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

 
Date: January 26th 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


026/08:58:30 000 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

033/17:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 216 5

040/11:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 215 6

Coasting Arc #1 (Orbit 3309)
---------------------------------------

Vector Time (GMT): 2019/025/14:35:17
515
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1130828
90                 A    =         6780015
64  meter
 Y    =        4072952
86  meter          E    =           
0003057
 Z    =        5302110
68                 I    =           51
55598
 XDOT =      -7483
224382                 Wp   =          332
57603
 YDOT =       1630
050789  meter/sec      RA   =          349
77013  deg
 ZDOT =        346
585143                 TA   =          114
13099
                                          MA   =          114
09901
                                          Ha   =            221
732  n
mi
                                          Hp   =            217
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3710068
58                 X    =         1059445
76
 Y    =       13362706
23  feet           Y    =         4085199
55  meter
 Z    =       17395376
25                 Z    =         5307430
27
 XDOT =     -24551
261097                 XDOT =       -7502
579390
 YDOT =       5347
935658  feet/sec       YDOT =        1546
259942  meter/sec
 ZDOT =       1137
090364                 ZDOT =         310
188136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -578371
87                 X    =         -176287
75
 Y    =       13826627
25  feet           Y    =         4214355
99  meter
 Z    =       17418826
21                 Z    =         5309258
23
 XDOT =     -24023
708654                 XDOT =       -7322
426398
 YDOT =      -2218
946258  feet/sec       YDOT =        -676
334819  meter/sec
 ZDOT =        972
628735                 ZDOT =         296
457238


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
65661760  
00016717  00000-0  10270-3 0  9001
2 25544  51
6409 350
1103 0005083 310
9371  49
1341 15
53222627 33104


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
65661760   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       350
1103  deg
Eccentricity:     
0005083     
Arg of perigee:   310
9371  deg
Mean anomaly:      49
1341  deg
Mean motion:   15
53222627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3310
Checksum:              269


Coasting Arc #2 (Orbit 3321)
---------------------------------------

Vector Time (GMT): 2019/026/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4755665
95                 A    =         6784299
71  meter
 Y    =        2294525
06  meter          E    =           
0005948
 Z    =        4254272
97                 I    =           51
54321
 XDOT =      -5270
997619                 Wp   =           84
75271
 YDOT =       4257
442309  meter/sec      RA   =          345
97319  deg
 ZDOT =       3592
185527                 TA   =          328
49126
                                          MA   =          328
52687
                                          Ha   =            221
795  n
mi
                                          Hp   =            217
390

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15602578
58                 X    =         4708989
93
 Y    =        7527969
35  feet           Y    =         2347445
32  meter
 Z    =       13957588
49                 Z    =         4277260
42
 XDOT =     -17293
299274                 XDOT =       -5335
662334
 YDOT =      13967
986578  feet/sec       YDOT =        4198
136834  meter/sec
 ZDOT =      11785
385588                 ZDOT =        3566
424309

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10323338
16                 X    =        -3146553
47
 Y    =       13807317
24  feet           Y    =         4208470
30  meter
 Z    =       14061000
57                 Z    =         4285792
97
 XDOT =      -9428
584817                 XDOT =       -2873
832652
 YDOT =     -18945
038579  feet/sec       YDOT =       -5774
447759  meter/sec
 ZDOT =      11668
569658                 ZDOT =        3556
580032


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
42870957  
00016717  00000-0  10270-3 0  9018
2 25544  51
6390 346
2659 0004875 314
3931  45
6822 15
53180197 33226


Satellite: ISS
Catalog Number: 25544
Epoch time:      19026
42870957   =   yrday
fracday
Element set:     901
Inclination:       51
6390  deg
RA of node:       346
2659  deg
Eccentricity:     
0004875     
Arg of perigee:   314
3931  deg
Mean anomaly:      45
6822  deg
Mean motion:   15
53180197  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3322
Checksum:              318


