[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: September 2nd 2020

  • spaceflight nasa gov will be taken offline by October 2020 *
  • Do you use any data hosted on this site? *
  • Please let us know how you use the data at the survey link below *
  • *
  • https://www surveymonkey com/r/KRLJMCN *
  • *

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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


249/11:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 221 8

253/10:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 221 7

254/20:33:53 536 0 4 1 4 1 4
N/A -1 4 0 1 229 3
000/00:03:43 072 -0 1 -0 0 222 4

Coasting Arc #1 (Orbit 368)
---------------------------------------

Vector Time (GMT): 2020/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3893493
39                 A    =         6793156
19  meter
 Y    =        2540174
58  meter          E    =           
0007390
 Z    =        4948477
26                 I    =           51
46741
 XDOT =      -5753
761167                 Wp   =          114
26626
 YDOT =       4571
943721  meter/sec      RA   =          335
15942  deg
 ZDOT =       2174
659024                 TA   =          314
43548
                                          MA   =          314
49592
                                          Ha   =            229
135  n
mi
                                          Hp   =            221
837

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12773928
43                 X    =         3840762
63
 Y    =        8333906
11  feet           Y    =         2583419
67  meter
 Z    =       16235161
62                 Z    =         4967261
83
 XDOT =     -18877
169183                 XDOT =       -5815
021424
 YDOT =      14999
815359  feet/sec       YDOT =        4507
258560  meter/sec
 ZDOT =       7134
708085                 ZDOT =        2146
561189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8882292
00                 X    =        -2707322
60
 Y    =      -12284755
83  feet           Y    =        -3744393
58  meter
 Z    =       16321684
18                 Z    =         4974849
34
 XDOT =      22120
134746                 XDOT =        6742
217071
 YDOT =      -6662
866998  feet/sec       YDOT =       -2030
841861  meter/sec
 ZDOT =       7004
815439                 ZDOT =        2135
067746


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   20244
55212941  
00016717  00000-0  10270-3 0  9008
2 25544  51
6452 335
5071 0001496  79
4117 280
7201 15
49230409  3693


Satellite: ISS
Catalog Number: 25544
Epoch time:      20244
55212941   =   yrday
fracday
Element set:     900
Inclination:       51
6452  deg
RA of node:       335
5071  deg
Eccentricity:     
0001496     
Arg of perigee:    79
4117  deg
Mean anomaly:     280
7201  deg
Mean motion:   15
49230409  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             369
Checksum:              285


Coasting Arc #2 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2020/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4032137
31                 A    =         6793173
83  meter
 Y    =       -2271496
77  meter          E    =           
0014071
 Z    =       -4985852
87                 I    =           51
43616
 XDOT =       5395
666975                 Wp   =           75
14793
 YDOT =      -5005
376459  meter/sec      RA   =          330
19972  deg
 ZDOT =      -2084
587950                 TA   =          174
46260
                                          MA   =          174
44702
                                          Ha   =            229
297  n
mi
                                          Hp   =            221
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13228796
96                 X    =        -3982219
11
 Y    =       -7452417
23  feet           Y    =        -2316308
11  meter
 Z    =      -16357785
00                 Z    =        -5005317
71
 XDOT =      17702
319472                 XDOT =        5461
363131
 YDOT =     -16421
838776  feet/sec       YDOT =       -4944
671003  meter/sec
 ZDOT =      -6839
199310                 ZDOT =       -2058
218635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9817977
90                 X    =         2992519
66
 Y    =       11454479
67  feet           Y    =         3491325
40  meter
 Z    =      -16447459
60                 Z    =        -5013185
69
 XDOT =     -21425
729283                 XDOT =       -6530
562286
 YDOT =       8725
962280  feet/sec       YDOT =        2659
673303  meter/sec
 ZDOT =      -6717
276578                 ZDOT =       -2047
425901


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   20245
51973125  
00016717  00000-0  10270-3 0  9014
2 25544  51
6445 330
7204 0001423  82
0955 278
0356 15
49186074  3846


