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

 
Date: September 16th 2020

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ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13864 993 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


263/20:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 7

267/16:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 7

270/23:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 5

Coasting Arc #1 (Orbit 585)
---------------------------------------

Vector Time (GMT): 2020/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4026159
91                 A    =         6793037
81  meter
 Y    =       -1783332
52  meter          E    =           
0004911
 Z    =        5169327
01                 I    =           51
23196
 XDOT =       1608
733241                 Wp   =          120
45757
 YDOT =       7380
283730  meter/sec      RA   =          265
58475  deg
 ZDOT =       1289
738385                 TA   =          317
05682
                                          MA   =          317
09515
                                          Ha   =            229
283  n
mi
                                          Hp   =            222
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13209186
07                 X    =         4020693
07
 Y    =       -5850828
49  feet           Y    =        -1738339
51  meter
 Z    =       16959734
27                 Z    =         5188871
09
 XDOT =       5277
996199                 XDOT =        1519
820380
 YDOT =      24213
529297  feet/sec       YDOT =        7397
776638  meter/sec
 ZDOT =       4231
425147                 ZDOT =        1297
336696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13706801
92                 X    =        -4177833
23
 Y    =        4215592
64  feet           Y    =         1284912
64  meter
 Z    =       17049918
97                 Z    =         5196815
30
 XDOT =      -1960
128442                 XDOT =        -597
447149
 YDOT =     -23672
621465  feet/sec       YDOT =       -7215
415023  meter/sec
 ZDOT =       4266
278895                 ZDOT =        1300
361807


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
55064888  
00016717  00000-0  10270-3 0  9008
2 25544  51
6408 266
2511 0000738  96
5164 263
6070 15
48946414  5867


Satellite: ISS
Catalog Number: 25544
Epoch time:      20258
55064888   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       266
2511  deg
Eccentricity:     
0000738     
Arg of perigee:    96
5164  deg
Mean anomaly:     263
6070  deg
Mean motion:   15
48946414  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             586
Checksum:              319


Coasting Arc #2 (Orbit 600)
---------------------------------------

Vector Time (GMT): 2020/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3862604
60                 A    =         6793096
10  meter
 Y    =        2131431
06  meter          E    =           
0014646
 Z    =       -5178655
22                 I    =           51
23500
 XDOT =      -2241
401991                 Wp   =           80
93115
 YDOT =      -7198
166384  meter/sec      RA   =          260
61232  deg
 ZDOT =      -1291
709515                 TA   =          176
56544
                                          MA   =          176
55537
                                          Ha   =            229
449  n
mi
                                          Hp   =            222
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12672587
26                 X    =        -3860997
15
 Y    =        6992884
05  feet           Y    =         2088245
32  meter
 Z    =      -16990338
66                 Z    =        -5197414
26
 XDOT =      -7353
681074                 XDOT =       -2154
469025
 YDOT =     -23616
031445  feet/sec       YDOT =       -7222
745351  meter/sec
 ZDOT =      -4237
892108                 ZDOT =       -1302
385682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13217661
83                 X    =         4028743
33
 Y    =       -5642617
10  feet           Y    =        -1719869
69  meter
 Z    =      -17076908
11                 Z    =        -5205041
59
 XDOT =       4406
765581                 XDOT =        1343
182149
 YDOT =      23288
159010  feet/sec       YDOT =        7098
230866  meter/sec
 ZDOT =      -4286
973041                 ZDOT =       -1306
669383


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   20259
51840992  
00016717  00000-0  10270-3 0  9014
2 25544  51
6400 261
4650 0000734  96
9818 263
1415 15
48932305  6016


Satellite: ISS
Catalog Number: 25544
Epoch time:      20259
51840992   =   yrday
fracday
Element set:     901
Inclination:       51
6400  deg
RA of node:       261
4650  deg
Eccentricity:     
0000734     
Arg of perigee:    96
9818  deg
Mean anomaly:     263
1415  deg
Mean motion:   15
48932305  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             601
Checksum:              294


