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

 
Date: March 29th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


090/15:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 2

092/20:30:41 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 215 2

094/03:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 2

094/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 1

Coasting Arc #1 (Orbit 2598)
---------------------------------------

Vector Time (GMT): 2018/087/16:39:03
372
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4021984
84                 A    =         6788902
97  meter
 Y    =        5388660
00  meter          E    =           
0009260
 Z    =        -899525
47                 I    =           51
98755
 XDOT =      -3344
173028                 Wp   =           29
63370
 YDOT =       3484
566526  meter/sec      RA   =           59
26513  deg
 ZDOT =       5955
844006                 TA   =          320
67770
                                          MA   =          320
74490
                                          Ha   =            220
327  n
mi
                                          Hp   =            215
272

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13195488
31                 X    =         3965797
83
 Y    =       17679330
70  feet           Y    =         5433322
33  meter
 Z    =       -2951199
06                 Z    =         -880125
33
 XDOT =     -10971
696285                 XDOT =       -3411
819949
 YDOT =      11432
304875  feet/sec       YDOT =        3446
792133  meter/sec
 ZDOT =      19540
170624                 ZDOT =        5939
434617

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20505711
51                 X    =         6250140
87
 Y    =       -8166683
93  feet           Y    =        -2489205
26  meter
 Z    =       -2865360
43                 Z    =         -873361
86
 XDOT =       7560
958704                 XDOT =        2304
580213
 YDOT =      12195
023776  feet/sec       YDOT =        3717
043247  meter/sec
 ZDOT =      19466
401938                 ZDOT =        5933
359311


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   18087
69548005  
00016717  00000-0  10270-3 0  9008
2 25544  51
6413  59
9899 0001781 276
9125  83
1825 15
54162944 25993


Satellite: ISS
Catalog Number: 25544
Epoch time:      18087
69548005   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:        59
9899  deg
Eccentricity:     
0001781     
Arg of perigee:   276
9125  deg
Mean anomaly:      83
1825  deg
Mean motion:   15
54162944  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2599
Checksum:              345


Coasting Arc #2 (Orbit 2614)
---------------------------------------

Vector Time (GMT): 2018/088/16:39:03
372
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3369281
26                 A    =         6788987
40  meter
 Y    =       -5827410
55  meter          E    =           
0008922
 Z    =        -846659
09                 I    =           51
97001
 XDOT =       4494
963619                 Wp   =          148
83414
 YDOT =      -1737
533409  meter/sec      RA   =           54
31882  deg
 ZDOT =      -5963
985314                 TA   =           40
28180
                                          MA   =           40
21574
                                          Ha   =            220
315  n
mi
                                          Hp   =            215
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11054072
39                 X    =        -3299754
56
 Y    =      -19118801
03  feet           Y    =        -5864699
54  meter
 Z    =       -2777752
93                 Z    =         -862856
16
 XDOT =      14747
255969                 XDOT =        4543
028848
 YDOT =      -5700
568928  feet/sec       YDOT =       -1686
999668  meter/sec
 ZDOT =     -19566
880952                 ZDOT =       -5942
033501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21228877
10                 X    =        -6470561
74
 Y    =        6054231
59  feet           Y    =         1845329
79  meter
 Z    =       -2849217
00                 Z    =         -868441
34
 XDOT =      -1471
377364                 XDOT =        -448
475821
 YDOT =     -14268
243013  feet/sec       YDOT =       -4348
960470  meter/sec
 ZDOT =     -19468
621473                 ZDOT =       -5934
035825


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   18088
72429219  
00016717  00000-0  10270-3 0  9019
2 25544  51
6414  54
8616 0001819 275
3452  84
7493 15
54135462 26155


Satellite: ISS
Catalog Number: 25544
Epoch time:      18088
72429219   =   yrday
fracday
Element set:     901
Inclination:       51
6414  deg
RA of node:        54
8616  deg
Eccentricity:     
0001819     
Arg of perigee:   275
3452  deg
Mean anomaly:      84
7493  deg
Mean motion:   15
54135462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2615
Checksum:              318


Coasting Arc #3 (Orbit 2630)
---------------------------------------

Vector Time (GMT): 2018/089/16:39:03
372
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2439482
53                 A    =         6786605
28  meter
 Y    =        5821233
36  meter          E    =           
0012132
 Z    =        2477497
77                 I    =           51
94302
 XDOT =      -5498
931893                 Wp   =           70
32780
 YDOT =         21
040621  meter/sec      RA   =           49
36638  deg
 ZDOT =       5347
866975                 TA   =          317
32022
                                          MA   =          317
41440
                                          Ha   =            220
293  n
mi
                                          Hp   =            215
270

