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

 
Date: April 10th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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


101/03:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 214 7

105/08:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 214 6

108/10:36:00 987 0 3 0 8 0 8
N/A -0 7 -0 0 220 9
000/00:02:01 974 -0 4 -0 0 214 8

Coasting Arc #1 (Orbit 2782)
---------------------------------------

Vector Time (GMT): 2018/099/12:03:23
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4867084
31                 A    =         6783191
69  meter
 Y    =       -2964863
85  meter          E    =           
0005258
 Z    =       -3685123
17                 I    =           51
65080
 XDOT =       5338
668199                 Wp   =           55
64099
 YDOT =      -3376
524123  meter/sec      RA   =             
57961  deg
 ZDOT =      -4335
925158                 TA   =          168
17766
                                          MA   =          168
16531
                                          Ha   =            220
511  n
mi
                                          Hp   =            214
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15968124
39                 X    =        -4815668
27
 Y    =       -9727243
60  feet           Y    =        -3019003
66  meter
 Z    =      -12090299
13                 Z    =        -3708640
74
 XDOT =      17515
315612                 XDOT =        5397
090279
 YDOT =     -11077
835049  feet/sec       YDOT =       -3316
497055  meter/sec
 ZDOT =     -14225
476240                 ZDOT =       -4309
849658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18090300
71                 X    =        -5513923
66
 Y    =       -4450217
35  feet           Y    =        -1356426
25  meter
 Z    =      -12194760
48                 Z    =        -3716962
99
 XDOT =      13093
867624                 XDOT =        3991
010852
 YDOT =     -14579
367606  feet/sec       YDOT =       -4443
791246  meter/sec
 ZDOT =     -14108
597956                 ZDOT =       -4300
300657


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
52661025  
00016717  00000-0  10270-3 0  9001
2 25544  51
6430   1
0083 0002203 324
9441  35
1566 15
54226406 27838


Satellite: ISS
Catalog Number: 25544
Epoch time:      18099
52661025   =   yrday
fracday
Element set:     900
Inclination:       51
6430  deg
RA of node:         1
0083  deg
Eccentricity:     
0002203     
Arg of perigee:   324
9441  deg
Mean anomaly:      35
1566  deg
Mean motion:   15
54226406  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2783
Checksum:              273


Coasting Arc #2 (Orbit 2798)
---------------------------------------

Vector Time (GMT): 2018/100/12:03:23
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3388321
38                 A    =         6779508
00  meter
 Y    =        3488995
99  meter          E    =           
0006069
 Z    =        4718786
83                 I    =           51
60573
 XDOT =      -6628
867395                 Wp   =          105
44335
 YDOT =       2702
651261  meter/sec      RA   =          355
58833  deg
 ZDOT =       2757
018754                 TA   =          317
23886
                                          MA   =          317
28606
                                          Ha   =            220
551  n
mi
                                          Hp   =            214
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11116539
96                 X    =         3326133
27
 Y    =       11446837
24  feet           Y    =         3526539
14  meter
 Z    =       15481584
09                 Z    =         4735094
83
 XDOT =     -21748
252607                 XDOT =       -6671
988649
 YDOT =       8866
966080  feet/sec       YDOT =        2628
281788  meter/sec
 ZDOT =       9045
337120                 ZDOT =        2724
713105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14095896
69                 X    =         4296429
31
 Y    =        7326134
32  feet           Y    =         2233005
74  meter
 Z    =       15553791
88                 Z    =         4740795
77
 XDOT =     -17293
910245                 XDOT =       -5271
183843
 YDOT =      14346
155977  feet/sec       YDOT =        4372
708342  meter/sec
 ZDOT =       8900
778230                 ZDOT =        2712
957205


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
55537957  
00016717  00000-0  10270-3 0  9014
2 25544  51
6433 355
8788 0002151 332
9599  27
1441 15
54223534 27997


Satellite: ISS
Catalog Number: 25544
Epoch time:      18100
55537957   =   yrday
fracday
Element set:     901
Inclination:       51
6433  deg
RA of node:       355
8788  deg
Eccentricity:     
0002151     
Arg of perigee:   332
9599  deg
Mean anomaly:      27
1441  deg
Mean motion:   15
54223534  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2799
Checksum:              325