Coasting Arc #3 (Orbit 616)
---------------------------------------

Vector Time (GMT): 2020/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3650969
26                 A    =         6793097
87  meter
 Y    =       -2466432
85  meter          E    =           
0004859
 Z    =        5167278
82                 I    =           51
24023
 XDOT =       2868
781022                 Wp   =          120
87021
 YDOT =       6984
922619  meter/sec      RA   =          255
63928  deg
 ZDOT =       1303
706377                 TA   =          316
50831
                                          MA   =          316
54662
                                          Ha   =            229
281  n
mi
                                          Hp   =            222
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11978245
59                 X    =         3653178
82
 Y    =       -8091971
30  feet           Y    =        -2425592
31  meter
 Z    =       16953014
51                 Z    =         5185019
23
 XDOT =       9412
011226                 XDOT =        2784
127694
 YDOT =      22916
412793  feet/sec       YDOT =        7016
530167  meter/sec
 ZDOT =       4277
251892                 ZDOT =        1317
435487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12523183
21                 X    =        -3817066
24
 Y    =        7024638
48  feet           Y    =         2141109
81  meter
 Z    =       17034887
86                 Z    =         5192233
82
 XDOT =      -6833
676592                 XDOT =       -2082
904625
 YDOT =     -22735
067614  feet/sec       YDOT =       -6929
648609  meter/sec
 ZDOT =       4340
444626                 ZDOT =        1322
967522


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   20260
55068883  
00016717  00000-0  10270-3 0  9022
2 25544  51
6385 256
3586 0000638  94
2370 265
8853 15
48932908  6177


Satellite: ISS
Catalog Number: 25544
Epoch time:      20260
55068883   =   yrday
fracday
Element set:     902
Inclination:       51
6385  deg
RA of node:       256
3586  deg
Eccentricity:     
0000638     
Arg of perigee:    94
2370  deg
Mean anomaly:     265
8853  deg
Mean motion:   15
48932908  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             617
Checksum:              333


Coasting Arc #4 (Orbit 631)
---------------------------------------

Vector Time (GMT): 2020/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3427640
45                 A    =         6793108
20  meter
 Y    =        2780528
30  meter          E    =           
0014582
 Z    =       -5176938
93                 I    =           51
25041
 XDOT =      -3459
973910                 Wp   =           80
78402
 YDOT =      -6695
458993  meter/sec      RA   =          250
66705  deg
 ZDOT =      -1306
159661                 TA   =          176
57314
                                          MA   =          176
56314
                                          Ha   =            229
432  n
mi
                                          Hp   =            222
450

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11245539
52                 X    =        -3433331
87
 Y    =        9122468
17  feet           Y    =         2742165
62  meter
 Z    =      -16984707
76                 Z    =        -5193603
11
 XDOT =     -11351
620438                 XDOT =       -3378
501563
 YDOT =     -21966
728980  feet/sec       YDOT =       -6733
695492  meter/sec
 ZDOT =      -4285
300726                 ZDOT =       -1322
768254

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11741695
95                 X    =         3578868
93
 Y    =       -8318394
46  feet           Y    =        -2535446
63  meter
 Z    =      -17061616
92                 Z    =        -5200380
84
 XDOT =       9146
387720                 XDOT =        2787
818977
 YDOT =      21850
926904  feet/sec       YDOT =        6660
162520  meter/sec
 ZDOT =      -4361
803271                 ZDOT =       -1329
477637


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   20261
51844988  
00016717  00000-0  10270-3 0  9038
2 25544  51
6390 251
5718 0000698  96
2361 263
8868 15
48935069  6327


Satellite: ISS
Catalog Number: 25544
Epoch time:      20261
51844988   =   yrday
fracday
Element set:     903
Inclination:       51
6390  deg
RA of node:       251
5718  deg
Eccentricity:     
0000698     
Arg of perigee:    96
2361  deg
Mean anomaly:     263
8868  deg
Mean motion:   15
48935069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             632
Checksum:              339