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8003551
60                 X    =         2362172
24
 Y    =       19098534
65  feet           Y    =         5848081
42  meter
 Z    =        8128273
54                 Z    =         2489159
32
 XDOT =     -18041
115133                 XDOT =       -5524
735564
 YDOT =         69
030910  feet/sec       YDOT =         -40
595746  meter/sec
 ZDOT =      17545
495325                 ZDOT =        5321
092442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20403363
48                 X    =         6218945
19
 Y    =       -3417395
08  feet           Y    =        -1041622
02  meter
 Z    =        8179478
25                 Z    =         2493104
97
 XDOT =      -4292
894075                 XDOT =       -1308
474114
 YDOT =      16212
880790  feet/sec       YDOT =        4941
686065  meter/sec
 ZDOT =      17425
961847                 ZDOT =        5311
433171


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   18089
75309951  
00016717  00000-0  10270-3 0  9024
2 25544  51
6421  49
7321 0001889 286
7046  73
3900 15
54159720 26319


Satellite: ISS
Catalog Number: 25544
Epoch time:      18089
75309951   =   yrday
fracday
Element set:     902
Inclination:       51
6421  deg
RA of node:        49
7321  deg
Eccentricity:     
0001889     
Arg of perigee:   286
7046  deg
Mean anomaly:      73
3900  deg
Mean motion:   15
54159720  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2631
Checksum:              317


Coasting Arc #4 (Orbit 2644)
---------------------------------------

Vector Time (GMT): 2018/090/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3415825
11                 A    =         6787591
15  meter
 Y    =       -5530502
61  meter          E    =           
0005383
 Z    =       -1945710
35                 I    =           51
92579
 XDOT =       5080
739827                 Wp   =          150
45395
 YDOT =      -1164
436509  meter/sec      RA   =           44
73797  deg
 ZDOT =      -5620
940474                 TA   =           50
90843
                                          MA   =           50
86057
                                          Ha   =            220
307  n
mi
                                          Hp   =            215
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11206775
28                 X    =        -3344276
39
 Y    =      -18144693
61  feet           Y    =        -5568300
94  meter
 Z    =       -6383564
14                 Z    =        -1962128
73
 XDOT =      16669
093920                 XDOT =        5120
686904
 YDOT =      -3820
329754  feet/sec       YDOT =       -1107
397610  meter/sec
 ZDOT =     -18441
405753                 ZDOT =       -5596
162752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21212486
52                 X    =        -6465565
89
 Y    =       -1980312
81  feet           Y    =         -603599
34  meter
 Z    =       -6456034
87                 Z    =        -1967799
43
 XDOT =       6890
811242                 XDOT =        2100
319267
 YDOT =     -14170
444169  feet/sec       YDOT =       -4319
151383  meter/sec
 ZDOT =     -18330
624046                 ZDOT =       -5587
174209


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   18090
65330256  
00016717  00000-0  10270-3 0  9038
2 25544  51
6422  45
2440 0001837 287
8142  72
2810 15
54160577 26450


Satellite: ISS
Catalog Number: 25544
Epoch time:      18090
65330256   =   yrday
fracday
Element set:     903
Inclination:       51
6422  deg
RA of node:        45
2440  deg
Eccentricity:     
0001837     
Arg of perigee:   287
8142  deg
Mean anomaly:      72
2810  deg
Mean motion:   15
54160577  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2645
Checksum:              292


Coasting Arc #5 (Orbit 2660)
---------------------------------------

Vector Time (GMT): 2018/091/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2274172
79                 A    =         6784183
98  meter
 Y    =        5389711
95  meter          E    =           
0010769
 Z    =        3425731
06                 I    =           51
89006
 XDOT =      -6109
964408                 Wp   =           86
14479
 YDOT =       -368
016226  meter/sec      RA   =           39
77829  deg
 ZDOT =       4623
315537                 TA   =          313
81457
                                          MA   =          313
90357
                                          Ha   =            220
351  n
mi
                                          Hp   =            215
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7461196
82                 X    =         2197094
04
 Y    =       17682782
00  feet           Y    =         5414712
79  meter
 Z    =       11239275
12                 Z    =         3436590
36
 XDOT =     -20045
814986                 XDOT =       -6127
852825
 YDOT =      -1207
402317  feet/sec       YDOT =        -436
441472  meter/sec
 ZDOT =      15168
358062                 ZDOT =        4593
591858

