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

 
Date: June 19th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 0 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


There are no maneuvers



Coasting Arc #1 (Orbit 3236)
---------------------------------------

Vector Time (GMT): 2020/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5379849
16                 A    =         6801789
43  meter
 Y    =        3800758
45  meter          E    =           
0015382
 Z    =        1669491
70                 I    =           51
50160
 XDOT =      -4025
220986                 Wp   =          110
15439
 YDOT =      -3181
083481  meter/sec      RA   =          336
38971  deg
 ZDOT =      -5691
485512                 TA   =           51
54979
                                          MA   =           51
41185
                                          Ha   =            229
095  n
mi
                                          Hp   =            221
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17650423
76                 X    =        -5430060
00
 Y    =       12469679
94  feet           Y    =         3740316
07  meter
 Z    =        5477334
96                 Z    =         1643237
15
 XDOT =     -13206
105597                 XDOT =       -3961
703900
 YDOT =     -10436
625593  feet/sec       YDOT =       -3225
740127  meter/sec
 ZDOT =     -18672
852729                 ZDOT =       -5710
884894

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11613947
66                 X    =         3539931
25
 Y    =       18260833
55  feet           Y    =         5565902
07  meter
 Z    =        5356281
63                 Z    =         1632594
64
 XDOT =      -9716
754274                 XDOT =       -2961
666703
 YDOT =      11720
050897  feet/sec       YDOT =        3572
271513  meter/sec
 ZDOT =     -18761
805278                 ZDOT =       -5718
598249


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   20171
53549068  
00016717  00000-0  10270-3 0  9008
2 25544  51
6398 336
8471 0002126  68
3295 291
8082 15
49468267 32377


Satellite: ISS
Catalog Number: 25544
Epoch time:      20171
53549068   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:       336
8471  deg
Eccentricity:     
0002126     
Arg of perigee:    68
3295  deg
Mean anomaly:     291
8082  deg
Mean motion:   15
49468267  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3237
Checksum:              329


Coasting Arc #2 (Orbit 3251)
---------------------------------------

Vector Time (GMT): 2020/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5129146
90                 A    =         6802000
98  meter
 Y    =       -4188778
08  meter          E    =           
0010143
 Z    =       -1539426
05                 I    =           51
47340
 XDOT =       4125
315161                 Wp   =           45
69546
 YDOT =       2954
328589  meter/sec      RA   =          331
42894  deg
 ZDOT =       5736
653263                 TA   =          297
48077
                                          MA   =          297
58385
                                          Ha   =            229
227  n
mi
                                          Hp   =            221
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16827909
78                 X    =         5183083
52
 Y    =      -13742710
25  feet           Y    =        -4131118
41  meter
 Z    =       -5050610
40                 Z    =        -1514380
48
 XDOT =      13534
498561                 XDOT =        4064
106964
 YDOT =       9692
679098  feet/sec       YDOT =        3000
117383  meter/sec
 ZDOT =      18821
040890                 ZDOT =        5756
544408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13223859
04                 X    =        -4030632
24
 Y    =      -17272050
56  feet           Y    =        -5264521
01  meter
 Z    =       -4935090
61                 Z    =        -1504215
62
 XDOT =       8837
417482                 XDOT =        2693
644848
 YDOT =     -12140
680130  feet/sec       YDOT =       -3700
479304  meter/sec
 ZDOT =      18912
273325                 ZDOT =        5764
460910


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   20172
50294005  
00016717  00000-0  10270-3 0  9015
2 25544  51
6415 332
0580 0002310  77
6183 282
5226 15
49451199 32520


Satellite: ISS
Catalog Number: 25544
Epoch time:      20172
50294005   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:       332
0580  deg
Eccentricity:     
0002310     
Arg of perigee:    77
6183  deg
Mean anomaly:     282
5226  deg
Mean motion:   15
49451199  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3252
Checksum:              279