Coasting Arc #3 (Orbit 2808)
---------------------------------------

Vector Time (GMT): 2018/101/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1133689
08                 A    =         6777810
29  meter
 Y    =        4267695
02  meter          E    =           
0005585
 Z    =        5140304
76                 I    =           51
57638
 XDOT =      -7519
905683                 Wp   =           34
40186
 YDOT =       -184
977385  meter/sec      RA   =          352
30987  deg
 ZDOT =      -1499
623099                 TA   =           70
07956
                                          MA   =           70
01940
                                          Ha   =            220
713  n
mi
                                          Hp   =            214
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3719452
37                 X    =        -1206296
24
 Y    =       14001624
10  feet           Y    =         4254611
76  meter
 Z    =       16864516
93                 Z    =         5134621
01
 XDOT =     -24671
606571                 XDOT =       -7509
993943
 YDOT =       -606
881183  feet/sec       YDOT =        -269
014842  meter/sec
 ZDOT =      -4920
023292                 ZDOT =       -1536
128100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12330231
70                 X    =        -3758254
62
 Y    =       -7663056
45  feet           Y    =        -2335699
61  meter
 Z    =       16838488
25                 Z    =         5132371
22
 XDOT =       7045
874112                 XDOT =        2147
582429
 YDOT =     -22544
342942  feet/sec       YDOT =       -6871
515729  meter/sec
 ZDOT =      -5082
854461                 ZDOT =       -1549
254040


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
19835660  
00016717  00000-0  10270-3 0  9028
2 25544  51
6409 352
6722 0001958 337
7050  22
4018 15
54243106 28099


Satellite: ISS
Catalog Number: 25544
Epoch time:      18101
19835660   =   yrday
fracday
Element set:     902
Inclination:       51
6409  deg
RA of node:       352
6722  deg
Eccentricity:     
0001958     
Arg of perigee:   337
7050  deg
Mean anomaly:      22
4018  deg
Mean motion:   15
54243106  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2809
Checksum:              291


Coasting Arc #4 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2018/102/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2863921
24                 A    =         6780792
97  meter
 Y    =       -4257989
88  meter          E    =           
0007838
 Z    =       -4439842
26                 I    =           51
55355
 XDOT =       6818
483753                 Wp   =           98
77725
 YDOT =       1149
703184  meter/sec      RA   =          347
30992  deg
 ZDOT =       3299
470024                 TA   =          204
56200
                                          MA   =          204
59935
                                          Ha   =            220
731  n
mi
                                          Hp   =            214
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9396067
07                 X    =         2932888
84
 Y    =      -13969783
06  feet           Y    =        -4225578
31  meter
 Z    =      -14566411
60                 Z    =        -4425762
41
 XDOT =      22370
353519                 XDOT =        6789
093587
 YDOT =       3771
992074  feet/sec       YDOT =        1225
788129  meter/sec
 ZDOT =      10825
032888                 ZDOT =        3332
520408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10909344
88                 X    =         3325168
32
 Y    =       12894662
90  feet           Y    =         3930293
25  meter
 Z    =      -14502935
06                 Z    =        -4420494
60
 XDOT =      -8680
993751                 XDOT =       -2645
966895
 YDOT =      19671
076831  feet/sec       YDOT =        5995
744218  meter/sec
 ZDOT =      10972
289593                 ZDOT =        3344
353868


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
16282206  
00016717  00000-0  10270-3 0  9039
2 25544  51
6409 347
8647 0002094 337
7882  22
3179 15
54217660 28246


Satellite: ISS
Catalog Number: 25544
Epoch time:      18102
16282206   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:       347
8647  deg
Eccentricity:     
0002094     
Arg of perigee:   337
7882  deg
Mean anomaly:      22
3179  deg
Mean motion:   15
54217660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2824
Checksum:              309


Coasting Arc #5 (Orbit 2839)
---------------------------------------

Vector Time (GMT): 2018/103/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4343883
65                 A    =         6784560
74  meter
 Y    =        4080693
19  meter          E    =           
0012234
 Z    =        3232809
45                 I    =           51
53406
 XDOT =      -5604
507494                 Wp   =           83
33064
 YDOT =      -2181
972832  meter/sec      RA   =          342
31620  deg
 ZDOT =      -4759
569356                 TA   =           59
15574
                                          MA   =           59
03543
                                          Ha   =            220
762  n
mi
                                          Hp   =            214
670