Coasting Arc #3 (Orbit 3336)
---------------------------------------

Vector Time (GMT): 2019/027/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3638313
64                 A    =         6781630
92  meter
 Y    =       -2903421
45  meter          E    =           
0011286
 Z    =       -4941906
04                 I    =           51
50276
 XDOT =       6165
003549                 Wp   =           51
04858
 YDOT =      -3975
512624  meter/sec      RA   =          340
98110  deg
 ZDOT =      -2199
568234                 TA   =          197
40258
                                          MA   =          197
44129
                                          Ha   =            222
034  n
mi
                                          Hp   =            217
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11936724
56                 X    =        -3581571
67
 Y    =       -9525660
93  feet           Y    =        -2943790
38  meter
 Z    =      -16213602
49                 Z    =        -4959441
52
 XDOT =      20226
389598                 XDOT =        6219
684789
 YDOT =     -13043
020421  feet/sec       YDOT =       -3906
265529  meter/sec
 ZDOT =      -7216
431213                 ZDOT =       -2169
488546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11419276
94                 X    =         3480595
61
 Y    =      -10013225
53  feet           Y    =        -3052031
14  meter
 Z    =      -16292327
75                 Z    =        -4965901
50
 XDOT =       8631
806922                 XDOT =        2630
974750
 YDOT =      21382
792581  feet/sec       YDOT =        6517
475179  meter/sec
 ZDOT =      -7080
180825                 ZDOT =       -2158
039115


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
39382193  
00016717  00000-0  10270-3 0  9026
2 25544  51
6394 341
4618 0004792 319
2322  40
8471 15
53191687 33377


Satellite: ISS
Catalog Number: 25544
Epoch time:      19027
39382193   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:       341
4618  deg
Eccentricity:     
0004792     
Arg of perigee:   319
2322  deg
Mean anomaly:      40
8471  deg
Mean motion:   15
53191687  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3337
Checksum:              317


Coasting Arc #4 (Orbit 3352)
---------------------------------------

Vector Time (GMT): 2019/028/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2384022
34                 A    =         6780217
87  meter
 Y    =        3534507
21  meter          E    =           
0002749
 Z    =        5272177
89                 I    =           51
46567
 XDOT =      -6749
089066                 Wp   =          351
89333
 YDOT =       3578
843399  meter/sec      RA   =          335
98158  deg
 ZDOT =        655
292166                 TA   =           91
84986
                                          MA   =           91
81837
                                          Ha   =            222
130  n
mi
                                          Hp   =            217
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7821595
59                 X    =         2318712
31
 Y    =       11596152
25  feet           Y    =         3560801
80  meter
 Z    =       17297171
56                 Z    =         5283599
83
 XDOT =     -22142
680664                 XDOT =       -6791
790103
 YDOT =      11741
612200  feet/sec       YDOT =        3503
131618  meter/sec
 ZDOT =       2149
908680                 ZDOT =         622
404353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12651805
13                 X    =        -3856270
20
 Y    =        5814729
40  feet           Y    =         1772329
52  meter
 Z    =       17348227
51                 Z    =         5287739
74
 XDOT =      -7740
859553                 XDOT =       -2359
413992
 YDOT =     -22786
410931  feet/sec       YDOT =       -6945
298052  meter/sec
 ZDOT =       2001
053738                 ZDOT =         609
921179


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
42327319  
00016717  00000-0  10270-3 0  9031
2 25544  51
6383 336
3369 0004955 322
6712  37
4095 15
53185346 33530


Satellite: ISS
Catalog Number: 25544
Epoch time:      19028
42327319   =   yrday
fracday
Element set:     903
Inclination:       51
6383  deg
RA of node:       336
3369  deg
Eccentricity:     
0004955     
Arg of perigee:   322
6712  deg
Mean anomaly:      37
4095  deg
Mean motion:   15
53185346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3353
Checksum:              315