Coasting Arc #3 (Orbit 3267)
---------------------------------------

Vector Time (GMT): 2020/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4875339
20                 A    =         6802195
48  meter
 Y    =        4533659
01  meter          E    =           
0015543
 Z    =        1362373
69                 I    =           51
44394
 XDOT =      -4194
234585                 Wp   =          114
24653
 YDOT =      -2756
602179  meter/sec      RA   =          326
46672  deg
 ZDOT =      -5789
950999                 TA   =           50
89868
                                          MA   =           50
76056
                                          Ha   =            229
187  n
mi
                                          Hp   =            221
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15995207
34                 X    =        -4932291
19
 Y    =       14874209
34  feet           Y    =         4478820
76  meter
 Z    =        4469729
95                 Z    =         1338553
90
 XDOT =     -13760
612156                 XDOT =       -4134
973530
 YDOT =      -9043
970403  feet/sec       YDOT =       -2803
172514  meter/sec
 ZDOT =     -18995
902228                 ZDOT =       -5810
181552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14661427
04                 X    =         4468802
96
 Y    =       16220410
82  feet           Y    =         4943981
22  meter
 Z    =        4359825
35                 Z    =         1328874
77
 XDOT =      -8041
516997                 XDOT =       -2451
054381
 YDOT =      12441
050780  feet/sec       YDOT =        3792
032278  meter/sec
 ZDOT =     -19088
713599                 ZDOT =       -5818
239905


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   20173
53488267  
00016717  00000-0  10270-3 0  9025
2 25544  51
6403 326
9496 0002290  78
6532 281
4875 15
49459007 32682


Satellite: ISS
Catalog Number: 25544
Epoch time:      20173
53488267   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:       326
9496  deg
Eccentricity:     
0002290     
Arg of perigee:    78
6532  deg
Mean anomaly:     281
4875  deg
Mean motion:   15
49459007  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3268
Checksum:              331


Coasting Arc #4 (Orbit 3282)
---------------------------------------

Vector Time (GMT): 2020/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4566178
64                 A    =         6802352
63  meter
 Y    =       -4884728
73  meter          E    =           
0010891
 Z    =       -1229284
90                 I    =           51
41828
 XDOT =       4274
194837                 Wp   =           46
73478
 YDOT =       2539
310129  meter/sec      RA   =          321
50318  deg
 ZDOT =       5826
180408                 TA   =          299
89151
                                          MA   =          299
99966
                                          Ha   =            229
242  n
mi
                                          Hp   =            221
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14980901
04                 X    =         4626432
88
 Y    =      -16026012
89  feet           Y    =        -4833329
30  meter
 Z    =       -4033086
94                 Z    =        -1206959
04
 XDOT =      14022
948940                 XDOT =        4217
181815
 YDOT =       8331
069978  feet/sec       YDOT =        2586
787202  meter/sec
 ZDOT =      19114
765117                 ZDOT =        5846
804691

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16085982
15                 X    =        -4903007
36
 Y    =      -14943971
97  feet           Y    =        -4554922
66  meter
 Z    =       -3930032
48                 Z    =        -1197873
90
 XDOT =       7186
905855                 XDOT =        2190
568905
 YDOT =     -12752
506787  feet/sec       YDOT =       -3886
964069  meter/sec
 ZDOT =      19209
408360                 ZDOT =        5855
027668


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   20174
50233003  
00016717  00000-0  10270-3 0  9030
2 25544  51
6416 322
1617 0002339  85
2993 274
8424 15
49450369 32833


Satellite: ISS
Catalog Number: 25544
Epoch time:      20174
50233003   =   yrday
fracday
Element set:     903
Inclination:       51
6416  deg
RA of node:       322
1617  deg
Eccentricity:     
0002339     
Arg of perigee:    85
2993  deg
Mean anomaly:     274
8424  deg
Mean motion:   15
49450369  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3283
Checksum:              297


Coasting Arc #5 (Orbit 3298)
---------------------------------------

Vector Time (GMT): 2020/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4259186
20                 A    =         6802509
02  meter
 Y    =        5190536
97  meter          E    =           
0015374
 Z    =        1048949
55                 I    =           51
39320
 XDOT =      -4328
232004                 Wp   =          118
58360
 YDOT =      -2353
865695  meter/sec      RA   =          316
53713  deg
 ZDOT =      -5868
379030                 TA   =           50
02429
                                          MA   =           49
88939
                                          Ha   =            229
170  n
mi
                                          Hp   =            221
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13973708
01                 X    =        -4322006
92
 Y    =       17029320
77  feet           Y    =         5142556
25  meter
 Z    =        3441435
52                 Z    =         1028108
80
 XDOT =     -14200
236233                 XDOT =       -4273
083809
 YDOT =      -7722
656481  feet/sec       YDOT =       -2401
957522  meter/sec
 ZDOT =     -19253
212041                 ZDOT =       -5889
270180

