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

 
Date: September 30th 2020

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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) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 431 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


276/01:38:44 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 222 6

277/05:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 222 5

278/10:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 7
000/00:00:00 000 0 0 0 0 222 7

280/09:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 222 5

281/08:14:18 140 -2 3 -2 5 2 5
N/A 1 1 -0 0 228 1
000/00:06:36 280 0 1 -0 0 222 6

283/20:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 222 6

Coasting Arc #1 (Orbit 802)
---------------------------------------

Vector Time (GMT): 2020/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -759042
60                 A    =         6793863
75  meter
 Y    =       -4430423
38  meter          E    =           
0006431
 Z    =        5090354
72                 I    =           51
51362
 XDOT =       7432
096846                 Wp   =          120
81535
 YDOT =        714
184410  meter/sec      RA   =          196
07331  deg
 ZDOT =       1724
974629                 TA   =          312
44441
                                          MA   =          312
49877
                                          Ha   =            229
787  n
mi
                                          Hp   =            222
595

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2490297
25                 X    =         -734169
81
 Y    =      -14535509
77  feet           Y    =        -4438772
11  meter
 Z    =       16700638
84                 Z    =         5086728
32
 XDOT =      24383
519836                 XDOT =        7415
179339
 YDOT =       2343
124706  feet/sec       YDOT =         797
200976  meter/sec
 ZDOT =       5659
365582                 ZDOT =        1761
035589

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4311700
63                 X    =         1314206
35
 Y    =       14122721
36  feet           Y    =         4304605
47  meter
 Z    =       16683882
68                 Z    =         5085247
44
 XDOT =     -23420
432651                 XDOT =       -7138
547872
 YDOT =        249
072750  feet/sec       YDOT =          75
917374  meter/sec
 ZDOT =       5825
898384                 ZDOT =        1775
733827


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
55149341  
00016717  00000-0  10270-3 0  9002
2 25544  51
6421 197
0085 0001162 100
5667 259
5613 15
48830030  8030


Satellite: ISS
Catalog Number: 25544
Epoch time:      20272
55149341   =   yrday
fracday
Element set:     900
Inclination:       51
6421  deg
RA of node:       197
0085  deg
Eccentricity:     
0001162     
Arg of perigee:   100
5667  deg
Mean anomaly:     259
5613  deg
Mean motion:   15
48830030  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             803
Checksum:              276


Coasting Arc #2 (Orbit 817)
---------------------------------------

Vector Time (GMT): 2020/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1204823
18                 A    =         6793969
53  meter
 Y    =        4353908
15  meter          E    =           
0014275
 Z    =       -5087343
23                 I    =           51
54782
 XDOT =      -7438
461786                 Wp   =           78
69550
 YDOT =        -20
948621  meter/sec      RA   =          191
12200  deg
 ZDOT =      -1781
086145                 TA   =          174
01478
                                          MA   =          173
99771
                                          Ha   =            229
826  n
mi
                                          Hp   =            222
587

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3952831
96                 X    =         1180758
32
 Y    =       14284475
57  feet           Y    =         4367246
36  meter
 Z    =      -16690758
64                 Z    =        -5081549
50
 XDOT =     -24404
402184                 XDOT =       -7429
023196
 YDOT =        -68
729071  feet/sec       YDOT =        -104
078214  meter/sec
 ZDOT =      -5843
458482                 ZDOT =       -1817
196333

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5968794
33                 X    =        -1819288
51
 Y    =      -13599177
83  feet           Y    =        -4145029
40  meter
 Z    =      -16663985
23                 Z    =        -5079182
70
 XDOT =      23155
904529                 XDOT =        7057
919701
 YDOT =      -2804
716506  feet/sec       YDOT =        -854
877591  meter/sec
 ZDOT =      -6010
236275                 ZDOT =       -1831
920017


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
51934585  
00016717  00000-0  10270-3 0  9012
2 25544  51
6433 192
2222 0001272  98
3936 261
7358 15
48819907  8185


Satellite: ISS
Catalog Number: 25544
Epoch time:      20273
51934585   =   yrday
fracday
Element set:     901
Inclination:       51
6433  deg
RA of node:       192
2222  deg
Eccentricity:     
0001272     
Arg of perigee:    98
3936  deg
Mean anomaly:     261
7358  deg
Mean motion:   15
48819907  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             818
Checksum:              321