Coasting Arc #5 (Orbit 3367)
---------------------------------------

Vector Time (GMT): 2019/029/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1110521
14                 A    =         6780440
24  meter
 Y    =       -4164772
64  meter          E    =           
0011711
 Z    =       -5243729
65                 I    =           51
43614
 XDOT =       6975
302063                 Wp   =           78
42074
 YDOT =      -3023
505221  meter/sec      RA   =          330
97918  deg
 ZDOT =        928
215023                 TA   =          200
47245
                                          MA   =          200
51942
                                          Ha   =            222
293  n
mi
                                          Hp   =            217
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3643442
07                 X    =        -1038396
16
 Y    =      -13663952
24  feet           Y    =        -4176787
88  meter
 Z    =      -17203837
42                 Z    =        -5248948
98
 XDOT =      22884
849288                 XDOT =        7004
084641
 YDOT =      -9919
636552  feet/sec       YDOT =       -2945
341618  meter/sec
 ZDOT =       3045
324880                 ZDOT =         962
167823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14021374
49                 X    =         4273714
95
 Y    =       -1608649
67  feet           Y    =         -490316
42  meter
 Z    =      -17226827
52                 Z    =        -5250737
03
 XDOT =       6551
647639                 XDOT =        1996
942200
 YDOT =      22991
741713  feet/sec       YDOT =        7007
882874  meter/sec
 ZDOT =       3198
900316                 ZDOT =         975
024816


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
38838274  
00016717  00000-0  10270-3 0  9045
2 25544  51
6381 331
5330 0004977 326
3306  33
7530 15
53176986 33686


Satellite: ISS
Catalog Number: 25544
Epoch time:      19029
38838274   =   yrday
fracday
Element set:     904
Inclination:       51
6381  deg
RA of node:       331
5330  deg
Eccentricity:     
0004977     
Arg of perigee:   326
3306  deg
Mean anomaly:      33
7530  deg
Mean motion:   15
53176986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3368
Checksum:              325


Coasting Arc #6 (Orbit 3383)
---------------------------------------

Vector Time (GMT): 2019/030/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -154546
08                 A    =         6782131
79  meter
 Y    =        4756350
24  meter          E    =           
0008720
 Z    =        4832209
55                 I    =           51
41376
 XDOT =      -6892
100663                 Wp   =           24
45801
 YDOT =       2284
771380  meter/sec      RA   =          325
97598  deg
 ZDOT =      -2459
947207                 TA   =           89
82830
                                          MA   =           89
72837
                                          Ha   =            222
403  n
mi
                                          Hp   =            216
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -507040
95                 X    =         -231193
28
 Y    =       15604823
64  feet           Y    =         4754193
28  meter
 Z    =       15853705
87                 Z    =         4831272
83
 XDOT =     -22611
878815                 XDOT =       -6905
188512
 YDOT =       7495
969096  feet/sec       YDOT =        2207
626009  meter/sec
 ZDOT =      -8070
692937                 ZDOT =       -2493
457656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15417229
22                 X    =        -4699171
47
 Y    =       -2496116
65  feet           Y    =         -760816
36  meter
 Z    =       15848849
99                 Z    =         4830729
48
 XDOT =      -4893
912201                 XDOT =       -1491
664439
 YDOT =     -22174
185792  feet/sec       YDOT =       -6758
691829  meter/sec
 ZDOT =      -8222
166820                 ZDOT =       -2506
116447


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   19030
41783043  
00016717  00000-0  10270-3 0  9055
2 25544  51
6384 326
4080 0005060 329
5869  30
4989 15
53203823 33848


Satellite: ISS
Catalog Number: 25544
Epoch time:      19030
41783043   =   yrday
fracday
Element set:     905
Inclination:       51
6384  deg
RA of node:       326
4080  deg
Eccentricity:     
0005060     
Arg of perigee:   329
5869  deg
Mean anomaly:      30
4989  deg
Mean motion:   15
53203823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3384
Checksum:              307


Coasting Arc #7 (Orbit 3398)
---------------------------------------

Vector Time (GMT): 2019/031/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1286556
46                 A    =         6784994
38  meter
 Y    =       -5254187
50  meter          E    =           
0005262
 Z    =       -4098109
37                 I    =           51
39667
 XDOT =       6510
373856                 Wp   =           63
89037
 YDOT =      -1367
687528  meter/sec      RA   =          320
97677  deg
 ZDOT =       3803
451742                 TA   =          245
51133
                                          MA   =          245
56621
                                          Ha   =            222
591  n
mi
                                          Hp   =            216
799