Coasting Arc #5 (Orbit 647)
---------------------------------------

Vector Time (GMT): 2020/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3160069
01                 A    =         6793106
84  meter
 Y    =       -3072023
95  meter          E    =           
0004867
 Z    =        5166259
36                 I    =           51
26323
 XDOT =       4039
631876                 Wp   =          120
53947
 YDOT =       6376
847343  meter/sec      RA   =          245
69539  deg
 ZDOT =       1317
578525                 TA   =          316
70694
                                          MA   =          316
74517
                                          Ha   =            229
287  n
mi
                                          Hp   =            222
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10367680
47                 X    =         3169091
63
 Y    =      -10078818
73  feet           Y    =        -3036634
81  meter
 Z    =       16949669
81                 Z    =         5181632
01
 XDOT =      13253
385420                 XDOT =        3961
623753
 YDOT =      20921
415166  feet/sec       YDOT =        6421
585367  meter/sec
 ZDOT =       4322
764188                 ZDOT =        1337
011406

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10771182
33                 X    =        -3283056
37
 Y    =        9520650
62  feet           Y    =         2901894
31  meter
 Z    =       17020620
87                 Z    =         5187885
24
 XDOT =     -11402
051800                 XDOT =       -3475
345389
 YDOT =     -20807
489184  feet/sec       YDOT =       -6342
122703  meter/sec
 ZDOT =       4412
318226                 ZDOT =        1344
874595


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   20262
55072710  
00016717  00000-0  10270-3 0  9040
2 25544  51
6395 246
4654 0000624  88
8655 271
2566 15
48936346  6480


Satellite: ISS
Catalog Number: 25544
Epoch time:      20262
55072710   =   yrday
fracday
Element set:     904
Inclination:       51
6395  deg
RA of node:       246
4654  deg
Eccentricity:     
0000624     
Arg of perigee:    88
8655  deg
Mean anomaly:     271
2566  deg
Mean motion:   15
48936346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             648
Checksum:              324


Coasting Arc #6 (Orbit 662)
---------------------------------------

Vector Time (GMT): 2020/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2885031
49                 A    =         6793116
01  meter
 Y    =        3340946
20  meter          E    =           
0014561
 Z    =       -5176426
91                 I    =           51
27845
 XDOT =      -4570
509544                 Wp   =           80
25737
 YDOT =      -5989
711692  meter/sec      RA   =          240
72481  deg
 ZDOT =      -1319
297084                 TA   =          176
97495
                                          MA   =          176
96614
                                          Ha   =            229
423  n
mi
                                          Hp   =            222
467

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9465326
41                 X    =        -2897032
20
 Y    =       10961109
56  feet           Y    =         3308616
13  meter
 Z    =      -16983027
93                 Z    =        -5190470
84
 XDOT =     -14995
110053                 XDOT =       -4496
782649
 YDOT =     -19651
285078  feet/sec       YDOT =       -6040
410294  meter/sec
 ZDOT =      -4328
402505                 ZDOT =       -1341
319395

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9735428
35                 X    =         2967358
56
 Y    =      -10618559
83  feet           Y    =        -3236537
04  meter
 Z    =      -17047849
92                 Z    =        -5196184
65
 XDOT =      13477
633862                 XDOT =        4107
982801
 YDOT =      19464
794867  feet/sec       YDOT =        5932
869475  meter/sec
 ZDOT =      -4429
922449                 ZDOT =       -1350
240362


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   20263
51848619  
00016717  00000-0  10270-3 0  9057
2 25544  51
6396 241
6785 0000684  86
5270 273
5958 15
48938654  6638


Satellite: ISS
Catalog Number: 25544
Epoch time:      20263
51848619   =   yrday
fracday
Element set:     905
Inclination:       51
6396  deg
RA of node:       241
6785  deg
Eccentricity:     
0000684     
Arg of perigee:    86
5270  deg
Mean anomaly:     273
5958  deg
Mean motion:   15
48938654  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             663
Checksum:              349