Coasting Arc #3 (Orbit 833)
---------------------------------------

Vector Time (GMT): 2020/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1649632
45                 A    =         6793985
03  meter
 Y    =       -4216232
11  meter          E    =           
0006775
 Z    =        5061571
67                 I    =           51
58182
 XDOT =       7406
330962                 Wp   =          121
31218
 YDOT =       -672
999570  meter/sec      RA   =          186
17387  deg
 ZDOT =       1847
943585                 TA   =          310
73240
                                          MA   =          310
79120
                                          Ha   =            229
803  n
mi
                                          Hp   =            222
583

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5412179
97                 X    =        -1626948
98
 Y    =      -13832782
50  feet           Y    =        -4234552
16  meter
 Z    =       16606206
25                 Z    =         5053613
87
 XDOT =      24298
986095                 XDOT =        7404
329907
 YDOT =      -2208
003837  feet/sec       YDOT =        -590
187675  meter/sec
 ZDOT =       6062
807036                 ZDOT =        1883
915964

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7574416
75                 X    =         2308682
22
 Y    =       12825202
58  feet           Y    =         3909121
75  meter
 Z    =       16569430
88                 Z    =         5050362
53
 XDOT =     -22699
473668                 XDOT =       -6918
799574
 YDOT =       5336
170839  feet/sec       YDOT =        1626
464872  meter/sec
 ZDOT =       6228
963288                 ZDOT =        1898
588010


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   20274
55171330  
00016717  00000-0  10270-3 0  9029
2 25544  51
6436 187
1176 0001178 105
0713 255
0568 15
48839673  8342


Satellite: ISS
Catalog Number: 25544
Epoch time:      20274
55171330   =   yrday
fracday
Element set:     902
Inclination:       51
6436  deg
RA of node:       187
1176  deg
Eccentricity:     
0001178     
Arg of perigee:   105
0713  deg
Mean anomaly:     255
0568  deg
Mean motion:   15
48839673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             834
Checksum:              305


Coasting Arc #4 (Orbit 848)
---------------------------------------

Vector Time (GMT): 2020/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2066276
83                 A    =         6794054
12  meter
 Y    =        4052645
24  meter          E    =           
0014043
 Z    =       -5059109
18                 I    =           51
61638
 XDOT =      -7286
091918                 Wp   =           78
25638
 YDOT =       1347
647928  meter/sec      RA   =          181
22761  deg
 ZDOT =      -1897
979273                 TA   =          173
29836
                                          MA   =          173
27956
                                          Ha   =            229
800  n
mi
                                          Hp   =            222
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6779123
45                 X    =         2045379
81
 Y    =       13296080
17  feet           Y    =         4075634
49  meter
 Z    =      -16598127
22                 Z    =        -5049123
09
 XDOT =     -23904
501043                 XDOT =       -7291
400833
 YDOT =       4421
417088  feet/sec       YDOT =        1266
139751  meter/sec
 ZDOT =      -6226
966118                 ZDOT =       -1933
385560

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9049792
39                 X    =        -2758376
72
 Y    =      -11932032
16  feet           Y    =        -3636883
40  meter
 Z    =      -16551977
40                 Z    =        -5045042
71
 XDOT =      21894
154967                 XDOT =        6673
338434
 YDOT =      -7748
363542  feet/sec       YDOT =       -2361
701207  meter/sec
 ZDOT =      -6390
521187                 ZDOT =       -1947
830858


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   20275
51955493  
00016717  00000-0  10270-3 0  9037
2 25544  51
6442 182
3319 0001294 100
7312 259
3983 15
48840357  8496


Satellite: ISS
Catalog Number: 25544
Epoch time:      20275
51955493   =   yrday
fracday
Element set:     903
Inclination:       51
6442  deg
RA of node:       182
3319  deg
Eccentricity:     
0001294     
Arg of perigee:   100
7312  deg
Mean anomaly:     259
3983  deg
Mean motion:   15
48840357  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             849
Checksum:              317


Coasting Arc #5 (Orbit 857)
---------------------------------------

Vector Time (GMT): 2020/276/01:38:44
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6788547
61                 A    =         6804731
27  meter
 Y    =          98596
05  meter          E    =           
0012655
 Z    =        -364009
99                 I    =           51
66980
 XDOT =       -383
235661                 Wp   =          135
45294
 YDOT =       4752
427023  meter/sec      RA   =          178
40267  deg
 ZDOT =      -5995
252475                 TA   =           48
46054
                                          MA   =           48
35207
                                          Ha   =            229
814  n
mi
                                          Hp   =            222
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22272137
81                 X    =         6788708
71
 Y    =         323477
84  feet           Y    =          174511
32  meter
 Z    =       -1194258
49                 Z    =         -331033
15
 XDOT =      -1257
334846                 XDOT =        -407
228430
 YDOT =      15591
952175  feet/sec       YDOT =        4748
006676  meter/sec
 ZDOT =     -19669
463500                 ZDOT =       -5997
172837