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14251586
76                 X    =        -4404895
57
 Y    =       13388101
01  feet           Y    =         4031776
07  meter
 Z    =       10606330
21                 Z    =         3211559
70
 XDOT =     -18387
491779                 XDOT =       -5556
571967
 YDOT =      -7158
703517  feet/sec       YDOT =       -2244
378736  meter/sec
 ZDOT =     -15615
385027                 ZDOT =       -4786
677576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9349893
28                 X    =        -2849847
47
 Y    =      -17232049
18  feet           Y    =        -5252328
59  meter
 Z    =       10510908
18                 Z    =         3203724
81
 XDOT =      10277
930043                 XDOT =        3132
713077
 YDOT =     -15209
124405  feet/sec       YDOT =       -4635
741119  meter/sec
 ZDOT =     -15735
963926                 ZDOT =       -4796
321805


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   18103
19158036  
00016717  00000-0  10270-3 0  9047
2 25544  51
6402 342
7351 0002210 343
5631  16
5450 15
54271875 28405


Satellite: ISS
Catalog Number: 25544
Epoch time:      18103
19158036   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:       342
7351  deg
Eccentricity:     
0002210     
Arg of perigee:   343
5631  deg
Mean anomaly:      16
5450  deg
Mean motion:   15
54271875  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2840
Checksum:              276


Coasting Arc #6 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2018/104/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5408234
01                 A    =         6787729
05  meter
 Y    =       -3724492
76  meter          E    =           
0009300
 Z    =       -1701135
83                 I    =           51
51303
 XDOT =       4004
940738                 Wp   =           28
23029
 YDOT =       3227
421532  meter/sec      RA   =          337
33207  deg
 ZDOT =       5687
057475                 TA   =          313
08370
                                          MA   =          313
16149
                                          Ha   =            220
839  n
mi
                                          Hp   =            214
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17743549
90                 X    =         5457743
64
 Y    =      -12219464
44  feet           Y    =        -3663737
51  meter
 Z    =       -5581154
29                 Z    =        -1674743
68
 XDOT =      13139
569349                 XDOT =        3940
928229
 YDOT =      10588
653320  feet/sec       YDOT =        3271
850186  meter/sec
 ZDOT =      18658
325048                 ZDOT =        5706
356441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7695204
57                 X    =         2345498
35
 Y    =       20155374
27  feet           Y    =         6143358
08  meter
 Z    =       -5462862
99                 Z    =        -1665080
64
 XDOT =     -11884
644672                 XDOT =       -3622
439696
 YDOT =       9598
932776  feet/sec       YDOT =        2925
754710  meter/sec
 ZDOT =      18743
902266                 ZDOT =        5713
141411


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   18104
15603885  
00016717  00000-0  10270-3 0  9052
2 25544  51
6396 337
9276 0002050 351
0126   9
0990 15
54273252 28557


Satellite: ISS
Catalog Number: 25544
Epoch time:      18104
15603885   =   yrday
fracday
Element set:     905
Inclination:       51
6396  deg
RA of node:       337
9276  deg
Eccentricity:     
0002050     
Arg of perigee:   351
0126  deg
Mean anomaly:       9
0990  deg
Mean motion:   15
54273252  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              303


Coasting Arc #7 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2018/105/03:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6027925
14                 A    =         6788950
90  meter
 Y    =        3113752
47  meter          E    =           
0010186
 Z    =         -49150
37                 I    =           51
48577
 XDOT =      -2158
170132                 Wp   =          127
18973
 YDOT =      -4259
060150  meter/sec      RA   =          332
35084  deg
 ZDOT =      -5998
948591                 TA   =           53
34073
                                          MA   =           53
24714
                                          Ha   =            220
843  n
mi
                                          Hp   =            214
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19776657
28                 X    =        -6062057
21
 Y    =       10215723
32  feet           Y    =         3046153
21  meter
 Z    =        -161254
48                 Z    =          -78515
48
 XDOT =      -7080
610669                 XDOT =       -2081
243676
 YDOT =     -13973
294456  feet/sec       YDOT =       -4282
764730  meter/sec
 ZDOT =     -19681
589867                 ZDOT =       -6009
245120

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5649151
69                 X    =        -1721861
43
 Y    =      -21529156
80  feet           Y    =        -6562086
99  meter
 Z    =        -292697
66                 Z    =          -89214
25
 XDOT =      13585
687291                 XDOT =        4140
917486
 YDOT =      -3317
865632  feet/sec       YDOT =       -1011
285444  meter/sec
 ZDOT =     -19726
853587                 ZDOT =       -6012
744973


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   18105
18479134  
00016717  00000-0  10270-3 0  9065
2 25544  51
6383 332
7976 0002280 351
5628   8
5486 15
54256841 28717