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4220985
75                 X    =         1365120
62
 Y    =      -17238147
96  feet           Y    =        -5239360
89  meter
 Z    =      -13445240
73                 Z    =        -4091669
27
 XDOT =      21359
494279                 XDOT =        6506
709142
 YDOT =      -4487
163805  feet/sec       YDOT =       -1294
904632  meter/sec
 ZDOT =      12478
516215                 ZDOT =        3835
067172

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16698140
58                 X    =         5089593
25
 Y    =        6077946
21  feet           Y    =         1852558
00  meter
 Z    =      -13415499
80                 Z    =        -4089044
34
 XDOT =       2695
459546                 XDOT =         821
576070
 YDOT =      20408
858903  feet/sec       YDOT =        6220
620194  meter/sec
 ZDOT =      12621
315000                 ZDOT =        3846
976812


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   19031
38293550  
00016717  00000-0  10270-3 0  9062
2 25544  51
6389 321
6039 0005146 334
5318  25
5580 15
53184292 33990


Satellite: ISS
Catalog Number: 25544
Epoch time:      19031
38293550   =   yrday
fracday
Element set:     906
Inclination:       51
6389  deg
RA of node:       321
6039  deg
Eccentricity:     
0005146     
Arg of perigee:   334
5318  deg
Mean anomaly:      25
5580  deg
Mean motion:   15
53184292  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3399
Checksum:              316


Coasting Arc #8 (Orbit 3414)
---------------------------------------

Vector Time (GMT): 2019/032/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2297076
35                 A    =         6788093
70  meter
 Y    =        5608881
42  meter          E    =           
0011531
 Z    =        3051170
95                 I    =           51
38174
 XDOT =      -5894
124799                 Wp   =           72
59291
 YDOT =        258
739730  meter/sec      RA   =          315
98247  deg
 ZDOT =      -4894
312289                 TA   =           72
27275
                                          MA   =           72
14692
                                          Ha   =            222
678  n
mi
                                          Hp   =            216
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7536339
72                 X    =        -2374446
29
 Y    =       18401841
93  feet           Y    =         5582761
19  meter
 Z    =       10010403
37                 Z    =         3039825
16
 XDOT =     -19337
679788                 XDOT =       -5872
806700
 YDOT =        848
883630  feet/sec       YDOT =         192
946911  meter/sec
 ZDOT =     -16057
455016                 ZDOT =       -4922
891338

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17673705
87                 X    =        -5386945
55
 Y    =       -9170651
64  feet           Y    =        -2795214
62  meter
 Z    =        9958496
26                 Z    =         3035349
66
 XDOT =        154
722488                 XDOT =          47
159414
 YDOT =     -17942
188226  feet/sec       YDOT =       -5468
778971  meter/sec
 ZDOT =     -16186
408982                 ZDOT =       -4933
617458


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   19032
41237957  
00016717  00000-0  10270-3 0  9077
2 25544  51
6385 316
4791 0005227 337
8424  22
2501 15
53212727 34158


Satellite: ISS
Catalog Number: 25544
Epoch time:      19032
41237957   =   yrday
fracday
Element set:     907
Inclination:       51
6385  deg
RA of node:       316
4791  deg
Eccentricity:     
0005227     
Arg of perigee:   337
8424  deg
Mean anomaly:      22
2501  deg
Mean motion:   15
53212727  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3415
Checksum:              299


Coasting Arc #9 (Orbit 3429)
---------------------------------------

Vector Time (GMT): 2019/033/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3086139
31                 A    =         6790640
10  meter
 Y    =       -5762779
89  meter          E    =           
0011065
 Z    =       -1815343
42                 I    =           51
36738
 XDOT =       5115
802011                 Wp   =           15
12263
 YDOT =        972
130984  meter/sec      RA   =          310
99350  deg
 ZDOT =       5629
246634                 TA   =          324
84629
                                          MA   =          324
91925
                                          Ha   =            222
770  n
mi
                                          Hp   =            216
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10125128
98                 X    =         3159168
69
 Y    =      -18906758
16  feet           Y    =        -5727860
13  meter
 Z    =       -5955851
13                 Z    =        -1800175
30
 XDOT =      16784
127334                 XDOT =        5077
208075
 YDOT =       3189
406115  feet/sec       YDOT =        1029
123470  meter/sec
 ZDOT =      18468
656936                 ZDOT =        5654
002970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18153976
01                 X    =         5533331
89
 Y    =       11455823
49  feet           Y    =         3491735
00  meter
 Z    =       -5886694
07                 Z    =        -1794264
35
 XDOT =      -3507
011896                 XDOT =       -1068
937226
 YDOT =      15074
059553  feet/sec       YDOT =        4594
573352  meter/sec
 ZDOT =      18580
208465                 ZDOT =        5663
247540