Satellite: ISS
Catalog Number: 25544
Epoch time:      20245
51973125   =   yrday
fracday
Element set:     901
Inclination:       51
6445  deg
RA of node:       330
7204  deg
Eccentricity:     
0001423     
Arg of perigee:    82
0955  deg
Mean anomaly:     278
0356  deg
Mean motion:   15
49186074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              294


Coasting Arc #3 (Orbit 399)
---------------------------------------

Vector Time (GMT): 2020/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4146305
51                 A    =         6792913
48  meter
 Y    =        1978637
95  meter          E    =           
0006993
 Z    =        4999107
83                 I    =           51
40775
 XDOT =      -5018
871177                 Wp   =          115
27784
 YDOT =       5433
185482  meter/sec      RA   =          325
23728  deg
 ZDOT =       2007
118609                 TA   =          315
11739
                                          MA   =          315
17391
                                          Ha   =            229
103  n
mi
                                          Hp   =            221
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13603364
52                 X    =         4099589
20
 Y    =        6491594
32  feet           Y    =         2024744
00  meter
 Z    =       16401272
42                 Z    =         5019135
06
 XDOT =     -16466
112787                 XDOT =       -5089
002960
 YDOT =      17825
411686  feet/sec       YDOT =        5376
668856  meter/sec
 ZDOT =       6585
034805                 ZDOT =        1982
568629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10677592
24                 X    =        -3254530
11
 Y    =      -10495034
60  feet           Y    =        -3198886
55  meter
 Z    =       16493554
28                 Z    =         5027235
35
 XDOT =      20610
655302                 XDOT =        6282
127736
 YDOT =     -10772
508014  feet/sec       YDOT =       -3283
460443  meter/sec
 ZDOT =       6471
502956                 ZDOT =        1972
514101


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   20246
55183382  
00016717  00000-0  10270-3 0  9028
2 25544  51
6452 325
6137 0001467  82
0639 278
0678 15
49237634  4004


Satellite: ISS
Catalog Number: 25544
Epoch time:      20246
55183382   =   yrday
fracday
Element set:     902
Inclination:       51
6452  deg
RA of node:       325
6137  deg
Eccentricity:     
0001467     
Arg of perigee:    82
0639  deg
Mean anomaly:     278
0678  deg
Mean motion:   15
49237634  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             400
Checksum:              306


Coasting Arc #4 (Orbit 414)
---------------------------------------

Vector Time (GMT): 2020/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4245112
76                 A    =         6792940
50  meter
 Y    =       -1702881
11  meter          E    =           
0014521
 Z    =       -5035560
53                 I    =           51
37903
 XDOT =       4596
810309                 Wp   =           76
23950
 YDOT =      -5806
860229  meter/sec      RA   =          320
27326  deg
 ZDOT =      -1912
805596                 TA   =          175
10042
                                          MA   =          175
08620
                                          Ha   =            229
329  n
mi
                                          Hp   =            221
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13927535
30                 X    =        -4201295
54
 Y    =       -5586880
29  feet           Y    =        -1750108
36  meter
 Z    =      -16520867
89                 Z    =        -5056074
84
 XDOT =      15081
398653                 XDOT =        4670
693929
 YDOT =     -19051
378704  feet/sec       YDOT =       -5755
042428  meter/sec
 ZDOT =      -6275
608911                 ZDOT =       -1890
296501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11441262
28                 X    =         3487296
74
 Y    =        9547477
29  feet           Y    =         2910071
08  meter
 Z    =      -16615406
76                 Z    =        -5064375
98
 XDOT =     -19532
855727                 XDOT =       -5953
614426
 YDOT =      12674
366199  feet/sec       YDOT =        3863
146817  meter/sec
 ZDOT =      -6171
493076                 ZDOT =       -1881
071090


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   20247
51942983  
00016717  00000-0  10270-3 0  9036
2 25544  51
6439 320
8268 0001533  82
3887 277
7437 15
49192059  4159