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17322280
36                 X    =         5279831
05
 Y    =       13632828
59  feet           Y    =         4155286
15  meter
 Z    =        3345197
68                 Z    =         1019616
25
 XDOT =      -6429
745226                 XDOT =       -1959
786345
 YDOT =      12966
061448  feet/sec       YDOT =        3952
055529  meter/sec
 ZDOT =     -19349
101972                 ZDOT =       -5897
606281


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   20175
53427170  
00016717  00000-0  10270-3 0  9045
2 25544  51
6416 317
0533 0002231  87
3068 272
8337 15
49456341 32994


Satellite: ISS
Catalog Number: 25544
Epoch time:      20175
53427170   =   yrday
fracday
Element set:     904
Inclination:       51
6416  deg
RA of node:       317
0533  deg
Eccentricity:     
0002231     
Arg of perigee:    87
3068  deg
Mean anomaly:     272
8337  deg
Mean motion:   15
49456341  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3299
Checksum:              303


Coasting Arc #6 (Orbit 3313)
---------------------------------------

Vector Time (GMT): 2020/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3898675
79                 A    =         6802617
16  meter
 Y    =       -5494195
27  meter          E    =           
0011682
 Z    =        -912019
87                 I    =           51
37145
 XDOT =       4392
644372                 Wp   =           47
73523
 YDOT =       2147
670356  meter/sec      RA   =          311
56991  deg
 ZDOT =       5895
832665                 TA   =          302
37665
                                          MA   =          302
48965
                                          Ha   =            229
231  n
mi
                                          Hp   =            221
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12790931
06                 X    =         3964253
76
 Y    =      -18025575
04  feet           Y    =        -5450230
66  meter
 Z    =       -2992191
18                 Z    =         -892923
65
 XDOT =      14411
562899                 XDOT =        4339
663863
 YDOT =       7046
162585  feet/sec       YDOT =        2196
494707  meter/sec
 ZDOT =      19343
283023                 ZDOT =        5917
041821

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18504198
33                 X    =        -5640079
65
 Y    =      -12109669
72  feet           Y    =        -3691027
33  meter
 Z    =       -2903967
04                 Z    =         -885129
16
 XDOT =       5610
873292                 XDOT =        1710
194180
 YDOT =     -13190
046865  feet/sec       YDOT =       -4020
326284  meter/sec
 ZDOT =      19440
656110                 ZDOT =        5925
511982


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   20176
50171568  
00016717  00000-0  10270-3 0  9051
2 25544  51
6432 312
2651 0002340  89
0786 271
0633 15
49454025 33142


Satellite: ISS
Catalog Number: 25544
Epoch time:      20176
50171568   =   yrday
fracday
Element set:     905
Inclination:       51
6432  deg
RA of node:       312
2651  deg
Eccentricity:     
0002340     
Arg of perigee:    89
0786  deg
Mean anomaly:     271
0633  deg
Mean motion:   15
49454025  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3314
Checksum:              287


Coasting Arc #7 (Orbit 3329)
---------------------------------------

Vector Time (GMT): 2020/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3546655
63                 A    =         6802728
68  meter
 Y    =        5751399
83  meter          E    =           
0015153
 Z    =         727707
32                 I    =           51
34940
 XDOT =      -4436
586413                 Wp   =          122
09872
 YDOT =      -1975
506053  meter/sec      RA   =          306
60139  deg
 ZDOT =      -5926
438384                 TA   =           50
02074
                                          MA   =           49
88777
                                          Ha   =            229
192  n
mi
                                          Hp   =            221
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11636009
29                 X    =        -3614240
63
 Y    =       18869422
03  feet           Y    =         5711360
59  meter
 Z    =        2387491
22                 Z    =          710316
11
 XDOT =     -14555
729703                 XDOT =       -4385
379196
 YDOT =      -6481
319072  feet/sec       YDOT =       -2024
831847  meter/sec
 ZDOT =     -19443
695485                 ZDOT =       -5947
865196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19487869
00                 X    =         5939902
47
 Y    =       10585468
23  feet           Y    =         3226450
72  meter
 Z    =        2307106
05                 Z    =          703205
92
 XDOT =      -4899
019211                 XDOT =       -1493
221055
 YDOT =      13339
732965  feet/sec       YDOT =        4065
950608  meter/sec
 ZDOT =     -19542
086539                 ZDOT =       -5956
427977