Coasting Arc #7 (Orbit 668)
---------------------------------------

Vector Time (GMT): 2020/263/20:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          38656
46                 A    =         6798692
83  meter
 Y    =       -5695413
81  meter          E    =           
0012131
 Z    =        3702811
76                 I    =           51
30460
 XDOT =       5695
082827                 Wp   =           94
27064
 YDOT =       2827
656818  meter/sec      RA   =          239
00550  deg
 ZDOT =       4276
804558                 TA   =          310
02545
                                          MA   =          310
13184
                                          Ha   =            229
325  n
mi
                                          Hp   =            222
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         126825
66                 X    =           84355
10
 Y    =      -18685740
84  feet           Y    =        -5694725
69  meter
 Z    =       12148332
54                 Z    =         3703111
02
 XDOT =      18684
654945                 XDOT =        5642
265368
 YDOT =       9277
089299  feet/sec       YDOT =        2891
048361  meter/sec
 ZDOT =      14031
511017                 ZDOT =        4304
340787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15530251
51                 X    =         4733620
66
 Y    =      -10389862
66  feet           Y    =        -3166830
14  meter
 Z    =       12149774
51                 Z    =         3703251
27
 XDOT =       1915
369338                 XDOT =         583
804574
 YDOT =      19469
839587  feet/sec       YDOT =        5934
407106  meter/sec
 ZDOT =      14158
506450                 ZDOT =        4315
512766


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   20263
90558965  
00016717  00000-0  10270-3 0  9063
2 25544  51
6414 239
7642 0000477  64
1557 295
9642 15
48933379  6692


Satellite: ISS
Catalog Number: 25544
Epoch time:      20263
90558965   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       239
7642  deg
Eccentricity:     
0000477     
Arg of perigee:    64
1557  deg
Mean anomaly:     295
9642  deg
Mean motion:   15
48933379  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             669
Checksum:              349


Coasting Arc #8 (Orbit 683)
---------------------------------------

Vector Time (GMT): 2020/264/20:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         448990
48                 A    =         6798643
77  meter
 Y    =        5681027
32  meter          E    =           
0006010
 Z    =       -3713682
02                 I    =           51
32230
 XDOT =      -5910
060736                 Wp   =           79
32542
 YDOT =      -2322
330308  meter/sec      RA   =          234
03695  deg
 ZDOT =      -4271
963855                 TA   =          145
05003
                                          MA   =          145
01056
                                          Ha   =            229
279  n
mi
                                          Hp   =            222
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1473065
89                 X    =          403469
32
 Y    =       18638541
08  feet           Y    =         5685793
50  meter
 Z    =      -12183996
12                 Z    =        -3711611
88
 XDOT =     -19389
963044                 XDOT =       -5862
901480
 YDOT =      -7619
193924  feet/sec       YDOT =       -2388
157422  meter/sec
 ZDOT =     -14015
629446                 ZDOT =       -4300
558279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14394970
96                 X    =        -4387587
15
 Y    =       11940740
10  feet           Y    =         3639537
58  meter
 Z    =      -12174499
37                 Z    =        -3710787
41
 XDOT =      -3919
567559                 XDOT =       -1194
684192
 YDOT =     -19133
493483  feet/sec       YDOT =       -5831
888814  meter/sec
 ZDOT =     -14147
525019                 ZDOT =       -4312
165626


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   20264
87334868  
00016717  00000-0  10270-3 0  9075
2 25544  51
6407 234
9777 0000323  77
2954 282
8232 15
48944910  6846


Satellite: ISS
Catalog Number: 25544
Epoch time:      20264
87334868   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       234
9777  deg
Eccentricity:     
0000323     
Arg of perigee:    77
2954  deg
Mean anomaly:     282
8232  deg
Mean motion:   15
48944910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             684
Checksum:              335


Coasting Arc #9 (Orbit 699)
---------------------------------------

Vector Time (GMT): 2020/265/20:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -959029
64                 A    =         6798681
47  meter
 Y    =       -5618740
09  meter          E    =           
0011966
 Z    =        3696186
20                 I    =           51
34375
 XDOT =       6092
802455                 Wp   =           94
74138
 YDOT =       1789
832562  meter/sec      RA   =          229
06896  deg
 ZDOT =       4288
663902                 TA   =          309
42329
                                          MA   =          309
52915
                                          Ha   =            229
238  n
mi
                                          Hp   =            222
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3146422
71                 X    =         -914082
09
 Y    =      -18434186
65  feet           Y    =        -5629213
19  meter
 Z    =       12126595
15                 Z    =         3691636
94
 XDOT =      19989
509367                 XDOT =        6051
503058
 YDOT =       5872
154076  feet/sec       YDOT =        1857
735888  meter/sec
 ZDOT =      14070
419627                 ZDOT =        4318
160319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13041204
02                 X    =         3974958
99
 Y    =      -13422135
21  feet           Y    =        -4091066
81  meter
 Z    =       12105651
88                 Z    =         3689802
69
 XDOT =       5924
620103                 XDOT =        1805
824207
 YDOT =      18608
115321  feet/sec       YDOT =        5671
753550  meter/sec
 ZDOT =      14206
497421                 ZDOT =        4330
140414