Satellite: ISS
Catalog Number: 25544
Epoch time:      20247
51942983   =   yrday
fracday
Element set:     903
Inclination:       51
6439  deg
RA of node:       320
8268  deg
Eccentricity:     
0001533     
Arg of perigee:    82
3887  deg
Mean anomaly:     277
7437  deg
Mean motion:   15
49192059  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              329


Coasting Arc #5 (Orbit 430)
---------------------------------------

Vector Time (GMT): 2020/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4317458
65                 A    =         6792710
72  meter
 Y    =        1406259
83  meter          E    =           
0006713
 Z    =        5047568
83                 I    =           51
35314
 XDOT =      -4157
124430                 Wp   =          115
65080
 YDOT =       6172
715682  meter/sec      RA   =          315
30721  deg
 ZDOT =       1831
325221                 TA   =          316
50743
                                          MA   =          316
56036
                                          Ha   =            229
139  n
mi
                                          Hp   =            221
795

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14164890
58                 X    =         4276894
52
 Y    =        4613713
36  feet           Y    =         1454314
31  meter
 Z    =       16560265
18                 Z    =         5068442
57
 XDOT =     -13638
859680                 XDOT =       -4234
736094
 YDOT =      20251
691869  feet/sec       YDOT =        6125
793919  meter/sec
 ZDOT =       6008
284846                 ZDOT =        1810
942725

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12112580
05                 X    =        -3691914
40
 Y    =       -8486472
21  feet           Y    =        -2586676
73  meter
 Z    =       16656471
80                 Z    =         5076892
61
 XDOT =      18340
089793                 XDOT =        5590
059369
 YDOT =     -14538
562200  feet/sec       YDOT =       -4431
353759  meter/sec
 ZDOT =       5913
979835                 ZDOT =        1802
581054


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   20248
55152854  
00016717  00000-0  10270-3 0  9042
2 25544  51
6435 315
7203 0001575  85
6192 274
5138 15
49234332  4310


Satellite: ISS
Catalog Number: 25544
Epoch time:      20248
55152854   =   yrday
fracday
Element set:     904
Inclination:       51
6435  deg
RA of node:       315
7203  deg
Eccentricity:     
0001575     
Arg of perigee:    85
6192  deg
Mean anomaly:     274
5138  deg
Mean motion:   15
49234332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              296


Coasting Arc #6 (Orbit 445)
---------------------------------------

Vector Time (GMT): 2020/249/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4029655
67                 A    =         6792040
75  meter
 Y    =        1686167
55  meter          E    =           
0005246
 Z    =        5197217
66                 I    =           51
32863
 XDOT =      -4164
963068                 Wp   =          114
05192
 YDOT =       6325
452762  meter/sec      RA   =          310
48962  deg
 ZDOT =       1174
050245                 TA   =          324
61518
                                          MA   =          324
64998
                                          Ha   =            229
107  n
mi
                                          Hp   =            221
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13220655
07                 X    =         3985255
90
 Y    =        5532045
78  feet           Y    =         1730982
17  meter
 Z    =       17051239
03                 Z    =         5216684
13
 XDOT =     -13664
576994                 XDOT =       -4241
089482
 YDOT =      20752
797777  feet/sec       YDOT =        6278
451596  meter/sec
 ZDOT =       3851
870884                 ZDOT =        1153
633194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9138768
78                 X    =        -2785496
72
 Y    =      -10899777
38  feet           Y    =        -3322252
14  meter
 Z    =       17140938
18                 Z    =         5224557
96
 XDOT =      20853
297451                 XDOT =        6356
085063
 YDOT =     -11559
662091  feet/sec       YDOT =       -3523
385005  meter/sec
 ZDOT =       3757
417419                 ZDOT =        1145
260829


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   20249
51911981  
00016717  00000-0  10270-3 0  9054
2 25544  51
6436 310
9325 0001519  90
3533 269
7791 15
49243410  4467