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18431857
81                 X    =         5618030
26
 Y    =      -12520385
52  feet           Y    =        -3816213
51  meter
 Z    =       -1041910
75                 Z    =         -317574
40
 XDOT =       7114
425756                 XDOT =        2168
476970
 YDOT =      12068
685124  feet/sec       YDOT =        3678
535226  meter/sec
 ZDOT =     -19678
313371                 ZDOT =       -5997
949916


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   20276
10025701  
00016717  00000-0  10270-3 0  9044
2 25544  51
6428 179
4591 0001313 116
7713 243
3571 15
48830213  8589


Satellite: ISS
Catalog Number: 25544
Epoch time:      20276
10025701   =   yrday
fracday
Element set:     904
Inclination:       51
6428  deg
RA of node:       179
4591  deg
Eccentricity:     
0001313     
Arg of perigee:   116
7713  deg
Mean anomaly:     243
3571  deg
Mean motion:   15
48830213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             858
Checksum:              287


Coasting Arc #6 (Orbit 873)
---------------------------------------

Vector Time (GMT): 2020/277/01:38:44
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6771088
63                 A    =         6804871
28  meter
 Y    =         543057
69  meter          E    =           
0013050
 Z    =         293542
37                 I    =           51
70309
 XDOT =       -113
675381                 Wp   =           53
27452
 YDOT =      -4757
686561  meter/sec      RA   =          173
45900  deg
 ZDOT =       6002
124736                 TA   =          309
87897
                                          MA   =          309
99366
                                          Ha   =            229
813  n
mi
                                          Hp   =            222
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22214857
71                 X    =        -6778083
91
 Y    =        1781685
35  feet           Y    =          467299
44  meter
 Z    =         963065
51                 Z    =          260633
54
 XDOT =       -372
950726                 XDOT =         -89
620376
 YDOT =     -15609
207877  feet/sec       YDOT =       -4758
822727  meter/sec
 ZDOT =      19692
010288                 ZDOT =        6001
631386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16928627
99                 X    =        -5159845
81
 Y    =       14503985
81  feet           Y    =         4420814
88  meter
 Z    =         811018
57                 Z    =          247198
46
 XDOT =      -8528
394744                 XDOT =       -2599
454718
 YDOT =     -11093
757184  feet/sec       YDOT =       -3381
377190  meter/sec
 ZDOT =      19689
710822                 ZDOT =        6001
423858


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   20277
13261532  
00016717  00000-0  10270-3 0  9053
2 25544  51
6423 174
3542 0001206 114
2976 245
8300 15
48788685  8749


Satellite: ISS
Catalog Number: 25544
Epoch time:      20277
13261532   =   yrday
fracday
Element set:     905
Inclination:       51
6423  deg
RA of node:       174
3542  deg
Eccentricity:     
0001206     
Arg of perigee:   114
2976  deg
Mean anomaly:     245
8300  deg
Mean motion:   15
48788685  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             874
Checksum:              306


Coasting Arc #7 (Orbit 875)
---------------------------------------

Vector Time (GMT): 2020/277/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1764120
09                 A    =         6794181
78  meter
 Y    =        4235861
78  meter          E    =           
0014078
 Z    =       -5023546
89                 I    =           51
67197
 XDOT =      -7345
887852                 Wp   =          105
87587
 YDOT =       -655
907237  meter/sec      RA   =          172
54958  deg
 ZDOT =       2027
580505                 TA   =          183
86868
                                          MA   =          183
87958
                                          Ha   =            229
820  n
mi
                                          Hp   =            222
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5787795
56                 X    =        -1786953
75
 Y    =       13897184
33  feet           Y    =         4216006
02  meter
 Z    =      -16481453
04                 Z    =        -5032172
25
 XDOT =     -24100
681930                 XDOT =       -7347
856318
 YDOT =      -2151
926632  feet/sec       YDOT =        -738
065055  meter/sec
 ZDOT =       6652
167012                 ZDOT =        1991
891778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14730236
83                 X    =         4489776
18
 Y    =        2887169
95  feet           Y    =          880009
40  meter
 Z    =      -16521288
59                 Z    =        -5035688
76
 XDOT =       2757
915996                 XDOT =         840
612796
 YDOT =      23032
931839  feet/sec       YDOT =        7020
437625  meter/sec
 ZDOT =       6487
267824                 ZDOT =        1977
319233