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18652006
64                 X    =         5685131
62
 Y    =        4402183
65  feet           Y    =         1341785
58  meter
 Z    =       11286938
01                 Z    =         3440258
71
 XDOT =     -12482
774470                 XDOT =       -3804
749658
 YDOT =      14239
916327  feet/sec       YDOT =        4340
326496  meter/sec
 ZDOT =      15035
735267                 ZDOT =        4582
892109


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   18091
68210282  
00016717  00000-0  10270-3 0  9049
2 25544  51
6418  40
1153 0001781 295
8940  64
2029 15
54171538 26613


Satellite: ISS
Catalog Number: 25544
Epoch time:      18091
68210282   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:        40
1153  deg
Eccentricity:     
0001781     
Arg of perigee:   295
8940  deg
Mean anomaly:      64
2029  deg
Mean motion:   15
54171538  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2661
Checksum:              296


Coasting Arc #6 (Orbit 2675)
---------------------------------------

Vector Time (GMT): 2018/092/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -839772
96                 A    =         6780262
27  meter
 Y    =       -4950639
02  meter          E    =           
0008756
 Z    =       -4564913
51                 I    =           51
85223
 XDOT =       6779
434641                 Wp   =           59
87902
 YDOT =       1727
601278  meter/sec      RA   =           34
80725  deg
 ZDOT =      -3120
929691                 TA   =          178
92102
                                          MA   =          178
91913
                                          Ha   =            220
267  n
mi
                                          Hp   =            215
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2755160
64                 X    =         -762177
01
 Y    =      -16242254
02  feet           Y    =        -4959596
59  meter
 Z    =      -14976750
35                 Z    =        -4568803
85
 XDOT =      22242
239637                 XDOT =        6774
772244
 YDOT =       5667
983196  feet/sec       YDOT =        1803
387164  meter/sec
 ZDOT =     -10239
270639                 ZDOT =       -3088
008768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14833668
07                 X    =        -4521302
03
 Y    =       -7132052
82  feet           Y    =        -2173849
70  meter
 Z    =      -14993361
56                 Z    =        -4569976
60
 XDOT =      16909
272452                 XDOT =        5153
946243
 YDOT =     -13953
045999  feet/sec       YDOT =       -4252
888421  meter/sec
 ZDOT =     -10092
593809                 ZDOT =       -3076
222593


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   18092
64659789  
00016717  00000-0  10270-3 0  9056
2 25544  51
6427  35
3080 0001975 297
1274  62
9678 15
54206001 26763


Satellite: ISS
Catalog Number: 25544
Epoch time:      18092
64659789   =   yrday
fracday
Element set:     905
Inclination:       51
6427  deg
RA of node:        35
3080  deg
Eccentricity:     
0001975     
Arg of perigee:   297
1274  deg
Mean anomaly:      62
9678  deg
Mean motion:   15
54206001  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2676
Checksum:              333


Coasting Arc #7 (Orbit 2679)
---------------------------------------

Vector Time (GMT): 2018/092/20:30:41
000
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1767678
73                 A    =         6777386
64  meter
 Y    =        3830856
03  meter          E    =           
0001075
 Z    =        5303211
54                 I    =           51
83129
 XDOT =      -6607
614216                 Wp   =          111
89411
 YDOT =      -3850
846546  meter/sec      RA   =           33
64343  deg
 ZDOT =        578
767597                 TA   =          332
59515
                                          MA   =          332
60082
                                          Ha   =            220
476  n
mi
                                          Hp   =            215
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5799470
89                 X    =        -1836145
48
 Y    =       12568425
30  feet           Y    =         3810706
38  meter
 Z    =       17398988
01                 Z    =         5294457
99
 XDOT =     -21678
524331                 XDOT =       -6566
873285
 YDOT =     -12634
010978  feet/sec       YDOT =       -3924
509578  meter/sec
 ZDOT =       1898
843822                 ZDOT =         546
769162

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12812363
04                 X    =         3905208
25
 Y    =       -5368505
30  feet           Y    =        -1636320
42  meter
 Z    =       17359333
66                 Z    =         5291124
90
 XDOT =       7245
602488                 XDOT =        2208
459638
 YDOT =      22977
453457  feet/sec       YDOT =        7003
527814  meter/sec
 ZDOT =       1756
611178                 ZDOT =         535
415087