Satellite: ISS
Catalog Number: 25544
Epoch time:      20249
51911981   =   yrday
fracday
Element set:     905
Inclination:       51
6436  deg
RA of node:       310
9325  deg
Eccentricity:     
0001519     
Arg of perigee:    90
3533  deg
Mean anomaly:     269
7791  deg
Mean motion:   15
49243410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             446
Checksum:              305


Coasting Arc #7 (Orbit 460)
---------------------------------------

Vector Time (GMT): 2020/250/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4116462
65                 A    =         6792111
62  meter
 Y    =       -1433495
55  meter          E    =           
0015797
 Z    =       -5222863
02                 I    =           51
30674
 XDOT =       3670
001868                 Wp   =           82
40753
 YDOT =      -6623
877127  meter/sec      RA   =          305
51955  deg
 ZDOT =      -1075
295327                 TA   =          177
21989
                                          MA   =          177
21110
                                          Ha   =            229
328  n
mi
                                          Hp   =            221
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13505454
90                 X    =        -4074757
23
 Y    =       -4703069
38  feet           Y    =        -1479295
93  meter
 Z    =      -17135377
35                 Z    =        -5242757
81
 XDOT =      12040
688543                 XDOT =        3749
022465
 YDOT =     -21731
880339  feet/sec       YDOT =       -6582
394774  meter/sec
 ZDOT =      -3527
871807                 ZDOT =       -1057
275527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9945332
96                 X    =         3031337
48
 Y    =       10122058
75  feet           Y    =         3085203
51  meter
 Z    =      -17227060
39                 Z    =        -5250808
01
 XDOT =     -19668
252598                 XDOT =       -5994
883392
 YDOT =      13466
833782  feet/sec       YDOT =        4104
690937  meter/sec
 ZDOT =      -3444
477249                 ZDOT =       -1049
876666


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   20250
48670955  
00016717  00000-0  10270-3 0  9066
2 25544  51
6430 306
1447 0001550  89
9248 270
2079 15
49200083  4617


Satellite: ISS
Catalog Number: 25544
Epoch time:      20250
48670955   =   yrday
fracday
Element set:     906
Inclination:       51
6430  deg
RA of node:       306
1447  deg
Eccentricity:     
0001550     
Arg of perigee:    89
9248  deg
Mean anomaly:     270
2079  deg
Mean motion:   15
49200083  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             461
Checksum:              297


Coasting Arc #8 (Orbit 476)
---------------------------------------

Vector Time (GMT): 2020/251/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4174807
62                 A    =         6791908
08  meter
 Y    =        1165879
17  meter          E    =           
0004998
 Z    =        5225154
18                 I    =           51
28807
 XDOT =      -3163
740278                 Wp   =          111
61293
 YDOT =       6911
004320  meter/sec      RA   =          300
54828  deg
 ZDOT =        983
164822                 TA   =          328
90982
                                          MA   =          328
93939
                                          Ha   =            229
136  n
mi
                                          Hp   =            221
761

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13696875
38                 X    =         4136079
22
 Y    =        3825062
88  feet           Y    =         1212348
58  meter
 Z    =       17142894
29                 Z    =         5245339
71
 XDOT =     -10379
725321                 XDOT =       -3245
561739
 YDOT =      22673
898687  feet/sec       YDOT =        6875
167668  meter/sec
 ZDOT =       3225
606371                 ZDOT =         967
597467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10664463
75                 X    =        -3250528
55
 Y    =       -9236142
93  feet           Y    =        -2815176
37  meter
 Z    =       17235927
67                 Z    =         5253510
75
 XDOT =      18380
993326                 XDOT =        5602
526766
 YDOT =     -15322
959222  feet/sec       YDOT =       -4670
437971  meter/sec
 ZDOT =       3153
523823                 ZDOT =         961
194061


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   20251
51880076  
00016717  00000-0  10270-3 0  9079
2 25544  51
6432 301
0378 0001627  90
6334 269
5002 15
49244768  4778