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   20277
26165785  
00016717  00000-0  10270-3 0  9061
2 25544  51
6404 173
7168 0001291 112
3921 247
7365 15
48810465  8764


Satellite: ISS
Catalog Number: 25544
Epoch time:      20277
26165785   =   yrday
fracday
Element set:     906
Inclination:       51
6404  deg
RA of node:       173
7168  deg
Eccentricity:     
0001291     
Arg of perigee:   112
3921  deg
Mean anomaly:     247
7365  deg
Mean motion:   15
48810465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             876
Checksum:              319


Coasting Arc #8 (Orbit 891)
---------------------------------------

Vector Time (GMT): 2020/278/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1339829
03                 A    =         6794024
34  meter
 Y    =       -4360958
27  meter          E    =           
0006436
 Z    =        5030175
38                 I    =           51
70509
 XDOT =       7401
514808                 Wp   =           65
65827
 YDOT =        -21
182618  meter/sec      RA   =          167
60893  deg
 ZDOT =      -1985
226698                 TA   =           43
64111
                                          MA   =           43
59023
                                          Ha   =            229
699  n
mi
                                          Hp   =            222
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4395764
54                 X    =         1364060
82
 Y    =      -14307605
88  feet           Y    =        -4345839
48  meter
 Z    =       16503200
08                 Z    =         5036743
05
 XDOT =      24283
185067                 XDOT =        7410
844859
 YDOT =        -69
496777  feet/sec       YDOT =          61
638452  meter/sec
 ZDOT =      -6513
210952                 ZDOT =       -1949
249696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14886952
20                 X    =        -4537543
03
 Y    =       -1186093
66  feet           Y    =         -361521
35  meter
 Z    =       16533535
03                 Z    =         5039421
48
 XDOT =      -5258
240114                 XDOT =       -1602
711587
 YDOT =     -22685
604006  feet/sec       YDOT =       -6914
572101  meter/sec
 ZDOT =      -6346
963741                 ZDOT =       -1934
554548


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   20278
29400787  
00016717  00000-0  10270-3 0  9070
2 25544  51
6404 168
6112 0001188 114
9589 245
1684 15
48841847  8921


Satellite: ISS
Catalog Number: 25544
Epoch time:      20278
29400787   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       168
6112  deg
Eccentricity:     
0001188     
Arg of perigee:   114
9589  deg
Mean anomaly:     245
1684  deg
Mean motion:   15
48841847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             892
Checksum:              335


Coasting Arc #9 (Orbit 894)
---------------------------------------

Vector Time (GMT): 2020/278/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937074
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6665967
16                 A    =         6804732
90  meter
 Y    =        1294705
57  meter          E    =           
0013163
 Z    =         337110
46                 I    =           51
74855
 XDOT =       -605
258861                 Wp   =           53
03356
 YDOT =      -4719
502724  meter/sec      RA   =          166
76547  deg
 ZDOT =       6003
120567                 TA   =          310
58644
                                          MA   =          310
70092
                                          Ha   =            229
720  n
mi
                                          Hp   =            222
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21869971
01                 X    =        -6681587
04
 Y    =        4247721
70  feet           Y    =         1220074
64  meter
 Z    =        1106005
45                 Z    =          304691
15
 XDOT =      -1985
757417                 XDOT =        -581
599268
 YDOT =     -15483
932820  feet/sec       YDOT =       -4726
138447  meter/sec
 ZDOT =      19695
277450                 ZDOT =        6000
238200

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22235173
99                 X    =         6777281
03
 Y    =        1498245
99  feet           Y    =          456665
38  meter
 Z    =         956198
81                 Z    =          291449
40
 XDOT =      -1807
389897                 XDOT =        -550
892441
 YDOT =      13888
160867  feet/sec       YDOT =        4233
111432  meter/sec
 ZDOT =      19681
943781                 ZDOT =        5999
056464


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   20278
48757445  
00016717  00000-0  10270-3 0  9088
2 25544  51
6426 167
6545 0001102 109
3580 250
7689 15
48832660  8952


Satellite: ISS
Catalog Number: 25544
Epoch time:      20278
48757445   =   yrday
fracday
Element set:     908
Inclination:       51
6426  deg
RA of node:       167
6545  deg
Eccentricity:     
0001102     
Arg of perigee:   109
3580  deg
Mean anomaly:     250
7689  deg
Mean motion:   15
48832660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             895
Checksum:              334