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   18092
90379727  
00016717  00000-0  10270-3 0  9067
2 25544  51
6383  34
0210 0001729 292
5230  67
5739 15
54147523 26800


Satellite: ISS
Catalog Number: 25544
Epoch time:      18092
90379727   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:        34
0210  deg
Eccentricity:     
0001729     
Arg of perigee:   292
5230  deg
Mean anomaly:      67
5739  deg
Mean motion:   15
54147523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2680
Checksum:              311


Coasting Arc #8 (Orbit 2694)
---------------------------------------

Vector Time (GMT): 2018/093/20:30:41
000
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3324314
64                 A    =         6777808
32  meter
 Y    =       -2837565
10  meter          E    =           
0012305
 Z    =       -5191203
09                 I    =           51
80621
 XDOT =       6020
802057                 Wp   =           98
58877
 YDOT =       4528
549983  meter/sec      RA   =           28
65541  deg
 ZDOT =       1381
221048                 TA   =          184
67026
                                          MA   =          184
68175
                                          Ha   =            220
381  n
mi
                                          Hp   =            215
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10906544
11                 X    =         3381014
38
 Y    =       -9309596
79  feet           Y    =        -2800073
74  meter
 Z    =      -17031506
19                 Z    =        -5174916
60
 XDOT =      19753
287588                 XDOT =        5963
005787
 YDOT =      14857
447450  feet/sec       YDOT =        4595
555694  meter/sec
 ZDOT =       4531
565119                 ZDOT =        1410
327546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14424188
50                 X    =        -4396492
65
 Y    =        -222732
82  feet           Y    =          -67888
96  meter
 Z    =      -16958380
70                 Z    =        -5168914
44
 XDOT =      -5118
903640                 XDOT =       -1560
241829
 YDOT =     -23108
288613  feet/sec       YDOT =       -7043
406369  meter/sec
 ZDOT =       4660
770907                 ZDOT =        1420
602972


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   18093
86828641  
00016717  00000-0  10270-3 0  9078
2 25544  51
6394  29
2126 0001577 295
0624  65
0365 15
54202488 26956


Satellite: ISS
Catalog Number: 25544
Epoch time:      18093
86828641   =   yrday
fracday
Element set:     907
Inclination:       51
6394  deg
RA of node:        29
2126  deg
Eccentricity:     
0001577     
Arg of perigee:   295
0624  deg
Mean anomaly:      65
0365  deg
Mean motion:   15
54202488  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2695
Checksum:              328


Coasting Arc #9 (Orbit 2699)
---------------------------------------

Vector Time (GMT): 2018/094/03:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 906820
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1327820
98                 A    =         6777176
17  meter
 Y    =        4008104
80  meter          E    =           
0000899
 Z    =        5300424
86                 I    =           51
79867
 XDOT =      -6996
322827                 Wp   =          107
46029
 YDOT =      -3088
251700  meter/sec      RA   =           27
25231  deg
 ZDOT =        582
282822                 TA   =          336
99375
                                          MA   =          336
99778
                                          Ha   =            220
308  n
mi
                                          Hp   =            215
158

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4356368
06                 X    =        -1398288
95
 Y    =       13149950
13  feet           Y    =         3992862
60  meter
 Z    =       17389845
34                 Z    =         5293803
23
 XDOT =     -22953
815048                 XDOT =       -6964
097625
 YDOT =     -10132
059384  feet/sec       YDOT =       -3166
309168  meter/sec
 ZDOT =       1910
376711                 ZDOT =         548
375290

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9539916
08                 X    =        -2907766
42
 Y    =      -10096415
84  feet           Y    =        -3077387
55  meter
 Z    =       17359672
82                 Z    =         5291228
27
 XDOT =      18949
928452                 XDOT =        5775
938192
 YDOT =     -14878
180036  feet/sec       YDOT =       -4534
869275  meter/sec
 ZDOT =       1759
525167                 ZDOT =         536
303271


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   18094
18978014  
00016717  00000-0  10270-3 0  9085
2 25544  51
6419  27
6126 0001910 294
6552  65
4402 15
54219530 27001


Satellite: ISS
Catalog Number: 25544
Epoch time:      18094
18978014   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:        27
6126  deg
Eccentricity:     
0001910     
Arg of perigee:   294
6552  deg
Mean anomaly:      65
4402  deg
Mean motion:   15
54219530  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2700
Checksum:              300