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   19033
37748206  
00016717  00000-0  10270-3 0  9088
2 25544  51
6388 311
6752 0005164 341
4198  18
6765 15
53208020 34303


Satellite: ISS
Catalog Number: 25544
Epoch time:      19033
37748206   =   yrday
fracday
Element set:     908
Inclination:       51
6388  deg
RA of node:       311
6752  deg
Eccentricity:     
0005164     
Arg of perigee:   341
4198  deg
Mean anomaly:      18
6765  deg
Mean motion:   15
53208020  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3430
Checksum:              305


Coasting Arc #10 (Orbit 3435)
---------------------------------------

Vector Time (GMT): 2019/033/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1920925
05                 A    =         6788612
50  meter
 Y    =        5880361
41  meter          E    =           
0011573
 Z    =        2789822
76                 I    =           51
35452
 XDOT =      -5706
981440                 Wp   =           76
51005
 YDOT =        558
827436  meter/sec      RA   =          309
22745  deg
 ZDOT =      -5086
934860                 TA   =           71
72962
                                          MA   =           71
60373
                                          Ha   =            222
697  n
mi
                                          Hp   =            216
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6302247
52                 X    =        -2000089
20
 Y    =       19292524
32  feet           Y    =         5858437
57  meter
 Z    =        9152961
80                 Z    =         2780299
76
 XDOT =     -18723
692389                 XDOT =       -5688
097384
 YDOT =       1833
423345  feet/sec       YDOT =         495
113726  meter/sec
 ZDOT =     -16689
418833                 ZDOT =       -5114
610648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5164674
61                 X    =         1574192
82
 Y    =       19648003
73  feet           Y    =         5988711
54  meter
 Z    =        9109259
79                 Z    =         2776502
38
 XDOT =     -13182
261400                 XDOT =       -4017
953275
 YDOT =      11291
901609  feet/sec       YDOT =        3441
771610  meter/sec
 ZDOT =     -16814
334238                 ZDOT =       -5125
009076


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   19033
76351947  
00016717  00000-0  10270-3 0  9094
2 25544  51
6399 309
7519 0005440 339
2592  20
8339 15
53253322 34367


Satellite: ISS
Catalog Number: 25544
Epoch time:      19033
76351947   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       309
7519  deg
Eccentricity:     
0005440     
Arg of perigee:   339
2592  deg
Mean anomaly:      20
8339  deg
Mean motion:   15
53253322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3436
Checksum:              325


Coasting Arc #11 (Orbit 3450)
---------------------------------------

Vector Time (GMT): 2019/034/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2653679
96                 A    =         6791041
20  meter
 Y    =       -6056570
54  meter          E    =           
0012126
 Z    =       -1517065
62                 I    =           51
34056
 XDOT =       5028
276108                 Wp   =           17
38985
 YDOT =        771
473645  meter/sec      RA   =          304
23654  deg
 ZDOT =       5738
857157                 TA   =          325
96951
                                          MA   =          326
04721
                                          Ha   =            222
845  n
mi
                                          Hp   =            216
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8706299
09                 X    =         2728577
87
 Y    =      -19870638
25  feet           Y    =        -6026476
44  meter
 Z    =       -4977249
42                 Z    =        -1503993
58
 XDOT =      16496
968858                 XDOT =        4991
400159
 YDOT =       2531
081513  feet/sec       YDOT =         827
497064  meter/sec
 ZDOT =      18828
271513                 ZDOT =        5763
192408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3854081
08                 X    =        -1174723
91
 Y    =      -21363025
66  feet           Y    =        -6511450
22  meter
 Z    =       -4917531
27                 Z    =        -1498863
53
 XDOT =      13434
332057                 XDOT =        4094
784411
 YDOT =      -6765
207753  feet/sec       YDOT =       -2062
035323  meter/sec
 ZDOT =      18937
950862                 ZDOT =        5772
287423