Satellite: ISS
Catalog Number: 25544
Epoch time:      20251
51880076   =   yrday
fracday
Element set:     907
Inclination:       51
6432  deg
RA of node:       301
0378  deg
Eccentricity:     
0001627     
Arg of perigee:    90
6334  deg
Mean anomaly:     269
5002  deg
Mean motion:   15
49244768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             477
Checksum:              301


Coasting Arc #9 (Orbit 491)
---------------------------------------

Vector Time (GMT): 2020/252/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4231163
12                 A    =         6791983
85  meter
 Y    =        -909989
41  meter          E    =           
0016133
 Z    =       -5248715
64                 I    =           51
27073
 XDOT =       2627
056991                 Wp   =           84
22459
 YDOT =      -7128
652077  meter/sec      RA   =          295
57585  deg
 ZDOT =       -882
598487                 TA   =          177
27323
                                          MA   =          177
26443
                                          Ha   =            229
382  n
mi
                                          Hp   =            221
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13881768
77                 X    =        -4195177
49
 Y    =       -2985529
57  feet           Y    =         -957104
29  meter
 Z    =      -17220195
68                 Z    =        -5269181
64
 XDOT =       8618
953381                 XDOT =        2710
863652
 YDOT =     -23387
966131  feet/sec       YDOT =       -7098
805883  meter/sec
 ZDOT =      -2895
664328                 ZDOT =        -869
633402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11333750
28                 X    =         3454527
09
 Y    =        8360927
27  feet           Y    =         2548410
63  meter
 Z    =      -17314532
34                 Z    =        -5277469
46
 XDOT =     -16849
083160                 XDOT =       -5135
600547
 YDOT =      16972
938091  feet/sec       YDOT =        5173
351530  meter/sec
 ZDOT =      -2835
586432                 ZDOT =        -864
286745


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   20252
48638776  
00016717  00000-0  10270-3 0  9085
2 25544  51
6421 296
2503 0001714  93
9497 266
1849 15
49203723  4929


Satellite: ISS
Catalog Number: 25544
Epoch time:      20252
48638776   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:       296
2503  deg
Eccentricity:     
0001714     
Arg of perigee:    93
9497  deg
Mean anomaly:     266
1849  deg
Mean motion:   15
49203723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             492
Checksum:              328


Coasting Arc #10 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2020/253/10:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2613954
13                 A    =         6803565
18  meter
 Y    =        6269742
60  meter          E    =           
0012877
 Z    =        -266683
61                 I    =           51
29713
 XDOT =      -4337
224178                 Wp   =          131
79822
 YDOT =      -2053
915109  meter/sec      RA   =          290
82942  deg
 ZDOT =      -5970
923164                 TA   =           51
08316
                                          MA   =           50
96842
                                          Ha   =            229
317  n
mi
                                          Hp   =            221
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8575964
99                 X    =        -2682574
60
 Y    =       20570021
65  feet           Y    =         6240127
81  meter
 Z    =        -874946
21                 Z    =         -279548
02
 XDOT =     -14229
738117                 XDOT =       -4284
930870
 YDOT =      -6738
566629  feet/sec       YDOT =       -2102
124786  meter/sec
 ZDOT =     -19589
642927                 ZDOT =       -5991
864743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19784222
55                 X    =         6030231
03
 Y    =      -10254253
76  feet           Y    =        -3125496
55  meter
 Z    =        -934513
30                 Z    =         -284839
65
 XDOT =       5721
771799                 XDOT =        1743
996044
 YDOT =      12778
755048  feet/sec       YDOT =        3894
964539  meter/sec
 ZDOT =     -19686
128325                 ZDOT =       -6000
331914


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   20253
45397139  
00016717  00000-0  10270-3 0  9099
2 25544  51
6425 291
4623 0001720  98
1838 261
9507 15
49231921  5078


Satellite: ISS
Catalog Number: 25544
Epoch time:      20253
45397139   =   yrday
fracday
Element set:     909
Inclination:       51
6425  deg
RA of node:       291
4623  deg
Eccentricity:     
0001720     
Arg of perigee:    98
1838  deg
Mean anomaly:     261
9507  deg
Mean motion:   15
49231921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              311


