468399                 XDOT =       -6873
423092
 YDOT =      11308
530287  feet/sec       YDOT =        3370
201805  meter/sec
 ZDOT =       1511
781840                 ZDOT =         427
500859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12869319
53                 X    =        -3922568
59
 Y    =        5156625
93  feet           Y    =         1571739
58  meter
 Z    =       17396879
73                 Z    =         5302568
94
 XDOT =      -7371
153172                 XDOT =       -2246
727487
 YDOT =     -22954
745743  feet/sec       YDOT =       -6996
606503  meter/sec
 ZDOT =       1361
129030                 ZDOT =         414
872128


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   19028
42328729  
00016717  00000-0  10270-3 0  9161
2 25544  51
6382 336
3390 0004944 321
7154  38
3647 15
53171978 33530


Satellite: ISS
Catalog Number: 25544
Epoch time:      19028
42328729   =   yrday
fracday
Element set:     916
Inclination:       51
6382  deg
RA of node:       336
3390  deg
Eccentricity:     
0004944     
Arg of perigee:   321
7154  deg
Mean anomaly:      38
3647  deg
Mean motion:   15
53171978  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3353
Checksum:              325


Coasting Arc #18 (Orbit 3367)
---------------------------------------

Vector Time (GMT): 2019/029/08:59:00
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -914478
66                 A    =         6780614
68  meter
 Y    =       -4247390
75  meter          E    =           
0011339
 Z    =       -5215137
31                 I    =           51
43666
 XDOT =       7011
476078                 Wp   =           79
92519
 YDOT =      -2873
526272  meter/sec      RA   =          330
97857  deg
 ZDOT =       1114
847045                 TA   =          200
78033
                                          MA   =          200
82646
                                          Ha   =            222
289  n
mi
                                          Hp   =            217
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3000258
08                 X    =         -841583
27
 Y    =      -13935009
03  feet           Y    =        -4257209
39  meter
 Z    =      -17110030
54                 Z    =        -5219402
49
 XDOT =      23003
530441                 XDOT =        7037
672318
 YDOT =      -9427
579631  feet/sec       YDOT =       -2794
972610  meter/sec
 ZDOT =       3657
634661                 ZDOT =        1148
969283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14199072
00                 X    =         4327877
15
 Y    =        -965912
05  feet           Y    =         -294409
99  meter
 Z    =      -17128705
10                 Z    =        -5220829
32
 XDOT =       6147
930116                 XDOT =        1873
889099
 YDOT =      23010
811451  feet/sec       YDOT =        7013
695330  meter/sec
 ZDOT =       3811
954469                 ZDOT =        1161
883722


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   19029
38840601  
00016717  00000-0  10270-3 0  9176
2 25544  51
6380 331
5353 0004968 325
4799  34
6030 15
53162305 33681


Satellite: ISS
Catalog Number: 25544
Epoch time:      19029
38840601   =   yrday
fracday
Element set:     917
Inclination:       51
6380  deg
RA of node:       331
5353  deg
Eccentricity:     
0004968     
Arg of perigee:   325
4799  deg
Mean anomaly:      34
6030  deg
Mean motion:   15
53162305  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3368
Checksum:              311
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