Satellite: ISS
Catalog Number: 25544
Epoch time:      18105
18479134   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:       332
7976  deg
Eccentricity:     
0002280     
Arg of perigee:   351
5628  deg
Mean anomaly:       8
5486  deg
Mean motion:   15
54256841  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2871
Checksum:              326


Coasting Arc #8 (Orbit 2873)
---------------------------------------

Vector Time (GMT): 2018/105/08:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         781172
47                 A    =         6779339
05  meter
 Y    =       -4763046
85  meter          E    =           
0010215
 Z    =       -4769822
55                 I    =           51
45030
 XDOT =       7043
055500                 Wp   =           96
63963
 YDOT =      -1473
252438  meter/sec      RA   =          331
26334  deg
 ZDOT =       2628
322806                 TA   =          199
36254
                                          MA   =          199
40138
                                          Ha   =            220
826  n
mi
                                          Hp   =            214
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2562901
81                 X    =          857545
69
 Y    =      -15626794
12  feet           Y    =        -4753884
64  meter
 Z    =      -15649024
12                 Z    =        -4765841
91
 XDOT =      23107
137466                 XDOT =        7046
239181
 YDOT =      -4833
505373  feet/sec       YDOT =       -1394
474102  meter/sec
 ZDOT =       8623
106318                 ZDOT =        2662
543834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9141851
35                 X    =         2786436
29
 Y    =      -12952604
51  feet           Y    =        -3947953
85  meter
 Z    =      -15630537
63                 Z    =        -4764187
87
 XDOT =      21937
208067                 XDOT =        6686
461019
 YDOT =       4907
395907  feet/sec       YDOT =        1495
774273  meter/sec
 ZDOT =       8775
950067                 ZDOT =        2674
909580


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   18105
37768308  
00016717  00000-0  10270-3 0  9071
2 25544  51
6412 331
8367 0002365 349
3320  10
7782 15
54259234 28748


Satellite: ISS
Catalog Number: 25544
Epoch time:      18105
37768308   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:       331
8367  deg
Eccentricity:     
0002365     
Arg of perigee:   349
3320  deg
Mean anomaly:      10
7782  deg
Mean motion:   15
54259234  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2874
Checksum:              313


Coasting Arc #9 (Orbit 2889)
---------------------------------------

Vector Time (GMT): 2018/106/08:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2348018
86                 A    =         6783113
85  meter
 Y    =        5148373
97  meter          E    =           
0011861
 Z    =        3733821
35                 I    =           51
43425
 XDOT =      -6380
551144                 Wp   =           72
58896
 YDOT =        184
633411  meter/sec      RA   =          326
25942  deg
 ZDOT =      -4252
339741                 TA   =           62
63061
                                          MA   =           62
50996
                                          Ha   =            220
926  n
mi
                                          Hp   =            214
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7703473
96                 X    =        -2423552
12
 Y    =       16890990
72  feet           Y    =         5121694
76  meter
 Z    =       12250070
06                 Z    =         3722231
45
 XDOT =     -20933
566744                 XDOT =       -6361
485576
 YDOT =        605
752660  feet/sec       YDOT =         113
387974  meter/sec
 ZDOT =     -13951
245868                 ZDOT =       -4283
288467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14098232
44                 X    =        -4297141
25
 Y    =       12131438
49  feet           Y    =         3697662
45  meter
 Z    =       12197595
56                 Z    =         3717827
13
 XDOT =     -18323
946392                 XDOT =       -5585
138860
 YDOT =      -7080
003148  feet/sec       YDOT =       -2157
984959  meter/sec
 ZDOT =     -14089
286876                 ZDOT =       -4294
414640


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   18106
40643124  
00016717  00000-0  10270-3 0  9085
2 25544  51
6411 326
7079 0002345 352
8270   7
2849 15
54249799 28909


Satellite: ISS
Catalog Number: 25544
Epoch time:      18106
40643124   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:       326
7079  deg
Eccentricity:     
0002345     
Arg of perigee:   352
8270  deg
Mean anomaly:       7
2849  deg
Mean motion:   15
54249799  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2890
Checksum:              318


Coasting Arc #10 (Orbit 2904)
---------------------------------------

Vector Time (GMT): 2018/107/08:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3605260
09                 A    =         6786666
83  meter
 Y    =       -5259540
59  meter          E    =           
0007709
 Z    =       -2314878
87                 I    =           51
42032
 XDOT =       5299
659365                 Wp   =           30
33820
 YDOT =       1264
972871  meter/sec      RA   =          321
26298  deg
 ZDOT =       5394
142861                 TA   =          303
78034
                                          MA   =          303
85375
                                          Ha   =            220
931  n
mi
                                          Hp   =            214
470