Coasting Arc #11 (Orbit 522)
---------------------------------------

Vector Time (GMT): 2020/254/10:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2111352
60                 A    =         6803654
32  meter
 Y    =       -6452660
87  meter          E    =           
0013992
 Z    =         334372
60                 I    =           51
28660
 XDOT =       4465
433156                 Wp   =           53
65247
 YDOT =       1778
894297  meter/sec      RA   =          285
85606  deg
 ZDOT =       5965
502907                 TA   =          309
96193
                                          MA   =          310
08474
                                          Ha   =            229
394  n
mi
                                          Hp   =            221
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6927009
85                 X    =         2181727
08
 Y    =      -21170147
20  feet           Y    =        -6428656
72  meter
 Z    =        1097022
96                 Z    =          344799
72
 XDOT =      14650
371246                 XDOT =        4416
232071
 YDOT =       5836
267377  feet/sec       YDOT =        1828
554906  meter/sec
 ZDOT =      19571
859930                 ZDOT =        5987
074776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18699920
43                 X    =        -5699735
75
 Y    =       12098066
63  feet           Y    =         3687490
71  meter
 Z    =        1145345
84                 Z    =          349101
41
 XDOT =      -6725
793024                 XDOT =       -2050
021714
 YDOT =     -12307
982500  feet/sec       YDOT =       -3751
473066  meter/sec
 ZDOT =      19671
267243                 ZDOT =        5995
802256


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   20254
48605920  
00016717  00000-0  10270-3 0  9105
2 25544  51
6429 286
3551 0001728  92
5875 267
5473 15
49196489  5233


Satellite: ISS
Catalog Number: 25544
Epoch time:      20254
48605920   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:       286
3551  deg
Eccentricity:     
0001728     
Arg of perigee:    92
5875  deg
Mean anomaly:     267
5473  deg
Mean motion:   15
49196489  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             523
Checksum:              332


Coasting Arc #12 (Orbit 528)
---------------------------------------

Vector Time (GMT): 2020/254/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3922518
31                 A    =         6792560
63  meter
 Y    =       -1769108
35  meter          E    =           
0015175
 Z    =       -5269066
79                 I    =           51
24491
 XDOT =       2338
001892                 Wp   =           95
04292
 YDOT =      -7249
573035  meter/sec      RA   =          283
68055  deg
 ZDOT =        693
990567                 TA   =          181
63600
                                          MA   =          181
64097
                                          Ha   =            229
334  n
mi
                                          Hp   =            222
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12869154
57                 X    =        -3876849
94
 Y    =       -5804161
24  feet           Y    =        -1812717
42  meter
 Z    =      -17286964
54                 Z    =        -5288009
95
 XDOT =       7670
609882                 XDOT =        2415
524018
 YDOT =     -23784
688435  feet/sec       YDOT =       -7222
994368  meter/sec
 ZDOT =       2276
871938                 ZDOT =         705
535982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -950481
22                 X    =         -289706
67
 Y    =      -13977642
05  feet           Y    =        -4260385
30  meter
 Z    =      -17374253
31                 Z    =        -5295672
41
 XDOT =      23546
167129                 XDOT =        7176
871741
 YDOT =      -4496
066693  feet/sec       YDOT =       -1370
401128  meter/sec
 ZDOT =       2330
374868                 ZDOT =         710
298260


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   20254
87309090  
00016717  00000-0  10270-3 0  9118
2 25544  51
6442 284
4423 0000611  87
3245 272
7975 15
48978810  5294


Satellite: ISS
Catalog Number: 25544
Epoch time:      20254
87309090   =   yrday
fracday
Element set:     911
Inclination:       51
6442  deg
RA of node:       284
4423  deg
Eccentricity:     
0000611     
Arg of perigee:    87
3245  deg
Mean anomaly:     272
7975  deg
Mean motion:   15
48978810  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             529
Checksum:              316