Coasting Arc #10 (Orbit 909)
---------------------------------------

Vector Time (GMT): 2020/279/10:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937074
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6525663
17                 A    =         6804732
31  meter
 Y    =       -1882614
20  meter          E    =           
0012600
 Z    =        -313081
09                 I    =           51
78153
 XDOT =       1055
789730                 Wp   =          135
17536
 YDOT =       4632
861572  meter/sec      RA   =          161
82725  deg
 ZDOT =      -6008
117874                 TA   =           48
18472
                                          MA   =           48
07718
                                          Ha   =            229
759  n
mi
                                          Hp   =            222
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21409656
06                 X    =         6547750
92
 Y    =       -6176555
76  feet           Y    =        -1809516
07  meter
 Z    =       -1027168
94                 Z    =         -281327
56
 XDOT =       3463
877068                 XDOT =        1033
089824
 YDOT =      15199
677073  feet/sec       YDOT =        4644
540923  meter/sec
 ZDOT =     -19711
672814                 ZDOT =       -6003
044537

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22272192
62                 X    =        -6788564
31
 Y    =         867516
90  feet           Y    =          264419
15  meter
 Z    =        -880420
18                 Z    =         -268352
07
 XDOT =        209
576512                 XDOT =          63
878921
 YDOT =     -13994
187477  feet/sec       YDOT =       -4265
428343  meter/sec
 ZDOT =     -19688
217931                 ZDOT =       -6000
968825


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   20279
45539765  
00016717  00000-0  10270-3 0  9090
2 25544  51
6429 162
8685 0001152 115
0702 245
0567 15
48834040  9106


Satellite: ISS
Catalog Number: 25544
Epoch time:      20279
45539765   =   yrday
fracday
Element set:     909
Inclination:       51
6429  deg
RA of node:       162
8685  deg
Eccentricity:     
0001152     
Arg of perigee:   115
0702  deg
Mean anomaly:     245
0567  deg
Mean motion:   15
48834040  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             910
Checksum:              310


Coasting Arc #11 (Orbit 924)
---------------------------------------

Vector Time (GMT): 2020/280/09:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 937074
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3560387
14                 A    =         6799251
89  meter
 Y    =        4569798
77  meter          E    =           
0006346
 Z    =       -3566099
78                 I    =           51
79474
 XDOT =      -6077
711064                 Wp   =          100
83191
 YDOT =      -1242
514814  meter/sec      RA   =          156
90279  deg
 ZDOT =       4481
367260                 TA   =          217
32324
                                          MA   =          217
36735
                                          Ha   =            229
648  n
mi
                                          Hp   =            222
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11681060
18                 X    =        -3593900
95
 Y    =       14992778
13  feet           Y    =         4529796
46  meter
 Z    =      -11699802
42                 Z    =        -3583476
67
 XDOT =     -19939
996930                 XDOT =       -6085
133560
 YDOT =      -4076
492173  feet/sec       YDOT =       -1310
521481  meter/sec
 ZDOT =      14702
648490                 ZDOT =        4451
825510

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15235626
61                 X    =         4643818
99
 Y    =      -11279200
81  feet           Y    =        -3437900
41  meter
 Z    =      -11780120
98                 Z    =        -3590580
87
 XDOT =      17358
102124                 XDOT =        5290
749527
 YDOT =       8252
965934  feet/sec       YDOT =        2515
504017  meter/sec
 ZDOT =      14566
100273                 ZDOT =        4439
747363


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   20280
42321805  
00016717  00000-0  10270-3 0  9105
2 25544  51
6425 158
0825 0001108 117
3371 242
7892 15
48863180  9251


Satellite: ISS
Catalog Number: 25544
Epoch time:      20280
42321805   =   yrday
fracday
Element set:     910
Inclination:       51
6425  deg
RA of node:       158
0825  deg
Eccentricity:     
0001108     
Arg of perigee:   117
3371  deg
Mean anomaly:     242
7892  deg
Mean motion:   15
48863180  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             925
Checksum:              290