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11828281
14                 X    =         3675050
43
 Y    =      -17255710
61  feet           Y    =        -5218834
00  meter
 Z    =       -7594746
95                 Z    =        -2297195
63
 XDOT =      17387
333874                 XDOT =        5258
917808
 YDOT =       4150
173461  feet/sec       YDOT =        1324
009813  meter/sec
 ZDOT =      17697
319097                 ZDOT =        5419
788230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17785778
54                 X    =         5421105
30
 Y    =      -11069664
48  feet           Y    =        -3374033
73  meter
 Z    =       -7515089
80                 Z    =        -2290599
37
 XDOT =      13363
593441                 XDOT =        4073
223281
 YDOT =       9411
812805  feet/sec       YDOT =        2868
720543  meter/sec
 ZDOT =      17811
481490                 ZDOT =        5428
939558


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   18107
37087805  
00016717  00000-0  10270-3 0  9091
2 25544  51
6417 321
8984 0002431 356
0098   4
1035 15
54277490 29055


Satellite: ISS
Catalog Number: 25544
Epoch time:      18107
37087805   =   yrday
fracday
Element set:     909
Inclination:       51
6417  deg
RA of node:       321
8984  deg
Eccentricity:     
0002431     
Arg of perigee:   356
0098  deg
Mean anomaly:       4
1035  deg
Mean motion:   15
54277490  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2905
Checksum:              310


Coasting Arc #11 (Orbit 2920)
---------------------------------------

Vector Time (GMT): 2018/108/08:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4534724
49                 A    =         6788859
43  meter
 Y    =        5009083
12  meter          E    =           
0011732
 Z    =         608203
78                 I    =           51
40178
 XDOT =      -3925
087827                 Wp   =          119
69961
 YDOT =      -2820
814987  meter/sec      RA   =          316
27492  deg
 ZDOT =      -5952
505009                 TA   =           53
71346
                                          MA   =           53
60515
                                          Ha   =            220
989  n
mi
                                          Hp   =            214
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14877705
03                 X    =        -4593354
78
 Y    =       16433999
75  feet           Y    =         4958044
91  meter
 Z    =        1995419
24                 Z    =          586032
67
 XDOT =     -12877
584733                 XDOT =       -3864
338294
 YDOT =      -9254
642347  feet/sec       YDOT =       -2864
368546  meter/sec
 ZDOT =     -19529
215910                 ZDOT =       -5971
424445

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20058650
34                 X    =        -6113876
62
 Y    =        9458364
65  feet           Y    =         2882909
54  meter
 Z    =        1895794
67                 Z    =          577838
22
 XDOT =      -7528
258243                 XDOT =       -2294
613113
 YDOT =     -11978
292397  feet/sec       YDOT =       -3650
983523  meter/sec
 ZDOT =     -19613
146423                 ZDOT =       -5978
087030


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   18108
39962065  
00016717  00000-0  10270-3 0  9106
2 25544  51
6412 316
7696 0002312 359
4382    
6768 15
54241367 29210


Satellite: ISS
Catalog Number: 25544
Epoch time:      18108
39962065   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:       316
7696  deg
Eccentricity:     
0002312     
Arg of perigee:   359
4382  deg
Mean anomaly:        
6768  deg
Mean motion:   15
54241367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2921
Checksum:              310


Coasting Arc #12 (Orbit 2921)
---------------------------------------

Vector Time (GMT): 2018/108/10:37:01
974
Vector Time (MET): N/A
Weight (LBS)     : 928428
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5027600
71                 A    =         6780431
92  meter
 Y    =        -199327
30  meter          E    =           
0010405
 Z    =       -4555589
45                 I    =           51
37005
 XDOT =       3025
674096                 Wp   =           56
80335
 YDOT =      -6335
419697  meter/sec      RA   =          315
92202  deg
 ZDOT =      -3061
463966                 TA   =          182
41968
                                          MA   =          182
42472
                                          Ha   =            220
921  n
mi
                                          Hp   =            214
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16494752
99                 X    =        -5002869
04
 Y    =        -653960
97  feet           Y    =         -255411
26  meter
 Z    =      -14946159
61                 Z    =        -4579952
18
 XDOT =       9926
752283                 XDOT =        3111
164874
 YDOT =     -20785
497695  feet/sec       YDOT =       -6301
106614  meter/sec
 ZDOT =     -10044
173117                 ZDOT =       -3046
558165