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   20265
90562481  
00016717  00000-0  10270-3 0  9085
2 25544  51
6411 229
8712 0000236  67
9820 292
1355 15
48951666  7009


Satellite: ISS
Catalog Number: 25544
Epoch time:      20265
90562481   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:       229
8712  deg
Eccentricity:     
0000236     
Arg of perigee:    67
9820  deg
Mean anomaly:     292
1355  deg
Mean motion:   15
48951666  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             700
Checksum:              308


Coasting Arc #10 (Orbit 714)
---------------------------------------

Vector Time (GMT): 2020/266/20:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1436099
39                 A    =         6798643
52  meter
 Y    =        5518792
43  meter          E    =           
0006097
 Z    =       -3707835
83                 I    =           51
36560
 XDOT =      -6216
369142                 Wp   =           79
64995
 YDOT =      -1256
920469  meter/sec      RA   =          224
10255  deg
 ZDOT =      -4283
469182                 TA   =          144
60331
                                          MA   =          144
56283
                                          Ha   =            229
310  n
mi
                                          Hp   =            222
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4711612
16                 X    =         1392290
56
 Y    =       18106274
36  feet           Y    =         5534606
89  meter
 Z    =      -12164815
71                 Z    =        -3700966
27
 XDOT =     -20394
911884                 XDOT =       -6181
045033
 YDOT =      -4123
754818  feet/sec       YDOT =       -1326
238939  meter/sec
 ZDOT =     -14053
376583                 ZDOT =       -4313
580321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11606739
51                 X    =        -3537734
20
 Y    =       14699977
44  feet           Y    =         4480553
12  meter
 Z    =      -12133155
52                 Z    =        -3698185
80
 XDOT =      -7808
830359                 XDOT =       -2380
131494
 YDOT =     -17866
328440  feet/sec       YDOT =       -5445
656909  meter/sec
 ZDOT =     -14192
313791                 ZDOT =       -4325
817244


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   20266
87338259  
00016717  00000-0  10270-3 0  9097
2 25544  51
6399 225
0840 0000455  76
5686 283
5515 15
48958408  7152


Satellite: ISS
Catalog Number: 25544
Epoch time:      20266
87338259   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       225
0840  deg
Eccentricity:     
0000455     
Arg of perigee:    76
5686  deg
Mean anomaly:     283
5515  deg
Mean motion:   15
48958408  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             715
Checksum:              343


Coasting Arc #11 (Orbit 727)
---------------------------------------

Vector Time (GMT): 2020/267/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1930195
09                 A    =         6798900
00  meter
 Y    =        5410422
25  meter          E    =           
0005809
 Z    =       -3642636
01                 I    =           51
39051
 XDOT =      -6253
395772                 Wp   =           81
67194
 YDOT =       -698
784424  meter/sec      RA   =          219
94279  deg
 ZDOT =      -4356
677130                 TA   =          141
58923
                                          MA   =          141
54786
                                          Ha   =            229
315  n
mi
                                          Hp   =            222
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6332661
04                 X    =         1887244
61
 Y    =       17750729
17  feet           Y    =         5431766
88  meter
 Z    =      -11950905
55                 Z    =        -3633364
21
 XDOT =     -20516
390327                 XDOT =       -6223
954617
 YDOT =      -2292
599816  feet/sec       YDOT =        -768
549816  meter/sec
 ZDOT =     -14293
560137                 ZDOT =       -4386
982341

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18872665
27                 X    =        -5752388
37
 Y    =        -183388
34  feet           Y    =          -55896
77  meter
 Z    =      -11908148
47                 Z    =        -3629603
65
 XDOT =       9261
162116                 XDOT =        2822
802213
 YDOT =     -16958
005959  feet/sec       YDOT =       -5168
800216  meter/sec
 ZDOT =     -14433
413847                 ZDOT =       -4399
304540