Coasting Arc #10 (Orbit 2704)
---------------------------------------

Vector Time (GMT): 2018/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1131190
19                 A    =         6779390
97  meter
 Y    =        4695900
88  meter          E    =           
0005627
 Z    =        4753717
67                 I    =           51
79554
 XDOT =      -7097
741636                 Wp   =          116
07709
 YDOT =      -1043
302983  meter/sec      RA   =           25
68897  deg
 ZDOT =       2714
681616                 TA   =          307
12904
                                          MA   =          307
18043
                                          Ha   =            220
263  n
mi
                                          Hp   =            215
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3711253
91                 X    =         1055503
99
 Y    =       15406498
96  feet           Y    =         4708127
79  meter
 Z    =       15596186
57                 Z    =         4759028
47
 XDOT =     -23286
553923                 XDOT =       -7098
734240
 YDOT =      -3422
910048  feet/sec       YDOT =       -1122
680164  meter/sec
 ZDOT =       8906
435749                 ZDOT =        2680
200581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2753769
93                 X    =          839349
08
 Y    =       15583108
23  feet           Y    =         4749731
39  meter
 Z    =       15619159
40                 Z    =         4760719
79
 XDOT =     -21984
515744                 XDOT =       -6700
880399
 YDOT =      -4904
068859  feet/sec       YDOT =       -1494
760188  meter/sec
 ZDOT =       8752
711333                 ZDOT =        2667
826414


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   18094
51127597  
00016717  00000-0  10270-3 0  9095
2 25544  51
6404  26
0109 0001970 302
9919  57
1044 15
54236915 27056


Satellite: ISS
Catalog Number: 25544
Epoch time:      18094
51127597   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:        26
0109  deg
Eccentricity:     
0001970     
Arg of perigee:   302
9919  deg
Mean anomaly:      57
1044  deg
Mean motion:   15
54236915  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2705
Checksum:              305


Coasting Arc #11 (Orbit 2719)
---------------------------------------

Vector Time (GMT): 2018/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         594638
71                 A    =         6777328
62  meter
 Y    =       -4222840
98  meter          E    =           
0013262
 Z    =       -5278989
03                 I    =           51
75805
 XDOT =       7327
073442                 Wp   =           77
52225
 YDOT =       2069
923060  meter/sec      RA   =           20
70028  deg
 ZDOT =       -829
424672                 TA   =          184
54622
                                          MA   =          184
55827
                                          Ha   =            220
387  n
mi
                                          Hp   =            215
105

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1950914
40                 X    =          667458
23
 Y    =      -13854465
15  feet           Y    =        -4215784
47  meter
 Z    =      -17319517
82                 Z    =        -5275923
34
 XDOT =      24038
954861                 XDOT =        7307
411376
 YDOT =       6791
086156  feet/sec       YDOT =        2151
749451  meter/sec
 ZDOT =      -2721
209554                 ZDOT =        -793
879876

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2589101
01                 X    =          789157
99
 Y    =      -13767549
93  feet           Y    =        -4196349
22  meter
 Z    =      -17305175
35                 Z    =        -5274617
45
 XDOT =      22777
695358                 XDOT =        6942
641545
 YDOT =       7509
267089  feet/sec       YDOT =        2288
824609  meter/sec
 ZDOT =      -2562
907851                 ZDOT =        -781
174313


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   18095
47576075  
00016717  00000-0  10270-3 0  9102
2 25544  51
6403  21
2024 0001947 309
2877  50
8103 15
54207623 27202


Satellite: ISS
Catalog Number: 25544
Epoch time:      18095
47576075   =   yrday
fracday
Element set:     910
Inclination:       51
6403  deg
RA of node:        21
2024  deg
Eccentricity:     
0001947     
Arg of perigee:   309
2877  deg
Mean anomaly:      50
8103  deg
Mean motion:   15
54207623  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2720
Checksum:              288