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   20177
53365428  
00016717  00000-0  10270-3 0  9066
2 25544  51
6422 307
1575 0002325  92
6699 267
4718 15
49459597 33305


Satellite: ISS
Catalog Number: 25544
Epoch time:      20177
53365428   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       307
1575  deg
Eccentricity:     
0002325     
Arg of perigee:    92
6699  deg
Mean anomaly:     267
4718  deg
Mean motion:   15
49459597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3330
Checksum:              335


Coasting Arc #8 (Orbit 3344)
---------------------------------------

Vector Time (GMT): 2020/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3142336
73                 A    =         6802820
34  meter
 Y    =       -5999487
20  meter          E    =           
0012363
 Z    =        -588473
93                 I    =           51
33091
 XDOT =       4491
705931                 Wp   =           49
71057
 YDOT =       1778
434345  meter/sec      RA   =          301
63139  deg
 ZDOT =       5944
427849                 TA   =          303
92392
                                          MA   =          304
04141
                                          Ha   =            229
226  n
mi
                                          Hp   =            221
164

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10309503
70                 X    =         3212049
66
 Y    =      -19683356
97  feet           Y    =        -5963957
48  meter
 Z    =       -1930688
74                 Z    =         -573041
41
 XDOT =      14736
568015                 XDOT =        4442
610906
 YDOT =       5834
758351  feet/sec       YDOT =        1828
388479  meter/sec
 ZDOT =      19502
716039                 ZDOT =        5966
127491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20382117
52                 X    =        -6212469
42
 Y    =       -8863419
85  feet           Y    =        -2701570
37  meter
 Z    =       -1859312
02                 Z    =         -566718
30
 XDOT =       4111
875277                 XDOT =        1253
299585
 YDOT =     -13502
808433  feet/sec       YDOT =       -4115
656011  meter/sec
 ZDOT =      19602
378774                 ZDOT =        5974
805050


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   20178
50109655  
00016717  00000-0  10270-3 0  9073
2 25544  51
6426 302
3695 0002341  95
2545 264
8872 15
49451420 33451


Satellite: ISS
Catalog Number: 25544
Epoch time:      20178
50109655   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:       302
3695  deg
Eccentricity:     
0002341     
Arg of perigee:    95
2545  deg
Mean anomaly:     264
8872  deg
Mean motion:   15
49451420  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3345
Checksum:              308


Coasting Arc #9 (Orbit 3360)
---------------------------------------

Vector Time (GMT): 2020/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2753244
18                 A    =         6802864
51  meter
 Y    =        6200716
21  meter          E    =           
0014731
 Z    =         401731
73                 I    =           51
31454
 XDOT =      -4531
421530                 Wp   =          126
00005
 YDOT =      -1616
284202  meter/sec      RA   =          296
65984  deg
 ZDOT =      -5963
129380                 TA   =           49
65710
                                          MA   =           49
52853
                                          Ha   =            229
152  n
mi
                                          Hp   =            221
195

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9032953
36                 X    =        -2824329
17
 Y    =       20343557
12  feet           Y    =         6169529
96  meter
 Z    =        1318017
49                 Z    =          388185
78
 XDOT =     -14866
868537                 XDOT =       -4484
045821
 YDOT =      -5302
769691  feet/sec       YDOT =       -1666
692182  meter/sec
 ZDOT =     -19564
072769                 ZDOT =       -5985
026145