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   20267
71210671  
00016717  00000-0  10270-3 0  9100
2 25544  51
6432 220
9385 0000395  75
2832 284
8362 15
48942873  7287


Satellite: ISS
Catalog Number: 25544
Epoch time:      20267
71210671   =   yrday
fracday
Element set:     910
Inclination:       51
6432  deg
RA of node:       220
9385  deg
Eccentricity:     
0000395     
Arg of perigee:    75
2832  deg
Mean anomaly:     284
8362  deg
Mean motion:   15
48942873  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             728
Checksum:              311


Coasting Arc #12 (Orbit 743)
---------------------------------------

Vector Time (GMT): 2020/268/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2409899
01                 A    =         6798980
09  meter
 Y    =       -5215784
74  meter          E    =           
0012446
 Z    =        3624905
65                 I    =           51
41686
 XDOT =       6290
536174                 Wp   =           92
95021
 YDOT =        142
705222  meter/sec      RA   =          214
98017  deg
 ZDOT =       4373
728226                 TA   =          310
09607
                                          MA   =          310
20511
                                          Ha   =            229
397  n
mi
                                          Hp   =            222
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7906492
83                 X    =        -2369003
18
 Y    =      -17112154
64  feet           Y    =        -5242505
24  meter
 Z    =       11892735
06                 Z    =         3613298
67
 XDOT =      20638
242042                 XDOT =        6267
227767
 YDOT =        468
192986  feet/sec       YDOT =         212
920236  meter/sec
 ZDOT =      14349
502053                 ZDOT =        4404
228630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18794491
42                 X    =         5728560
99
 Y    =       -1837504
44  feet           Y    =         -560071
35  meter
 Z    =       11839184
18                 Z    =         3608583
34
 XDOT =      -7411
799097                 XDOT =       -2259
116365
 YDOT =      17842
233807  feet/sec       YDOT =        5438
312864  meter/sec
 ZDOT =      14490
280623                 ZDOT =        4416
637534


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   20268
74438233  
00016717  00000-0  10270-3 0  9111
2 25544  51
6427 215
8327 0000525  72
0734 288
0473 15
48935103  7446


Satellite: ISS
Catalog Number: 25544
Epoch time:      20268
74438233   =   yrday
fracday
Element set:     911
Inclination:       51
6427  deg
RA of node:       215
8327  deg
Eccentricity:     
0000525     
Arg of perigee:    72
0734  deg
Mean anomaly:     288
0473  deg
Mean motion:   15
48935103  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             744
Checksum:              301


Coasting Arc #13 (Orbit 758)
---------------------------------------

Vector Time (GMT): 2020/269/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2847725
17                 A    =         6798936
23  meter
 Y    =        4993004
82  meter          E    =           
0005638
 Z    =       -3636811
01                 I    =           51
44555
 XDOT =      -6271
203334                 Wp   =           82
14812
 YDOT =        398
059152  meter/sec      RA   =          210
01973  deg
 ZDOT =      -4369
112422                 TA   =          140
98636
                                          MA   =          140
94567
                                          Ha   =            229
272  n
mi
                                          Hp   =            222
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9342930
33                 X    =         2809345
75
 Y    =       16381249
42  feet           Y    =         5024635
46  meter
 Z    =      -11931794
66                 Z    =        -3623071
22
 XDOT =     -20574
814087                 XDOT =       -6253
965849
 YDOT =       1305
968347  feet/sec       YDOT =         328
026350  meter/sec
 ZDOT =     -14334
358340                 ZDOT =       -4399
533563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18521536
27                 X    =        -5645364
26
 Y    =        3754682
32  feet           Y    =         1144427
17  meter
 Z    =      -11868380
62                 Z    =        -3617482
41
 XDOT =       5517
056511                 XDOT =        1681
598825
 YDOT =     -18485
994119  feet/sec       YDOT =       -5634
531007  meter/sec
 ZDOT =     -14474
793306                 ZDOT =       -4411
917000


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   20269
71213799  
00016717  00000-0  10270-3 0  9128
2 25544  51
6431 211
0463 0000263  72
8669 287
2510 15
48943066  7590