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   19034
72862036  
00016717  00000-0  10270-3 0  9109
2 25544  51
6384 304
9469 0005181 344
5550  15
5444 15
53212064 34510


Satellite: ISS
Catalog Number: 25544
Epoch time:      19034
72862036   =   yrday
fracday
Element set:     910
Inclination:       51
6384  deg
RA of node:       304
9469  deg
Eccentricity:     
0005181     
Arg of perigee:   344
5550  deg
Mean anomaly:      15
5444  deg
Mean motion:   15
53212064  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3451
Checksum:              293


Coasting Arc #12 (Orbit 3466)
---------------------------------------

Vector Time (GMT): 2019/035/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3243326
85                 A    =         6791828
30  meter
 Y    =        5963924
49  meter          E    =           
0008426
 Z    =         105247
00                 I    =           51
32545
 XDOT =      -4254
586932                 Wp   =          111
75609
 YDOT =      -2201
419922  meter/sec      RA   =          299
24942  deg
 ZDOT =      -5981
560406                 TA   =           67
10621
                                          MA   =           67
01728
                                          Ha   =            222
934  n
mi
                                          Hp   =            216
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10640836
13                 X    =        -3310287
31
 Y    =       19566681
38  feet           Y    =         5927280
94  meter
 Z    =         345298
56                 Z    =           89329
95
 XDOT =     -13958
618544                 XDOT =       -4200
599570
 YDOT =      -7222
506307  feet/sec       YDOT =       -2248
695833  meter/sec
 ZDOT =     -19624
542013                 ZDOT =       -6002
095869

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2486473
01                 X    =          757876
97
 Y    =       22134694
27  feet           Y    =         6746654
81  meter
 Z    =         272775
43                 Z    =           83141
95
 XDOT =     -13857
544193                 XDOT =       -4223
779470
 YDOT =       1819
282624  feet/sec       YDOT =         554
517344  meter/sec
 ZDOT =     -19716
908924                 ZDOT =       -6009
713840


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   19035
75805743  
00016717  00000-0  10270-3 0  9116
2 25544  51
6379 299
8225 0005413 348
8712  11
2320 15
53266801 34672


Satellite: ISS
Catalog Number: 25544
Epoch time:      19035
75805743   =   yrday
fracday
Element set:     911
Inclination:       51
6379  deg
RA of node:       299
8225  deg
Eccentricity:     
0005413     
Arg of perigee:   348
8712  deg
Mean anomaly:      11
2320  deg
Mean motion:   15
53266801  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3467
Checksum:              312


Coasting Arc #13 (Orbit 3482)
---------------------------------------

Vector Time (GMT): 2019/036/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3639969
69                 A    =         6791274
53  meter
 Y    =       -5576178
74  meter          E    =           
0016433
 Z    =        1282683
37                 I    =           51
30704
 XDOT =       3475
171633                 Wp   =           42
67376
 YDOT =       3611
973229  meter/sec      RA   =          294
26028  deg
 ZDOT =       5808
569954                 TA   =          331
35070
                                          MA   =          331
44089
                                          Ha   =            222
974  n
mi
                                          Hp   =            216
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11942157
76                 X    =         3695823
18
 Y    =      -18294549
67  feet           Y    =        -5535161
74  meter
 Z    =        4208278
79                 Z    =         1300500
24
 XDOT =      11401
481736                 XDOT =        3406
309255
 YDOT =      11850
305869  feet/sec       YDOT =        3650
450106  meter/sec
 ZDOT =      19056
988037                 ZDOT =        5825
283227

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1091089
40                 X    =         -332564
05
 Y    =      -21804280
65  feet           Y    =        -6645944
74  meter
 Z    =        4289307
55                 Z    =         1307380
94
 XDOT =      14493
736796                 XDOT =        4417
690976
 YDOT =       3058
549064  feet/sec       YDOT =         932
245755  meter/sec
 ZDOT =      19131
952350                 ZDOT =        5831
419076


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   19036
78749627  
00016717  00000-0  10270-3 0  9129
2 25544  51
6371 294
6973 0005082 352
4869   7
6206 15
53212786 34836