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16391909
31                 X    =        -4996253
96
 Y    =         742759
68  feet           Y    =          226393
15  meter
 Z    =      -15054761
57                 Z    =        -4588691
33
 XDOT =       8241
564729                 XDOT =        2512
028929
 YDOT =     -20366
079244  feet/sec       YDOT =       -6207
580953  meter/sec
 ZDOT =      -9976
742271                 ZDOT =       -3040
911044


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   18108
46391582  
00016717  00000-0  10270-3 0  9115
2 25544  51
6404 316
4487 0002296 341
6735  18
4334 15
54124266 29227


Satellite: ISS
Catalog Number: 25544
Epoch time:      18108
46391582   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:       316
4487  deg
Eccentricity:     
0002296     
Arg of perigee:   341
6735  deg
Mean anomaly:      18
4334  deg
Mean motion:   15
54124266  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2922
Checksum:              306


Coasting Arc #13 (Orbit 2937)
---------------------------------------

Vector Time (GMT): 2018/109/10:37:01
974
Vector Time (MET): N/A
Weight (LBS)     : 928428
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4064318
32                 A    =         6777892
68  meter
 Y    =        1627552
55  meter          E    =           
0002861
 Z    =        5171718
14                 I    =           51
33931
 XDOT =      -4144
949705                 Wp   =           91
33505
 YDOT =       6329
389669  meter/sec      RA   =          310
90600  deg
 ZDOT =       1264
860751                 TA   =          346
47033
                                          MA   =          346
47799
                                          Ha   =            220
875  n
mi
                                          Hp   =            214
850

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13334377
69                 X    =         4020694
61
 Y    =        5339739
32  feet           Y    =         1672758
68  meter
 Z    =       16967579
21                 Z    =         5191355
56
 XDOT =     -13598
916356                 XDOT =       -4221
562734
 YDOT =      20765
714137  feet/sec       YDOT =        6282
609630  meter/sec
 ZDOT =       4149
805613                 ZDOT =        1244
539543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13698770
02                 X    =         4175385
10
 Y    =        3961250
81  feet           Y    =         1207389
25  meter
 Z    =       17054893
16                 Z    =         5198331
43
 XDOT =     -11142
619256                 XDOT =       -3396
270349
 YDOT =      21051
428955  feet/sec       YDOT =        6416
475545  meter/sec
 ZDOT =       4058
234609                 ZDOT =        1236
949909


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   18109
49275164  
00016717  00000-0  10270-3 0  9127
2 25544  51
6412 311
3196 0002295 346
7724  13
3368 15
54114373 29386


Satellite: ISS
Catalog Number: 25544
Epoch time:      18109
49275164   =   yrday
fracday
Element set:     912
Inclination:       51
6412  deg
RA of node:       311
3196  deg
Eccentricity:     
0002295     
Arg of perigee:   346
7724  deg
Mean anomaly:      13
3368  deg
Mean motion:   15
54114373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2938
Checksum:              307


Coasting Arc #14 (Orbit 2952)
---------------------------------------

Vector Time (GMT): 2018/110/10:37:01
974
Vector Time (MET): N/A
Weight (LBS)     : 928428
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2972828
26                 A    =         6777460
59  meter
 Y    =       -3082845
58  meter          E    =           
0014146
 Z    =       -5264996
19                 I    =           51
31641
 XDOT =       4893
323825                 Wp   =           85
88629
 YDOT =      -5853
205712  meter/sec      RA   =          305
88274  deg
 ZDOT =        666
845586                 TA   =          190
50345
                                          MA   =          190
53303
                                          Ha   =            220
988  n
mi
                                          Hp   =            214
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9753373
57                 X    =        -2912559
19
 Y    =      -10114322
77  feet           Y    =        -3115752
77  meter
 Z    =      -17273609
56                 Z    =        -5279290
99
 XDOT =      16054
212023                 XDOT =        4955
173057
 YDOT =     -19203
430814  feet/sec       YDOT =       -5798
139383  meter/sec
 ZDOT =       2187
813604                 ZDOT =         690
766144

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10777323
12                 X    =        -3284928
09
 Y    =       -8893096
71  feet           Y    =        -2710615
88  meter
 Z    =      -17336883
96                 Z    =        -5284282
23
 XDOT =      12984
615875                 XDOT =        3957
710919
 YDOT =     -20194
230142  feet/sec       YDOT =       -6155
201347  meter/sec
 ZDOT =       2295
355295                 ZDOT =         699
624294