Satellite: ISS
Catalog Number: 25544
Epoch time:      20269
71213799   =   yrday
fracday
Element set:     912
Inclination:       51
6431  deg
RA of node:       211
0463  deg
Eccentricity:     
0000263     
Arg of perigee:    72
8669  deg
Mean anomaly:     287
2510  deg
Mean motion:   15
48943066  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             759
Checksum:              312


Coasting Arc #14 (Orbit 774)
---------------------------------------

Vector Time (GMT): 2020/270/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3285101
06                 A    =         6798995
72  meter
 Y    =       -4717580
84  meter          E    =           
0012367
 Z    =        3620019
28                 I    =           51
47573
 XDOT =       6211
667871                 Wp   =           92
40580
 YDOT =       -949
847781  meter/sec      RA   =          205
06036  deg
 ZDOT =       4385
632573                 TA   =          310
52470
                                          MA   =          310
63236
                                          Ha   =            229
369  n
mi
                                          Hp   =            222
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10777890
61                 X    =        -3249687
41
 Y    =      -15477627
44  feet           Y    =        -4754119
06  meter
 Z    =       11876703
67                 Z    =         3604147
79
 XDOT =      20379
487767                 XDOT =        6200
524879
 YDOT =      -3116
298493  feet/sec       YDOT =        -880
446604  meter/sec
 ZDOT =      14388
558311                 ZDOT =        4415
779277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18022873
09                 X    =         5493371
72
 Y    =       -5712360
70  feet           Y    =        -1741127
54  meter
 Z    =       11803429
50                 Z    =         3597685
31
 XDOT =      -3532
230516                 XDOT =       -1076
623861
 YDOT =      18966
347915  feet/sec       YDOT =        5780
942844  meter/sec
 ZDOT =      14527
745790                 ZDOT =        4428
056917


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   20270
74441074  
00016717  00000-0  10270-3 0  9133
2 25544  51
6432 205
9398 0000471  57
5909 302
5287 15
48941066  7756


Satellite: ISS
Catalog Number: 25544
Epoch time:      20270
74441074   =   yrday
fracday
Element set:     913
Inclination:       51
6432  deg
RA of node:       205
9398  deg
Eccentricity:     
0000471     
Arg of perigee:    57
5909  deg
Mean anomaly:     302
5287  deg
Mean motion:   15
48941066  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             775
Checksum:              313


Coasting Arc #15 (Orbit 778)
---------------------------------------

Vector Time (GMT): 2020/270/23:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4598970
31                 A    =         6795367
55  meter
 Y    =        1993324
85  meter          E    =           
0010849
 Z    =       -4599155
23                 I    =           51
47285
 XDOT =      -5106
365977                 Wp   =          111
47609
 YDOT =      -4835
678149  meter/sec      RA   =          203
50098  deg
 ZDOT =       3012
189731                 TA   =          188
73134
                                          MA   =          188
75023
                                          Ha   =            229
310  n
mi
                                          Hp   =            222
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15088485
26                 X    =        -4598578
49
 Y    =        6539779
69  feet           Y    =         1941897
87  meter
 Z    =      -15089091
95                 Z    =        -4621494
26
 XDOT =     -16753
169217                 XDOT =       -5066
543888
 YDOT =     -15865
085792  feet/sec       YDOT =       -4892
558410  meter/sec
 ZDOT =       9882
512241                 ZDOT =        2987
482029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14706452
70                 X    =        -4482526
78
 Y    =        7143390
04  feet           Y    =         2177305
28  meter
 Z    =      -15192235
82                 Z    =        -4630593
48
 XDOT =     -16931
054823                 XDOT =       -5160
585510
 YDOT =     -14094
674407  feet/sec       YDOT =       -4296
056759  meter/sec
 ZDOT =       9768
434146                 ZDOT =        2977
418728


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   20271
00247898  
00016717  00000-0  10270-3 0  9142
2 25544  51
6425 204
6593 0000640 129
5278 230
5929 15
48964758  7798