Coasting Arc #12 (Orbit 2735)
---------------------------------------

Vector Time (GMT): 2018/096/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2358401
39                 A    =         6777537
80  meter
 Y    =        3617227
14  meter          E    =           
0004070
 Z    =        5222927
00                 I    =           51
72831
 XDOT =      -7004
100370                 Wp   =           25
93582
 YDOT =      -2907
990648  meter/sec      RA   =           15
70761  deg
 ZDOT =      -1144
794706                 TA   =           75
04665
                                          MA   =           75
00158
                                          Ha   =            220
467  n
mi
                                          Hp   =            215
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7737537
36                 X    =        -2424045
31
 Y    =       11867543
10  feet           Y    =         3590487
10  meter
 Z    =       17135587
27                 Z    =         5211311
01
 XDOT =     -22979
331921                 XDOT =       -6965
501024
 YDOT =      -9540
651731  feet/sec       YDOT =       -2986
099553  meter/sec
 ZDOT =      -3755
888142                 ZDOT =       -1178
724505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8094775
30                 X    =        -2467287
51
 Y    =       11703672
73  feet           Y    =         3567279
45  meter
 Z    =       17083180
98                 Z    =         5206953
56
 XDOT =     -21897
971559                 XDOT =       -6674
501731
 YDOT =      -9424
211636  feet/sec       YDOT =       -2872
499707  meter/sec
 ZDOT =      -3906
841249                 ZDOT =       -1190
805213


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   18096
50453668  
00016717  00000-0  10270-3 0  9110
2 25544  51
6409  16
0741 0002065 313
0031  47
0948 15
54224668 27363


Satellite: ISS
Catalog Number: 25544
Epoch time:      18096
50453668   =   yrday
fracday
Element set:     911
Inclination:       51
6409  deg
RA of node:        16
0741  deg
Eccentricity:     
0002065     
Arg of perigee:   313
0031  deg
Mean anomaly:      47
0948  deg
Mean motion:   15
54224668  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2736
Checksum:              297


Coasting Arc #13 (Orbit 2750)
---------------------------------------

Vector Time (GMT): 2018/097/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3992781
35                 A    =         6780095
00  meter
 Y    =       -2957905
93  meter          E    =           
0008422
 Z    =       -4620854
17                 I    =           51
70479
 XDOT =       6091
729136                 Wp   =          102
92818
 YDOT =       3555
838072  meter/sec      RA   =           10
71530  deg
 ZDOT =       2990
319757                 TA   =          196
88109
                                          MA   =          196
90913
                                          Ha   =            220
479  n
mi
                                          Hp   =            215
078

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13099676
36                 X    =         4048006
47
 Y    =       -9704415
77  feet           Y    =        -2912947
34  meter
 Z    =      -15160282
73                 Z    =        -4601324
28
 XDOT =      19985
987980                 XDOT =        6036
988583
 YDOT =      11666
135406  feet/sec       YDOT =        3623
654050  meter/sec
 ZDOT =       9810
760356                 ZDOT =        3019
778250

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13233594
32                 X    =         4033599
55
 Y    =       -9659092
83  feet           Y    =        -2944091
49  meter
 Z    =      -15072666
84                 Z    =        -4594148
85
 XDOT =      19175
226018                 XDOT =        5844
608890
 YDOT =      10771
916580  feet/sec       YDOT =        3283
280173  meter/sec
 ZDOT =       9941
649767                 ZDOT =        3030
214849


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   18097
46900864  
00016717  00000-0  10270-3 0  9122
2 25544  51
6408  11
2651 0002012 319
1609  40
9392 15
54230198 27516


Satellite: ISS
Catalog Number: 25544
Epoch time:      18097
46900864   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:        11
2651  deg
Eccentricity:     
0002012     
Arg of perigee:   319
1609  deg
Mean anomaly:      40
9392  deg
Mean motion:   15
54230198  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2751
Checksum:              292


Coasting Arc #14 (Orbit 2766)
---------------------------------------

Vector Time (GMT): 2018/098/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5358253
57                 A    =         6783937
99  meter
 Y    =        2240360
23  meter          E    =           
0011178
 Z    =        3498306
32                 I    =           51
68515
 XDOT =      -4666
560270                 Wp   =           80
21705
 YDOT =      -4065
648867  meter/sec      RA   =            5
73146  deg
 ZDOT =      -4529
756969                 TA   =           58
66470
                                          MA   =           58
55534
                                          Ha   =            220
553  n
mi
                                          Hp   =            214
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17579572
08                 X    =        -5399900
61
 Y    =        7350263
23  feet           Y    =         2180207
87  meter
 Z    =       11477382
95                 Z    =         3472176
47
 XDOT =     -15310
237105                 XDOT =       -4598
747035
 YDOT =     -13338
743003  feet/sec       YDOT =       -4117
454619  meter/sec
 ZDOT =     -14861
407379                 ZDOT =       -4552
260629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17552761
43                 X    =        -5350081
68
 Y    =        7592043
57  feet           Y    =         2314054
88  meter
 Z    =       11360435
03                 Z    =         3462660
60
 XDOT =     -14839
226107                 XDOT =       -4522
996118
 YDOT =     -11850
544481  feet/sec       YDOT =       -3612
045958  meter/sec
 ZDOT =     -14961
175724                 ZDOT =       -4560
166361