Satellite: ISS
Catalog Number: 25544
Epoch time:      19036
78749627   =   yrday
fracday
Element set:     912
Inclination:       51
6371  deg
RA of node:       294
6973  deg
Eccentricity:     
0005082     
Arg of perigee:   352
4869  deg
Mean anomaly:       7
6206  deg
Mean motion:   15
53212786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3483
Checksum:              339


Coasting Arc #14 (Orbit 3497)
---------------------------------------

Vector Time (GMT): 2019/037/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3924711
10                 A    =         6788949
09  meter
 Y    =        4890225
67  meter          E    =           
0004449
 Z    =       -2609158
13                 I    =           51
28782
 XDOT =      -2692
567617                 Wp   =           59
44107
 YDOT =      -4934
499101  meter/sec      RA   =          289
26720  deg
 ZDOT =      -5202
759612                 TA   =          150
05382
                                          MA   =          150
02836
                                          Ha   =            223
156  n
mi
                                          Hp   =            215
811

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12876348
74                 X    =        -3966429
79
 Y    =       16044047
48  feet           Y    =         4846103
45  meter
 Z    =       -8560230
09                 Z    =        -2628323
89
 XDOT =      -8833
883259                 XDOT =       -2611
917114
 YDOT =     -16189
301511  feet/sec       YDOT =       -4964
158516  meter/sec
 ZDOT =     -17069
421299                 ZDOT =       -5215
642678

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -609732
05                 X    =         -185846
33
 Y    =       20526634
08  feet           Y    =         6256518
07  meter
 Z    =       -8647246
71                 Z    =        -2635680
80
 XDOT =     -15200
368646                 XDOT =       -4633
072363
 YDOT =      -7660
527105  feet/sec       YDOT =       -2334
928661  meter/sec
 ZDOT =     -17126
965741                 ZDOT =       -5220
299158


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   19037
75259094  
00016717  00000-0  10270-3 0  9132
2 25544  51
6379 289
8927 0005232 357
9598   2
1532 15
53247312 34986


Satellite: ISS
Catalog Number: 25544
Epoch time:      19037
75259094   =   yrday
fracday
Element set:     913
Inclination:       51
6379  deg
RA of node:       289
8927  deg
Eccentricity:     
0005232     
Arg of perigee:   357
9598  deg
Mean anomaly:       2
1532  deg
Mean motion:   15
53247312  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3498
Checksum:              342


Coasting Arc #15 (Orbit 3513)
---------------------------------------

Vector Time (GMT): 2019/038/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4080646
36                 A    =         6785943
27  meter
 Y    =       -3928509
51  meter          E    =           
0012178
 Z    =        3723508
55                 I    =           51
26639
 XDOT =       1969
453015                 Wp   =           72
05128
 YDOT =       6078
615214  meter/sec      RA   =          284
26658  deg
 ZDOT =       4247
137012                 TA   =          332
71191
                                          MA   =          332
77583
                                          Ha   =            223
048  n
mi
                                          Hp   =            215
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13387947
39                 X    =         4106186
50
 Y    =      -12888810
72  feet           Y    =        -3882733
88  meter
 Z    =       12216235
39                 Z    =         3743392
53
 XDOT =       6461
460023                 XDOT =        1880
704130
 YDOT =      19942
963302  feet/sec       YDOT =        6100
143000  meter/sec
 ZDOT =      13934
176550                 ZDOT =        4256
487785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2579679
64                 X    =          786286
35
 Y    =      -18343760
16  feet           Y    =        -5591178
10  meter
 Z    =       12306368
28                 Z    =         3750981
05
 XDOT =      15940
546871                 XDOT =        4858
678686
 YDOT =      11634
664433  feet/sec       YDOT =        3546
245719  meter/sec
 ZDOT =      13975
672933                 ZDOT =        4259
785110


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   19038
78202413  
00016717  00000-0  10270-3 0  9140
2 25544  51
6365 284
7672 0004990    
9249 359
1912 15
53240618 35148