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   18110
45728008  
00016717  00000-0  10270-3 0  9136
2 25544  51
6403 306
5098 0002363 349
2220  10
8882 15
54148241 29539


Satellite: ISS
Catalog Number: 25544
Epoch time:      18110
45728008   =   yrday
fracday
Element set:     913
Inclination:       51
6403  deg
RA of node:       306
5098  deg
Eccentricity:     
0002363     
Arg of perigee:   349
2220  deg
Mean anomaly:      10
8882  deg
Mean motion:   15
54148241  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2953
Checksum:              289


Coasting Arc #15 (Orbit 2968)
---------------------------------------

Vector Time (GMT): 2018/111/10:37:01
974
Vector Time (MET): N/A
Weight (LBS)     : 928428
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1816212
61                 A    =         6779452
80  meter
 Y    =        4438690
96  meter          E    =           
0008472
 Z    =        4788895
01                 I    =           51
30454
 XDOT =      -5308
664564                 Wp   =           45
26552
 YDOT =       4919
917449  meter/sec      RA   =          300
86270  deg
 ZDOT =      -2538
162228                 TA   =           69
86700
                                          MA   =           69
77587
                                          Ha   =            220
962  n
mi
                                          Hp   =            214
709

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5958702
78                 X    =         1743180
85
 Y    =       14562634
38  feet           Y    =         4458592
69  meter
 Z    =       15711597
80                 Z    =         4797540
29
 XDOT =     -17416
878490                 XDOT =       -5350
956715
 YDOT =      16141
461448  feet/sec       YDOT =        4860
315872  meter/sec
 ZDOT =      -8327
303899                 ZDOT =       -2564
052753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7786522
14                 X    =         2373331
95
 Y    =       13629180
93  feet           Y    =         4154174
35  meter
 Z    =       15749484
58                 Z    =         4800442
90
 XDOT =     -14003
775892                 XDOT =       -4268
350892
 YDOT =      17790
222604  feet/sec       YDOT =        5422
459850  meter/sec
 ZDOT =      -8443
482789                 ZDOT =       -2573
573554


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   18111
48610845  
00016717  00000-0  10270-3 0  9140
2 25544  51
6401 301
3817 0002396 350
9958   9
1152 15
54160972 29695


Satellite: ISS
Catalog Number: 25544
Epoch time:      18111
48610845   =   yrday
fracday
Element set:     914
Inclination:       51
6401  deg
RA of node:       301
3817  deg
Eccentricity:     
0002396     
Arg of perigee:   350
9958  deg
Mean anomaly:       9
1152  deg
Mean motion:   15
54160972  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2969
Checksum:              309


Coasting Arc #16 (Orbit 2983)
---------------------------------------

Vector Time (GMT): 2018/112/10:37:01
974
Vector Time (MET): N/A
Weight (LBS)     : 928428
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -722045
42                 A    =         6783032
00  meter
 Y    =       -5552613
83  meter          E    =           
0005798
 Z    =       -3832765
32                 I    =           51
29953
 XDOT =       5393
879500                 Wp   =           82
45802
 YDOT =      -3547
059297  meter/sec      RA   =          295
84813  deg
 ZDOT =       4128
695537                 TA   =          231
17553
                                          MA   =          231
22731
                                          Ha   =            221
039  n
mi
                                          Hp   =            214
665

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2368915
43                 X    =         -641283
29
 Y    =      -18217236
99  feet           Y    =        -5560236
65  meter
 Z    =      -12574689
37                 Z    =        -3836076
65
 XDOT =      17696
455054                 XDOT =        5413
087690
 YDOT =     -11637
333652  feet/sec       YDOT =       -3486
633847  meter/sec
 ZDOT =      13545
589032                 ZDOT =        4154
943879

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5053724
21                 X    =        -1540375
14
 Y    =      -17651866
10  feet           Y    =        -5380288
79  meter
 Z    =      -12588637
40                 Z    =        -3837016
68
 XDOT =      14325
697897                 XDOT =        4366
472719
 YDOT =     -13831
155050  feet/sec       YDOT =       -4215
736059  meter/sec
 ZDOT =      13663
153537                 ZDOT =        4164
529198


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   18112
45063402  
00016717  00000-0  10270-3 0  9150
2 25544  51
6392 296
5729 0002307 353
4424   6
6698 15
54148038 29842