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   18098
49777408  
00016717  00000-0  10270-3 0  9133
2 25544  51
6409   6
1368 0002052 321
7087  38
3919 15
54233911 27677


Satellite: ISS
Catalog Number: 25544
Epoch time:      18098
49777408   =   yrday
fracday
Element set:     913
Inclination:       51
6409  deg
RA of node:         6
1368  deg
Eccentricity:     
0002052     
Arg of perigee:   321
7087  deg
Mean anomaly:      38
3919  deg
Mean motion:   15
54233911  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2767
Checksum:              324


Coasting Arc #15 (Orbit 2781)
---------------------------------------

Vector Time (GMT): 2018/099/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6296300
63                 A    =         6787335
89  meter
 Y    =       -1514752
32  meter          E    =           
0007585
 Z    =       -2020277
85                 I    =           51
66427
 XDOT =       2849
001759                 Wp   =           23
72201
 YDOT =       4438
633961  meter/sec      RA   =             
75481  deg
 ZDOT =       5565
136525                 TA   =          313
96461
                                          MA   =          314
02715
                                          Ha   =            220
539  n
mi
                                          Hp   =            214
970

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20657154
29                 X    =         6322584
50
 Y    =       -4969659
83  feet           Y    =        -1444195
90  meter
 Z    =       -6628208
19                 Z    =        -1989628
67
 XDOT =       9347
118632                 XDOT =        2772
123490
 YDOT =      14562
447377  feet/sec       YDOT =        4470
063927  meter/sec
 ZDOT =      18258
321933                 ZDOT =        5578
789013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20537131
23                 X    =         6259717
60
 Y    =       -5607051
11  feet           Y    =        -1709029
18  meter
 Z    =       -6491217
50                 Z    =        -1978523
09
 XDOT =       9262
779245                 XDOT =        2823
295114
 YDOT =      12774
419266  feet/sec       YDOT =        3893
642992  meter/sec
 ZDOT =      18318
533945                 ZDOT =        5583
489146


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   18099
46223655  
00016717  00000-0  10270-3 0  9142
2 25544  51
6413   1
3280 0002109 323
4801  36
6208 15
54241865 27824


Satellite: ISS
Catalog Number: 25544
Epoch time:      18099
46223655   =   yrday
fracday
Element set:     914
Inclination:       51
6413  deg
RA of node:         1
3280  deg
Eccentricity:     
0002109     
Arg of perigee:   323
4801  deg
Mean anomaly:      36
6208  deg
Mean motion:   15
54241865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2782
Checksum:              290


Coasting Arc #16 (Orbit 2797)
---------------------------------------

Vector Time (GMT): 2018/100/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6738767
85                 A    =         6788987
46  meter
 Y    =         727761
97  meter          E    =           
0010596
 Z    =         291052
14                 I    =           51
63783
 XDOT =       -773
764518                 Wp   =          128
56122
 YDOT =      -4707
408472  meter/sec      RA   =          355
78393  deg
 ZDOT =      -6003
109304                 TA   =           48
30233
                                          MA   =           48
21171
                                          Ha   =            220
549  n
mi
                                          Hp   =            214
901

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22108818
41                 X    =        -6747818
82
 Y    =        2387670
51  feet           Y    =          652353
84  meter
 Z    =         954895
48                 Z    =          258295
52
 XDOT =      -2538
597501                 XDOT =        -691
907552
 YDOT =     -15444
253517  feet/sec       YDOT =       -4715
603959  meter/sec
 ZDOT =     -19695
240498                 ZDOT =       -6006
668844

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21974301
45                 X    =        -6697767
08
 Y    =        3448018
47  feet           Y    =         1050956
03  meter
 Z    =         808635
89                 Z    =          246472
22
 XDOT =      -2896
690989                 XDOT =        -882
911413
 YDOT =     -13709
768622  feet/sec       YDOT =       -4178
737476  meter/sec
 ZDOT =     -19710
378260                 ZDOT =       -6007
723294


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   18100
49099052  
00016717  00000-0  10270-3 0  9151
2 25544  51
6423 356
1989 0002057 328
4081  31
6948 15
54236976 27989