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21073951
64                 X    =         6423340
46
 Y    =        7176661
03  feet           Y    =         2187446
28  meter
 Z    =        1255321
18                 Z    =          382621
89
 XDOT =      -3434
830300                 XDOT =       -1046
936275
 YDOT =      13613
524008  feet/sec       YDOT =        4149
402118  meter/sec
 ZDOT =     -19664
654857                 ZDOT =       -5993
786800


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   20179
53303300  
00016717  00000-0  10270-3 0  9081
2 25544  51
6426 297
2614 0002266 100
0140 260
1266 15
49463083 33618


Satellite: ISS
Catalog Number: 25544
Epoch time:      20179
53303300   =   yrday
fracday
Element set:     908
Inclination:       51
6426  deg
RA of node:       297
2614  deg
Eccentricity:     
0002266     
Arg of perigee:   100
0140  deg
Mean anomaly:     260
1266  deg
Mean motion:   15
49463083  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3361
Checksum:              273


Coasting Arc #10 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2020/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2315863
90                 A    =         6802912
47  meter
 Y    =       -6385848
58  meter          E    =           
0013083
 Z    =        -259477
38                 I    =           51
30151
 XDOT =       4580
759249                 Wp   =           51
92616
 YDOT =       1427
293446  meter/sec      RA   =          291
68706  deg
 ZDOT =       5971
670699                 TA   =          305
27043
                                          MA   =          305
39276
                                          Ha   =            229
216  n
mi
                                          Hp   =            221
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7597978
66                 X    =         2388360
62
 Y    =      -20950946
77  feet           Y    =        -6359545
55  meter
 Z    =        -851303
76                 Z    =         -248052
54
 XDOT =      15028
737693                 XDOT =        4535
451603
 YDOT =       4682
721279  feet/sec       YDOT =        1478
264750  meter/sec
 ZDOT =      19592
095470                 ZDOT =        5993
812218

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21644284
14                 X    =        -6597177
80
 Y    =       -5318246
34  feet           Y    =        -1621001
49  meter
 Z    =        -798366
08                 Z    =         -243341
98
 XDOT =       2675
370167                 XDOT =         815
452827
 YDOT =     -13732
178236  feet/sec       YDOT =       -4185
567926  meter/sec
 ZDOT =      19693
816478                 ZDOT =        6002
675263


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   20180
50047177  
00016717  00000-0  10270-3 0  9098
2 25544  51
6435 292
4730 0002371  98
6876 261
4543 15
49457984 33760


Satellite: ISS
Catalog Number: 25544
Epoch time:      20180
50047177   =   yrday
fracday
Element set:     909
Inclination:       51
6435  deg
RA of node:       292
4730  deg
Eccentricity:     
0002371     
Arg of perigee:    98
6876  deg
Mean anomaly:     261
4543  deg
Mean motion:   15
49457984  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3376
Checksum:              332


Coasting Arc #11 (Orbit 3391)
---------------------------------------

Vector Time (GMT): 2020/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1900594
98                 A    =         6802938
23  meter
 Y    =        6525183
73  meter          E    =           
0014299
 Z    =          70219
87                 I    =           51
28930
 XDOT =      -4620
164066                 Wp   =          129
01888
 YDOT =      -1272
626985  meter/sec      RA   =          286
71375  deg
 ZDOT =      -5977
823846                 TA   =           50
22250
                                          MA   =           50
09665
                                          Ha   =            229
189  n
mi
                                          Hp   =            221
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6235547
83                 X    =        -1973761
36
 Y    =       21408083
10  feet           Y    =         6503520
81  meter
 Z    =         230380
15                 Z    =           60810
64
 XDOT =     -15158
018588                 XDOT =       -4576
553007
 YDOT =      -4175
285385  feet/sec       YDOT =       -1324
048375  meter/sec
 ZDOT =     -19612
282958                 ZDOT =       -6000
160985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22016555
62                 X    =         6710646
15
 Y    =        3532360
27  feet           Y    =         1076663
41  meter
 Z    =         186716
57                 Z    =           56911
21
 XDOT =      -2022
248006                 XDOT =        -616
381192
 YDOT =      13820
631547  feet/sec       YDOT =        4212
528496  meter/sec
 ZDOT =     -19714
914574                 ZDOT =       -6009
105962