Satellite: ISS
Catalog Number: 25544
Epoch time:      18112
45063402   =   yrday
fracday
Element set:     915
Inclination:       51
6392  deg
RA of node:       296
5729  deg
Eccentricity:     
0002307     
Arg of perigee:   353
4424  deg
Mean anomaly:       6
6698  deg
Mean motion:   15
54148038  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2984
Checksum:              316


Coasting Arc #17 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2018/113/10:37:01
974
Vector Time (MET): N/A
Weight (LBS)     : 928428
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -309774
36                 A    =         6786618
53  meter
 Y    =        6318327
07  meter          E    =           
0013140
 Z    =        2444684
96                 I    =           51
29892
 XDOT =      -5235
480616                 Wp   =           94
63377
 YDOT =       1805
207092  meter/sec      RA   =          290
84325  deg
 ZDOT =      -5305
338227                 TA   =           57
85658
                                          MA   =           57
72916
                                          Ha   =            221
070  n
mi
                                          Hp   =            214
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1016320
09                 X    =         -392279
61
 Y    =       20729419
51  feet           Y    =         6314401
67  meter
 Z    =        8020619
93                 Z    =         2442979
71
 XDOT =     -17176
773673                 XDOT =       -5229
507238
 YDOT =       5922
595446  feet/sec       YDOT =        1746
693682  meter/sec
 ZDOT =     -17405
965313                 ZDOT =       -5330
755937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2478606
48                 X    =          755479
26
 Y    =       20609095
94  feet           Y    =         6281652
44  meter
 Z    =        8012100
74                 Z    =         2442088
31
 XDOT =     -14300
083677                 XDOT =       -4358
665505
 YDOT =       8561
037769  feet/sec       YDOT =        2609
404312  meter/sec
 ZDOT =     -17519
566934                 ZDOT =       -5339
964002


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   18113
47945538  
00016717  00000-0  10270-3 0  9163
2 25544  51
6396 291
4436 0002574 356
7094   3
4042 15
54191947 30005


Satellite: ISS
Catalog Number: 25544
Epoch time:      18113
47945538   =   yrday
fracday
Element set:     916
Inclination:       51
6396  deg
RA of node:       291
4436  deg
Eccentricity:     
0002574     
Arg of perigee:   356
7094  deg
Mean anomaly:       3
4042  deg
Mean motion:   15
54191947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3000
Checksum:              312


Coasting Arc #18 (Orbit 3014)
---------------------------------------

Vector Time (GMT): 2018/114/10:37:01
974
Vector Time (MET): N/A
Weight (LBS)     : 928428
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1188687
76                 A    =         6788989
57  meter
 Y    =       -6625994
89  meter          E    =           
0012155
 Z    =        -830744
21                 I    =           51
29342
 XDOT =       4884
062998                 Wp   =           32
84234
 YDOT =        141
396522  meter/sec      RA   =          285
84582  deg
 ZDOT =       5911
446551                 TA   =          318
12775
                                          MA   =          318
22066
                                          Ha   =            221
177  n
mi
                                          Hp   =            214
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3899894
22                 X    =         1266728
42
 Y    =      -21738828
38  feet           Y    =        -6612265
84  meter
 Z    =       -2725538
74                 Z    =         -824780
21
 XDOT =      16023
828733                 XDOT =        4853
404128
 YDOT =        463
899350  feet/sec       YDOT =         195
842237  meter/sec
 ZDOT =      19394
509682                 ZDOT =        5935
097207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -223649
24                 X    =          -68168
29
 Y    =      -22088122
74  feet           Y    =        -6732459
81  meter
 Z    =       -2698001
15                 Z    =         -822350
75
 XDOT =      14090
433773                 XDOT =        4294
764214
 YDOT =      -2503
984908  feet/sec       YDOT =        -763
214600  meter/sec
 ZDOT =      19499
950912                 ZDOT =        5943
585038


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   18114
44397532  
00016717  00000-0  10270-3 0  9177
2 25544  51
6374 286
6349 0002309   2
8088 357
3077 15
54146144 30152


Satellite: ISS
Catalog Number: 25544
Epoch time:      18114
44397532   =   yrday
fracday
Element set:     917
Inclination:       51
6374  deg
RA of node:       286
6349  deg
Eccentricity:     
0002309     
Arg of perigee:     2
8088  deg
Mean anomaly:     357
3077  deg
Mean motion:   15
54146144  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3015
Checksum:              313
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list