Coasting Arc #13 (Orbit 544)
---------------------------------------

Vector Time (GMT): 2020/255/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4053521
20                 A    =         6792466
36  meter
 Y    =        1423447
44  meter          E    =           
0003540
 Z    =        5258526
79                 I    =           51
23744
 XDOT =      -1705
476347                 Wp   =           66
61876
 YDOT =       7438
027080  meter/sec      RA   =          278
70838  deg
 ZDOT =       -697
006043                 TA   =           30
09036
                                          MA   =           30
07003
                                          Ha   =            229
102  n
mi
                                          Hp   =            222
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13298954
06                 X    =         4011759
66
 Y    =        4670103
15  feet           Y    =         1468543
31  meter
 Z    =       17252384
48                 Z    =         5278115
73
 XDOT =      -5595
394840                 XDOT =       -1785
138198
 YDOT =      24402
975985  feet/sec       YDOT =        7418
509805  meter/sec
 ZDOT =      -2286
765233                 ZDOT =        -705
484034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2390027
50                 X    =          728480
38
 Y    =       13778111
86  feet           Y    =         4199568
49  meter
 Z    =       17342670
35                 Z    =         5286045
92
 XDOT =     -23000
167455                 XDOT =       -7010
451040
 YDOT =       6924
853940  feet/sec       YDOT =        2110
695481  meter/sec
 ZDOT =      -2326
113317                 ZDOT =        -708
999339


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   20255
90535463  
00016717  00000-0  10270-3 0  9129
2 25544  51
6435 279
3369 0000511  89
2158 270
9051 15
49006501  5454


Satellite: ISS
Catalog Number: 25544
Epoch time:      20255
90535463   =   yrday
fracday
Element set:     912
Inclination:       51
6435  deg
RA of node:       279
3369  deg
Eccentricity:     
0000511     
Arg of perigee:    89
2158  deg
Mean anomaly:     270
9051  deg
Mean motion:   15
49006501  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             545
Checksum:              297


Coasting Arc #14 (Orbit 559)
---------------------------------------

Vector Time (GMT): 2020/256/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4169820
07                 A    =         6792536
27  meter
 Y    =       -1067254
44  meter          E    =           
0015077
 Z    =       -5267950
71                 I    =           51
23334
 XDOT =       1052
462301                 Wp   =           95
25047
 YDOT =      -7544
126792  meter/sec      RA   =          273
73574  deg
 ZDOT =        695
698892                 TA   =          181
44629
                                          MA   =          181
45066
                                          Ha   =            229
283  n
mi
                                          Hp   =            222
410

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13680512
05                 X    =        -4131987
27
 Y    =       -3501490
94  feet           Y    =        -1113672
84  meter
 Z    =      -17283302
86                 Z    =        -5288114
05
 XDOT =       3452
960304                 XDOT =        1133
365486
 YDOT =     -24751
072152  feet/sec       YDOT =       -7531
905043  meter/sec
 ZDOT =       2282
476681                 ZDOT =         701
007845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3827862
58                 X    =        -1166732
51
 Y    =      -13473773
53  feet           Y    =        -4106806
17  meter
 Z    =      -17376256
83                 Z    =        -5296283
08
 XDOT =      22114
961640                 XDOT =        6740
640308
 YDOT =      -9256
656284  feet/sec       YDOT =       -2821
428835  meter/sec
 ZDOT =       2307
194381                 ZDOT =         703
232847


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   20256
87310286  
00016717  00000-0  10270-3 0  9131
2 25544  51
6433 274
5506 0000504  90
8916 269
2292 15
48986081  5608


Satellite: ISS
Catalog Number: 25544
Epoch time:      20256
87310286   =   yrday
fracday
Element set:     913
Inclination:       51
6433  deg
RA of node:       274
5506  deg
Eccentricity:     
0000504     
Arg of perigee:    90
8916  deg
Mean anomaly:     269
2292  deg
Mean motion:   15
48986081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             560
Checksum:              313