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   20181
53240543  
00016717  00000-0  10270-3 0  9106
2 25544  51
6426 287
3651 0002376 104
4909 255
6505 15
49458206 33922


Satellite: ISS
Catalog Number: 25544
Epoch time:      20181
53240543   =   yrday
fracday
Element set:     910
Inclination:       51
6426  deg
RA of node:       287
3651  deg
Eccentricity:     
0002376     
Arg of perigee:   104
4909  deg
Mean anomaly:     255
6505  deg
Mean motion:   15
49458206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3392
Checksum:              302


Coasting Arc #12 (Orbit 3407)
---------------------------------------

Vector Time (GMT): 2020/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1440240
98                 A    =         6802934
92  meter
 Y    =       -6642744
89  meter          E    =           
0013605
 Z    =          73030
68                 I    =           51
28149
 XDOT =       4667
810269                 Wp   =           54
71213
 YDOT =       1086
365497  meter/sec      RA   =          281
73966  deg
 ZDOT =       5976
446209                 TA   =          306
07686
                                          MA   =          306
20279
                                          Ha   =            229
188  n
mi
                                          Hp   =            221
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4725200
08                 X    =         1514060
35
 Y    =      -21793782
45  feet           Y    =        -6626226
35  meter
 Z    =         239601
98                 Z    =           80205
16
 XDOT =      15314
338152                 XDOT =        4626
285117
 YDOT =       3564
191264  feet/sec       YDOT =        1138
331246  meter/sec
 ZDOT =      19607
763152                 ZDOT =        5999
019918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22242264
20                 X    =        -6779442
13
 Y    =       -1600325
24  feet           Y    =         -487779
13  meter
 Z    =         272984
68                 Z    =           83205
73
 XDOT =       1270
406581                 XDOT =         387
219926
 YDOT =     -13909
637484  feet/sec       YDOT =       -4239
657505  meter/sec
 ZDOT =      19711
496511                 ZDOT =        6008
064136


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   20182
56433869  
00016717  00000-0  10270-3 0  9116
2 25544  51
6433 282
2576 0002341 105
0526 255
0884 15
49458882 34086


Satellite: ISS
Catalog Number: 25544
Epoch time:      20182
56433869   =   yrday
fracday
Element set:     911
Inclination:       51
6433  deg
RA of node:       282
2576  deg
Eccentricity:     
0002341     
Arg of perigee:   105
0526  deg
Mean anomaly:     255
0884  deg
Mean motion:   15
49458882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3408
Checksum:              316


Coasting Arc #13 (Orbit 3422)
---------------------------------------

Vector Time (GMT): 2020/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1009110
27                 A    =         6802901
53  meter
 Y    =        6716517
83  meter          E    =           
0013646
 Z    =        -262998
34                 I    =           51
27559
 XDOT =      -4709
890568                 Wp   =          132
32943
 YDOT =       -933
236410  meter/sec      RA   =          276
76509  deg
 ZDOT =      -5969
978797                 TA   =           50
51340
                                          MA   =           50
39280
                                          Ha   =            229
146  n
mi
                                          Hp   =            221
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3310729
24                 X    =        -1082863
88
 Y    =       22035819
65  feet           Y    =         6704820
90  meter
 Z    =        -862855
45                 Z    =         -268078
22
 XDOT =     -15452
396877                 XDOT =       -4670
106032
 YDOT =      -3061
799245  feet/sec       YDOT =        -985
682320  meter/sec
 ZDOT =     -19586
544610                 ZDOT =       -5992
761151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22281104
62                 X    =         6791280
69
 Y    =        -221613
19  feet           Y    =          -67547
70  meter
 Z    =        -886600
18                 Z    =         -270235
73
 XDOT =       -617
972986                 XDOT =        -188
358166
 YDOT =      13985
372701  feet/sec       YDOT =        4262
741599  meter/sec
 ZDOT =     -19691
251189                 ZDOT =       -6001
893362


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   20183
53177455  
00016717  00000-0  10270-3 0  9121
2 25544  51
6432 277
4690 0002319 110
8244 249
3155 15
49460393 34238