Satellite: ISS
Catalog Number: 25544
Epoch time:      19038
78202413   =   yrday
fracday
Element set:     914
Inclination:       51
6365  deg
RA of node:       284
7672  deg
Eccentricity:     
0004990     
Arg of perigee:      
9249  deg
Mean anomaly:     359
1912  deg
Mean motion:   15
53240618  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3514
Checksum:              312


Coasting Arc #16 (Orbit 3528)
---------------------------------------

Vector Time (GMT): 2019/039/17:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4183159
99                 A    =         6782893
12  meter
 Y    =        2742469
45  meter          E    =           
0013267
 Z    =       -4594328
94                 I    =           51
24987
 XDOT =      -1283
959719                 Wp   =           49
87340
 YDOT =      -6938
497963  meter/sec      RA   =          279
25978  deg
 ZDOT =      -2970
026815                 TA   =          190
28258
                                          MA   =          190
30974
                                          Ha   =            223
310  n
mi
                                          Hp   =            215
506

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13724278
20                 X    =        -4191199
94
 Y    =        8997603
17  feet           Y    =         2695645
21  meter
 Z    =      -15073257
68                 Z    =        -4614668
41
 XDOT =      -4212
466271                 XDOT =       -1191
849621
 YDOT =     -22764
100929  feet/sec       YDOT =       -6952
341253  meter/sec
 ZDOT =      -9744
182464                 ZDOT =       -2976
039552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4954042
44                 X    =        -1509992
14
 Y    =       15555925
23  feet           Y    =         4741446
01  meter
 Z    =      -15165303
35                 Z    =        -4622384
46
 XDOT =     -16387
291033                 XDOT =       -4994
846307
 YDOT =     -14752
534116  feet/sec       YDOT =       -4496
572398  meter/sec
 ZDOT =      -9770
544271                 ZDOT =       -2978
061894


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   19039
74711811  
00016717  00000-0  10270-3 0  9155
2 25544  51
6374 279
9638 0005066   5
8606 354
2605 15
53238560 35296


Satellite: ISS
Catalog Number: 25544
Epoch time:      19039
74711811   =   yrday
fracday
Element set:     915
Inclination:       51
6374  deg
RA of node:       279
9638  deg
Eccentricity:     
0005066     
Arg of perigee:     5
8606  deg
Mean anomaly:     354
2605  deg
Mean motion:   15
53238560  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3529
Checksum:              325


Coasting Arc #17 (Orbit 3540)
---------------------------------------

Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916020
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3848227
16                 A    =         6780876
79  meter
 Y    =        2368977
60  meter          E    =           
0009772
 Z    =        5053735
33                 I    =           51
24363
 XDOT =      -2099
293688                 Wp   =           29
31900
 YDOT =       7164
983783  meter/sec      RA   =          275
48298  deg
 ZDOT =      -1750
287442                 TA   =           77
75451
                                          MA   =           77
64510
                                          Ha   =            223
241  n
mi
                                          Hp   =            215
574

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12625417
21                 X    =         3796902
80
 Y    =        7772236
21  feet           Y    =         2411724
50  meter
 Z    =       16580496
48                 Z    =         5072303
42
 XDOT =      -6887
446483                 XDOT =       -2170
756771
 YDOT =      23507
164641  feet/sec       YDOT =        7141
108333  meter/sec
 ZDOT =      -5742
412866                 ZDOT =       -1760
658839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1836319
51                 X    =          559710
19
 Y    =       14617141
68  feet           Y    =         4455304
78  meter
 Z    =       16663996
48                 Z    =         5079186
13
 XDOT =     -21511
215334                 XDOT =       -6556
618434
 YDOT =       9339
700476  feet/sec       YDOT =        2846
740705  meter/sec
 ZDOT =      -5789
965591                 ZDOT =       -1764
781512


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   19040
51918971  
00016717  00000-0  10270-3 0  9169
2 25544  51
6410 276
1246 0005494   4
3951 355
7248 15
53273072 35413


Satellite: ISS
Catalog Number: 25544
Epoch time:      19040
51918971   =   yrday
fracday
Element set:     916
Inclination:       51
6410  deg
RA of node:       276
1246  deg
Eccentricity:     
0005494     
Arg of perigee:     4
3951  deg
Mean anomaly:     355
7248  deg
Mean motion:   15
53273072  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3541
Checksum:              306
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