Coasting Arc #12 (Orbit 939)
---------------------------------------

Vector Time (GMT): 2020/281/08:17:36
280
Vector Time (MET): N/A
Weight (LBS)     : 936804
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -122172
26                 A    =         6792297
48  meter
 Y    =       -4473682
04  meter          E    =           
0004004
 Z    =        5107460
35                 I    =           51
80361
 XDOT =       7132
233707                 Wp   =           50
35852
 YDOT =      -2190
395118  meter/sec      RA   =          152
32598  deg
 ZDOT =      -1744
585671                 TA   =           56
50148
                                          MA   =           56
46323
                                          Ha   =            228
143  n
mi
                                          Hp   =            222
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -400827
63                 X    =          -96946
73
 Y    =      -14677434
51  feet           Y    =        -4474907
11  meter
 Z    =       16756759
67                 Z    =         5106928
22
 XDOT =      23399
716885                 XDOT =        7164
671648
 YDOT =      -7186
335689  feet/sec       YDOT =       -2110
456028  meter/sec
 ZDOT =      -5723
706269                 ZDOT =       -1709
860554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9051630
02                 X    =        -2758936
83
 Y    =       11564513
86  feet           Y    =         3524863
82  meter
 Z    =       16754305
55                 Z    =         5106712
33
 XDOT =     -21720
603481                 XDOT =       -6620
439941
 YDOT =      -8924
954888  feet/sec       YDOT =       -2720
326250  meter/sec
 ZDOT =      -5563
176197                 ZDOT =       -1695
656105


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   20281
39101646  
00016717  00000-0  10270-3 0  9112
2 25544  51
6415 153
2963 0001230 252
7414 107
3601 15
49333722  9404


Satellite: ISS
Catalog Number: 25544
Epoch time:      20281
39101646   =   yrday
fracday
Element set:     911
Inclination:       51
6415  deg
RA of node:       153
2963  deg
Eccentricity:     
0001230     
Arg of perigee:   252
7414  deg
Mean anomaly:     107
3601  deg
Mean motion:   15
49333722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             940
Checksum:              270


Coasting Arc #13 (Orbit 954)
---------------------------------------

Vector Time (GMT): 2020/282/08:17:36
280
Vector Time (MET): N/A
Weight (LBS)     : 936804
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         373708
19                 A    =         6792434
58  meter
 Y    =        4503090
29  meter          E    =           
0012054
 Z    =       -5082413
86                 I    =           51
83421
 XDOT =      -6917
674848                 Wp   =          106
37582
 YDOT =       2682
575979  meter/sec      RA   =          147
38839  deg
 ZDOT =       1868
516254                 TA   =          181
71815
                                          MA   =          181
72229
                                          Ha   =            228
120  n
mi
                                          Hp   =            222
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1226076
73                 X    =          348013
38
 Y    =       14773918
27  feet           Y    =         4507125
66  meter
 Z    =      -16674586
15                 Z    =        -5080660
94
 XDOT =     -22695
783623                 XDOT =       -6956
234422
 YDOT =       8801
102293  feet/sec       YDOT =        2605
001991  meter/sec
 ZDOT =       6130
302672                 ZDOT =        1834
818649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8271986
75                 X    =         2521301
56
 Y    =      -12313242
56  feet           Y    =        -3753076
33  meter
 Z    =      -16666494
57                 Z    =        -5079947
55
 XDOT =      22301
135725                 XDOT =        6797
386169
 YDOT =       6896
727159  feet/sec       YDOT =        2102
122438  meter/sec
 ZDOT =       5974
495161                 ZDOT =        1821
026125


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   20282
35853315  
00016717  00000-0  10270-3 0  9127
2 25544  51
6422 148
5071 0001174 259
1221 100
9797 15
49339436  9552


Satellite: ISS
Catalog Number: 25544
Epoch time:      20282
35853315   =   yrday
fracday
Element set:     912
Inclination:       51
6422  deg
RA of node:       148
5071  deg
Eccentricity:     
0001174     
Arg of perigee:   259
1221  deg
Mean anomaly:     100
9797  deg
Mean motion:   15
49339436  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             955
Checksum:              303


Coasting Arc #14 (Orbit 970)
---------------------------------------

Vector Time (GMT): 2020/283/08:17:36
280
Vector Time (MET): N/A
Weight (LBS)     : 936804
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -618192
15                 A    =         6792550
08  meter
 Y    =       -4512704
62  meter          E    =           
0004825
 Z    =        5036833
66                 I    =           51
86243
 XDOT =       6688
236261                 Wp   =           49
59364
 YDOT =      -3156
812023  meter/sec      RA   =          142
45477  deg
 ZDOT =      -2003
132163                 TA   =           59
84361
                                          MA   =           59
79582
                                          Ha   =            228
122  n
mi
                                          Hp   =            222
612