Satellite: ISS
Catalog Number: 25544
Epoch time:      18100
49099052   =   yrday
fracday
Element set:     915
Inclination:       51
6423  deg
RA of node:       356
1989  deg
Eccentricity:     
0002057     
Arg of perigee:   328
4081  deg
Mean anomaly:      31
6948  deg
Mean motion:   15
54236976  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2798
Checksum:              334


Coasting Arc #17 (Orbit 2813)
---------------------------------------

Vector Time (GMT): 2018/101/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6625001
53                 A    =         6788057
06  meter
 Y    =          84871
70  meter          E    =           
0014153
 Z    =        1440495
44                 I    =           51
60182
 XDOT =      -1326
907197                 Wp   =           52
23532
 YDOT =       4859
777448  meter/sec      RA   =          350
81181  deg
 ZDOT =       5785
896052                 TA   =          323
49347
                                          MA   =          323
58987
                                          Ha   =            220
588  n
mi
                                          Hp   =            214
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21735569
32                 X    =         6616562
92
 Y    =         278450
47  feet           Y    =          158909
96  meter
 Z    =        4726034
90                 Z    =         1472656
90
 XDOT =      -4353
370068                 XDOT =       -1409
256775
 YDOT =      15944
151733  feet/sec       YDOT =        4844
479084  meter/sec
 ZDOT =      18982
598596                 ZDOT =        5779
249989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21675821
91                 X    =         6606790
52
 Y    =       -1137814
20  feet           Y    =         -346805
77  meter
 Z    =        4869500
74                 Z    =         1484223
82
 XDOT =      -3511
749446                 XDOT =       -1070
381231
 YDOT =      14623
231943  feet/sec       YDOT =        4457
161096  meter/sec
 ZDOT =      18952
185167                 ZDOT =        5776
626039


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   18101
51973968  
00016717  00000-0  10270-3 0  9163
2 25544  51
6419 351
0699 0002191 334
5421  25
5624 15
54246313 28149


Satellite: ISS
Catalog Number: 25544
Epoch time:      18101
51973968   =   yrday
fracday
Element set:     916
Inclination:       51
6419  deg
RA of node:       351
0699  deg
Eccentricity:     
0002191     
Arg of perigee:   334
5421  deg
Mean anomaly:      25
5624  deg
Mean motion:   15
54246313  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2814
Checksum:              306


Coasting Arc #18 (Orbit 2828)
---------------------------------------

Vector Time (GMT): 2018/102/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928606
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5986353
60                 A    =         6784931
09  meter
 Y    =        -980033
66  meter          E    =           
0003325
 Z    =       -3043145
09                 I    =           51
55996
 XDOT =       3295
894926                 Wp   =           78
06182
 YDOT =      -4861
210349  meter/sec      RA   =          345
83248  deg
 ZDOT =      -4921
904357                 TA   =          136
86208
                                          MA   =          136
83603
                                          Ha   =            220
547  n
mi
                                          Hp   =            214
757

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19640267
70                 X    =        -5960167
65
 Y    =       -3215333
53  feet           Y    =        -1046831
05  meter
 Z    =       -9984071
81                 Z    =        -3072161
08
 XDOT =      10813
303562                 XDOT =        3373
917414
 YDOT =     -15948
852851  feet/sec       YDOT =       -4823
917589  meter/sec
 ZDOT =     -16147
980174                 ZDOT =       -4905
704057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19772323
36                 X    =        -6026604
16
 Y    =       -1592311
86  feet           Y    =         -485336
66  meter
 Z    =      -10113354
88                 Z    =        -3082550
57
 XDOT =       9452
226112                 XDOT =        2881
038519
 YDOT =     -15353
818102  feet/sec       YDOT =       -4679
843758  meter/sec
 ZDOT =     -16074
952829                 ZDOT =       -4899
645622


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   18102
48418724  
00016717  00000-0  10270-3 0  9175
2 25544  51
6426 346
2622 0002211 331
1182  28
9848 15
54255584 28290


Satellite: ISS
Catalog Number: 25544
Epoch time:      18102
48418724   =   yrday
fracday
Element set:     917
Inclination:       51
6426  deg
RA of node:       346
2622  deg
Eccentricity:     
0002211     
Arg of perigee:   331
1182  deg
Mean anomaly:      28
9848  deg
Mean motion:   15
54255584  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2829
Checksum:              309
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