Satellite: ISS
Catalog Number: 25544
Epoch time:      20271
00247898   =   yrday
fracday
Element set:     914
Inclination:       51
6425  deg
RA of node:       204
6593  deg
Eccentricity:     
0000640     
Arg of perigee:   129
5278  deg
Mean anomaly:     230
5929  deg
Mean motion:   15
48964758  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             779
Checksum:              334


Coasting Arc #16 (Orbit 794)
---------------------------------------

Vector Time (GMT): 2020/271/23:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4404643
44                 A    =         6795459
93  meter
 Y    =       -2374533
69  meter          E    =           
0008762
 Z    =        4592052
19                 I    =           51
50421
 XDOT =       5515
614554                 Wp   =           70
23725
 YDOT =       4381
447499  meter/sec      RA   =          198
54508  deg
 ZDOT =      -3017
279263                 TA   =           50
00551
                                          MA   =           49
92862
                                          Ha   =            229
290  n
mi
                                          Hp   =            222
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14450929
91                 X    =         4408563
35
 Y    =       -7790464
85  feet           Y    =        -2325255
61  meter
 Z    =       15065788
04                 Z    =         4613457
81
 XDOT =      18095
848275                 XDOT =        5480
866117
 YDOT =      14374
827754  feet/sec       YDOT =        4442
932583  meter/sec
 ZDOT =      -9899
210182                 ZDOT =       -2990
571337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13872707
19                 X    =         4228401
15
 Y    =       -8607011
57  feet           Y    =        -2623417
13  meter
 Z    =       15164631
03                 Z    =         4622179
54
 XDOT =      18336
909500                 XDOT =        5589
090016
 YDOT =      12287
565958  feet/sec       YDOT =        3745
250104  meter/sec
 ZDOT =      -9775
873293                 ZDOT =       -2979
686180


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   20272
03475207  
00016717  00000-0  10270-3 0  9154
2 25544  51
6424 199
5534 0000752 126
9564 233
1655 15
48933497  7956


Satellite: ISS
Catalog Number: 25544
Epoch time:      20272
03475207   =   yrday
fracday
Element set:     915
Inclination:       51
6424  deg
RA of node:       199
5534  deg
Eccentricity:     
0000752     
Arg of perigee:   126
9564  deg
Mean anomaly:     233
1655  deg
Mean motion:   15
48933497  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             795
Checksum:              324


Coasting Arc #17 (Orbit 809)
---------------------------------------

Vector Time (GMT): 2020/272/23:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4175009
94                 A    =         6795315
41  meter
 Y    =        2757244
68  meter          E    =           
0010848
 Z    =       -4608947
88                 I    =           51
53739
 XDOT =      -5873
166526                 Wp   =          111
82072
 YDOT =      -3874
965677  meter/sec      RA   =          193
59259  deg
 ZDOT =       3003
814484                 TA   =          188
26462
                                          MA   =          188
28250
                                          Ha   =            229
275  n
mi
                                          Hp   =            222
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13697539
16                 X    =        -4183144
39
 Y    =        9046078
34  feet           Y    =         2710510
88  meter
 Z    =      -15121220
08                 Z    =        -4629248
38
 XDOT =     -19268
919048                 XDOT =       -5843
989771
 YDOT =     -12713
141984  feet/sec       YDOT =       -3940
480264  meter/sec
 ZDOT =       9855
034395                 ZDOT =        2975
356169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12876759
16                 X    =        -3924836
19
 Y    =       10039884
18  feet           Y    =         3060156
70  meter
 Z    =      -15214966
59                 Z    =        -4637521
82
 XDOT =     -19503
133594                 XDOT =       -5944
555120
 YDOT =     -10287
015484  feet/sec       YDOT =       -3135
482319  meter/sec
 ZDOT =       9723
594097                 ZDOT =        2963
751481


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   20273
00250588  
00016717  00000-0  10270-3 0  9166
2 25544  51
6433 194
7679 0000626 136
7266 223
3933 15
48973340  8100


Satellite: ISS
Catalog Number: 25544
Epoch time:      20273
00250588   =   yrday
fracday
Element set:     916
Inclination:       51
6433  deg
RA of node:       194
7679  deg
Eccentricity:     
0000626     
Arg of perigee:   136
7266  deg
Mean anomaly:     223
3933  deg
Mean motion:   15
48973340  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             810
Checksum:              310
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