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2028189
48                 X    =         -592150
17
 Y    =      -14805461
34  feet           Y    =        -4519472
07  meter
 Z    =       16525044
82                 Z    =         5033893
94
 XDOT =      21943
032353                 XDOT =        6732
769802
 YDOT =     -10356
994826  feet/sec       YDOT =       -3081
770370  meter/sec
 ZDOT =      -6571
955915                 ZDOT =       -1970
534719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7447946
36                 X    =        -2270134
05
 Y    =       12972731
62  feet           Y    =         3954088
60  meter
 Z    =       16511470
97                 Z    =         5032696
35
 XDOT =     -22748
429240                 XDOT =       -6933
721232
 YDOT =      -4869
592408  feet/sec       YDOT =       -1484
251766  meter/sec
 ZDOT =      -6421
206954                 ZDOT =       -1957
183880


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   20283
39054727  
00016717  00000-0  10270-3 0  9133
2 25544  51
6421 143
4007 0001165 266
6677  93
4340 15
49355773  9712


Satellite: ISS
Catalog Number: 25544
Epoch time:      20283
39054727   =   yrday
fracday
Element set:     913
Inclination:       51
6421  deg
RA of node:       143
4007  deg
Eccentricity:     
0001165     
Arg of perigee:   266
6677  deg
Mean anomaly:      93
4340  deg
Mean motion:   15
49355773  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             971
Checksum:              309


Coasting Arc #15 (Orbit 978)
---------------------------------------

Vector Time (GMT): 2020/283/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936804
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2924852
60                 A    =         6791243
56  meter
 Y    =       -3012963
60  meter          E    =           
0001616
 Z    =        5336523
68                 I    =           51
87309
 XDOT =       5724
882145                 Wp   =          136
39735
 YDOT =      -5085
380944  meter/sec      RA   =          139
94398  deg
 ZDOT =        265
347402                 TA   =          311
07243
                                          MA   =          311
08639
                                          Ha   =            228
112  n
mi
                                          Hp   =            222
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9595973
10                 X    =        -2916865
44
 Y    =       -9885051
17  feet           Y    =        -3045626
72  meter
 Z    =       17508279
79                 Z    =         5322335
13
 XDOT =      18782
421735                 XDOT =        5780
034000
 YDOT =     -16684
320683  feet/sec       YDOT =       -5021
052833  meter/sec
 ZDOT =        870
562344                 ZDOT =         293
290930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2708543
19                 X    =         -825563
96
 Y    =      -13592405
41  feet           Y    =        -4142965
17  meter
 Z    =       17442680
61                 Z    =         5316529
05
 XDOT =      23858
011752                 XDOT =        7271
921982
 YDOT =      -3466
115374  feet/sec       YDOT =       -1056
471966  meter/sec
 ZDOT =        999
812435                 ZDOT =         304
742830


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   20283
90655146  
00016717  00000-0  10270-3 0  9143
2 25544  51
6434 140
8438 0001460 247
9940 112
1055 15
49378318  9798


Satellite: ISS
Catalog Number: 25544
Epoch time:      20283
90655146   =   yrday
fracday
Element set:     914
Inclination:       51
6434  deg
RA of node:       140
8438  deg
Eccentricity:     
0001460     
Arg of perigee:   247
9940  deg
Mean anomaly:     112
1055  deg
Mean motion:   15
49378318  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             979
Checksum:              315


Coasting Arc #16 (Orbit 993)
---------------------------------------

Vector Time (GMT): 2020/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936804
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3066671
43                 A    =         6791343
20  meter
 Y    =        2866599
50  meter          E    =           
0013397
 Z    =       -5350146
85                 I    =           51
89752
 XDOT =      -5339
921116                 Wp   =           90
73583
 YDOT =       5477
661852  meter/sec      RA   =          135
01248  deg
 ZDOT =       -126
328920                 TA   =          178
06444
                                          MA   =          178
05925
                                          Ha   =            228
026  n
mi
                                          Hp   =            222
833

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10061257
96                 X    =         3060376
50
 Y    =        9404854
00  feet           Y    =         2900857
97  meter
 Z    =      -17552975
22                 Z    =        -5335265
35
 XDOT =     -17519
426235                 XDOT =       -5400
163469
 YDOT =      17971
331534  feet/sec       YDOT =        5417
610186  meter/sec
 ZDOT =       -414
464961                 ZDOT =        -152
414759

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3591953
55                 X    =         1094827
44
 Y    =       13386148
37  feet           Y    =         4080098
02  meter
 Z    =      -17484165
15                 Z    =        -5329173
54
 XDOT =     -23427
696771                 XDOT =       -7140
761976
 YDOT =       5589
354579  feet/sec       YDOT =        1703
635276  meter/sec
 ZDOT =       -535
149630                 ZDOT =        -163
113607