Satellite: ISS
Catalog Number: 25544
Epoch time:      20183
53177455   =   yrday
fracday
Element set:     912
Inclination:       51
6432  deg
RA of node:       277
4690  deg
Eccentricity:     
0002319     
Arg of perigee:   110
8244  deg
Mean anomaly:     249
3155  deg
Mean motion:   15
49460393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3423
Checksum:              303


Coasting Arc #14 (Orbit 3438)
---------------------------------------

Vector Time (GMT): 2020/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         538720
56                 A    =         6802864
77  meter
 Y    =       -6763389
15  meter          E    =           
0014128
 Z    =         408024
30                 I    =           51
27349
 XDOT =       4757
191988                 Wp   =           57
38512
 YDOT =        747
066805  meter/sec      RA   =          271
78996  deg
 ZDOT =       5958
524020                 TA   =          307
02798
                                          MA   =          307
15715
                                          Ha   =            229
153  n
mi
                                          Hp   =            221
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1767455
89                 X    =          612328
80
 Y    =      -22189596
95  feet           Y    =        -6756953
30  meter
 Z    =        1338662
39                 Z    =          410818
69
 XDOT =      15607
585262                 XDOT =        4719
541446
 YDOT =       2451
006579  feet/sec       YDOT =         800
053477  meter/sec
 ZDOT =      19548
963320                 ZDOT =        5981
541264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22154576
91                 X    =        -6752715
04
 Y    =        2154355
68  feet           Y    =          656647
61  meter
 Z    =        1351888
97                 Z    =          412055
76
 XDOT =       -138
265302                 XDOT =         -42
143264
 YDOT =     -14048
720603  feet/sec       YDOT =       -4282
050040  meter/sec
 ZDOT =      19654
767970                 ZDOT =        5990
773277


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   20184
56370444  
00016717  00000-0  10270-3 0  9139
2 25544  51
6440 272
3612 0002279 107
7307 252
4092 15
49459725 34394


Satellite: ISS
Catalog Number: 25544
Epoch time:      20184
56370444   =   yrday
fracday
Element set:     913
Inclination:       51
6440  deg
RA of node:       272
3612  deg
Eccentricity:     
0002279     
Arg of perigee:   107
7307  deg
Mean anomaly:     252
4092  deg
Mean motion:   15
49459725  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3439
Checksum:              307


Coasting Arc #15 (Orbit 3453)
---------------------------------------

Vector Time (GMT): 2020/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -103838
42                 A    =         6802776
01  meter
 Y    =        6770190
57  meter          E    =           
0012888
 Z    =        -598219
81                 I    =           51
27202
 XDOT =      -4802
922920                 Wp   =          134
55524
 YDOT =       -590
632622  meter/sec      RA   =          266
81573  deg
 ZDOT =      -5938
875693                 TA   =           51
92221
                                          MA   =           51
80603
                                          Ha   =            229
139  n
mi
                                          Hp   =            221
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -340677
22                 X    =         -176631
19
 Y    =       22211911
32  feet           Y    =         6768622
49  meter
 Z    =       -1962663
43                 Z    =         -598899
64
 XDOT =     -15757
621130                 XDOT =       -4767
113835
 YDOT =      -1937
771068  feet/sec       YDOT =        -644
140901  meter/sec
 ZDOT =     -19484
500306                 ZDOT =       -5962
119435

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21861335
48                 X    =         6663335
05
 Y    =       -3943775
75  feet           Y    =        -1202062
85  meter
 Z    =       -1966152
86                 Z    =         -599283
39
 XDOT =        809
758972                 XDOT =         246
814535
 YDOT =      14111
819381  feet/sec       YDOT =        4301
282547  meter/sec
 ZDOT =     -19591
364867                 ZDOT =       -5971
448011


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   20185
53113843  
00016717  00000-0  10270-3 0  9146
2 25544  51
6426 267
5734 0002319 113
1063 247
0332 15
49461732 34549


Satellite: ISS
Catalog Number: 25544
Epoch time:      20185
53113843   =   yrday
fracday
Element set:     914
Inclination:       51
6426  deg
RA of node:       267
5734  deg
Eccentricity:     
0002319     
Arg of perigee:   113
1063  deg
Mean anomaly:     247
0332  deg
Mean motion:   15
49461732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3454
Checksum:              289
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