Coasting Arc #15 (Orbit 575)
---------------------------------------

Vector Time (GMT): 2020/257/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4238709
10                 A    =         6792457
02  meter
 Y    =         706335
75  meter          E    =           
0003385
 Z    =        5257836
76                 I    =           51
23272
 XDOT =       -398
380382                 Wp   =           66
78568
 YDOT =       7620
194112  meter/sec      RA   =          268
76259  deg
 ZDOT =       -700
859200                 TA   =           29
96069
                                          MA   =           29
94133
                                          Ha   =            229
041  n
mi
                                          Hp   =            222
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13906525
93                 X    =         4204956
29
 Y    =        2317374
50  feet           Y    =          753547
41  meter
 Z    =       17250120
60                 Z    =         5278344
57
 XDOT =      -1307
022251                 XDOT =        -480
157733
 YDOT =      25000
636852  feet/sec       YDOT =        7615
281877  meter/sec
 ZDOT =      -2299
406825                 ZDOT =        -702
993132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5188190
81                 X    =         1581360
56
 Y    =       12983568
61  feet           Y    =         3957391
71  meter
 Z    =       17344681
35                 Z    =         5286658
87
 XDOT =     -21080
750688                 XDOT =       -6425
412810
 YDOT =      11516
285265  feet/sec       YDOT =        3510
163749  meter/sec
 ZDOT =      -2309
461187                 ZDOT =        -703
923770


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   20257
90536292  
00016717  00000-0  10270-3 0  9144
2 25544  51
6437 269
4449 0000378  97
3959 262
7234 15
49008888  5761


Satellite: ISS
Catalog Number: 25544
Epoch time:      20257
90536292   =   yrday
fracday
Element set:     914
Inclination:       51
6437  deg
RA of node:       269
4449  deg
Eccentricity:     
0000378     
Arg of perigee:    97
3959  deg
Mean anomaly:     262
7234  deg
Mean motion:   15
49008888  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             576
Checksum:              349


Coasting Arc #16 (Orbit 590)
---------------------------------------

Vector Time (GMT): 2020/258/20:35:45
072
Vector Time (MET): N/A
Weight (LBS)     : 922309
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4291655
90                 A    =         6792506
83  meter
 Y    =        -339151
10  meter          E    =           
0015015
 Z    =       -5267201
89                 I    =           51
23417
 XDOT =       -260
632491                 Wp   =           95
09569
 YDOT =      -7612
126798  meter/sec      RA   =          263
78879  deg
 ZDOT =        702
932480                 TA   =          181
67059
                                          MA   =          181
67561
                                          Ha   =            229
247  n
mi
                                          Hp   =            222
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14080235
89                 X    =        -4261959
67
 Y    =       -1112700
46  feet           Y    =         -386977
65  meter
 Z    =      -17280846
10                 Z    =        -5287976
71
 XDOT =       -855
093473                 XDOT =        -178
906436
 YDOT =     -24974
169286  feet/sec       YDOT =       -7614
584388  meter/sec
 ZDOT =       2306
208923                 ZDOT =         701
865265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6521636
86                 X    =        -1987794
91
 Y    =      -12395116
92  feet           Y    =        -3778031
64  meter
 Z    =      -17376654
35                 Z    =        -5296404
25
 XDOT =      19737
754943                 XDOT =        6016
067707
 YDOT =     -13609
377487  feet/sec       YDOT =       -4148
138258  meter/sec
 ZDOT =       2301
473481                 ZDOT =         701
489117


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   20258
87310559  
00016717  00000-0  10270-3 0  9158
2 25544  51
6432 264
6577 0000450  82
6378 277
4823 15
48995854  5919


Satellite: ISS
Catalog Number: 25544
Epoch time:      20258
87310559   =   yrday
fracday
Element set:     915
Inclination:       51
6432  deg
RA of node:       264
6577  deg
Eccentricity:     
0000450     
Arg of perigee:    82
6378  deg
Mean anomaly:     277
4823  deg
Mean motion:   15
48995854  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             591
Checksum:              341
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