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   20284
87406170  
00016717  00000-0  10270-3 0  9152
2 25544  51
6428 136
0565 0001481 253
7132 106
3855 15
49340325  9947


Satellite: ISS
Catalog Number: 25544
Epoch time:      20284
87406170   =   yrday
fracday
Element set:     915
Inclination:       51
6428  deg
RA of node:       136
0565  deg
Eccentricity:     
0001481     
Arg of perigee:   253
7132  deg
Mean anomaly:     106
3855  deg
Mean motion:   15
49340325  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             994
Checksum:              303


Coasting Arc #17 (Orbit 1009)
---------------------------------------

Vector Time (GMT): 2020/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936804
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3194865
65                 A    =         6791186
58  meter
 Y    =       -2707833
05  meter          E    =           
0000992
 Z    =        5345282
67                 I    =           51
92152
 XDOT =       4941
292197                 Wp   =          109
37629
 YDOT =      -5855
618528  meter/sec      RA   =          130
08171  deg
 ZDOT =        -13
278069                 TA   =          340
74797
                                          MA   =          340
75172
                                          Ha   =            228
053  n
mi
                                          Hp   =            222
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10481842
70                 X    =        -3190312
89
 Y    =       -8883966
71  feet           Y    =        -2743534
74  meter
 Z    =       17537016
63                 Z    =         5329774
29
 XDOT =      16211
588574                 XDOT =        5006
468740
 YDOT =     -19211
346878  feet/sec       YDOT =       -5799
997030  meter/sec
 ZDOT =        -43
563218                 ZDOT =          10
883399

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4451431
05                 X    =        -1356796
19
 Y    =      -13095376
23  feet           Y    =        -3991470
68  meter
 Z    =       17465300
63                 Z    =         5323423
63
 XDOT =      22873
040240                 XDOT =        6971
702665
 YDOT =      -7682
676451  feet/sec       YDOT =       -2341
679782  meter/sec
 ZDOT =         68
243835                 ZDOT =          20
800721


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   20285
90606598  
00016717  00000-0  10270-3 0  9164
2 25544  51
6437 130
9489 0001501 259
3738 100
7243 15
49387251 10100


Satellite: ISS
Catalog Number: 25544
Epoch time:      20285
90606598   =   yrday
fracday
Element set:     916
Inclination:       51
6437  deg
RA of node:       130
9489  deg
Eccentricity:     
0001501     
Arg of perigee:   259
3738  deg
Mean anomaly:     100
7243  deg
Mean motion:   15
49387251  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1010
Checksum:              308


Coasting Arc #18 (Orbit 1024)
---------------------------------------

Vector Time (GMT): 2020/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936804
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3325169
39                 A    =         6791315
37  meter
 Y    =        2556817
18  meter          E    =           
0013418
 Z    =       -5352733
36                 I    =           51
94142
 XDOT =      -4503
366174                 Wp   =           91
52078
 YDOT =       6183
105064  meter/sec      RA   =          125
15273  deg
 ZDOT =        155
914351                 TA   =          179
96235
                                          MA   =          179
96225
                                          Ha   =            228
009  n
mi
                                          Hp   =            222
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10909348
41                 X    =         3322331
84
 Y    =        8388507
81  feet           Y    =         2593985
50  meter
 Z    =      -17561461
16                 Z    =        -5336587
90
 XDOT =     -14774
823407                 XDOT =       -4572
930168
 YDOT =      20285
777769  feet/sec       YDOT =        6132
356243  meter/sec
 ZDOT =        511
530024                 ZDOT =         133
869386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5295174
73                 X    =         1613969
26
 Y    =       12804650
62  feet           Y    =         3902857
51  meter
 Z    =      -17486792
48                 Z    =        -5329974
35
 XDOT =     -22056
800260                 XDOT =       -6722
912719
 YDOT =       9680
532022  feet/sec       YDOT =        2950
626160  meter/sec
 ZDOT =        409
493313                 ZDOT =         124
813562


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   20286
87356795  
00016717  00000-0  10270-3 0  9173
2 25544  51
6428 126
1611 0001411 268
5360  91
5629 15
49348595 10256


Satellite: ISS
Catalog Number: 25544
Epoch time:      20286
87356795   =   yrday
fracday
Element set:     917
Inclination:       51
6428  deg
RA of node:       126
1611  deg
Eccentricity:     
0001411     
Arg of perigee:   268
5360  deg
Mean anomaly:      91
5629  deg
Mean motion:   15
49348595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1025
Checksum:              323
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