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

 
Date: August 2nd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19965 9774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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


216/18:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 8
000/00:00:00 000 0 0 0 0 220 9

218/16:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 4
000/00:00:00 000 0 0 0 0 221 2

220/06:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 2
000/00:00:00 000 0 0 0 0 221 4

227/05:42:47 315 0 3 1 8 1 8
N/A 1 7 0 0 223 7
000/00:09:34 629 0 4 -0 0 222 9

227/08:44:47 258 0 6 1 8 1 8
N/A 1 7 -0 0 224 0
000/00:09:34 515 0 1 -0 0 223 6

Coasting Arc #1 (Orbit 2243)
---------------------------------------

Vector Time (GMT): 2019/214/12:08:31
897
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4523021
05                 A    =         6787850
16  meter
 Y    =        -740059
83  meter          E    =           
0008836
 Z    =        5008045
63                 I    =           51
91891
 XDOT =       3403
236619                 Wp   =          167
41438
 YDOT =      -6536
224932  meter/sec      RA   =          130
39903  deg
 ZDOT =       2098
658151                 TA   =          262
17237
                                          MA   =          262
27268
                                          Ha   =            226
068  n
mi
                                          Hp   =            220
483

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14839307
91                 X    =        -4538734
98
 Y    =       -2428017
81  feet           Y    =         -790727
57  meter
 Z    =       16430595
89                 Z    =         4986036
87
 XDOT =      11165
474471                 XDOT =        3465
879793
 YDOT =     -21444
307520  feet/sec       YDOT =       -6497
817406  meter/sec
 ZDOT =       6885
361387                 ZDOT =        2115
341131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8209254
00                 X    =         2502180
62
 Y    =       12727435
60  feet           Y    =         3879322
37  meter
 Z    =       16330503
45                 Z    =         4977537
45
 XDOT =     -22443
164095                 XDOT =       -6840
676416
 YDOT =       5504
861154  feet/sec       YDOT =        1677
881680  meter/sec
 ZDOT =       6961
739213                 ZDOT =        2121
938112


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   19214
55795705  
00016717  00000-0  10270-3 0  9007
2 25544  51
6429 131
2149 0006170 211
9520 148
1257 15
51041972 22449


Satellite: ISS
Catalog Number: 25544
Epoch time:      19214
55795705   =   yrday
fracday
Element set:     900
Inclination:       51
6429  deg
RA of node:       131
2149  deg
Eccentricity:     
0006170     
Arg of perigee:   211
9520  deg
Mean anomaly:     148
1257  deg
Mean motion:   15
51041972  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2244
Checksum:              290


Coasting Arc #2 (Orbit 2258)
---------------------------------------

Vector Time (GMT): 2019/215/12:08:31
897
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4206634
48                 A    =         6786981
40  meter
 Y    =        1130051
37  meter          E    =           
0010472
 Z    =       -5213138
31                 I    =           51
93715
 XDOT =      -3466
181343                 Wp   =          103
40886
 YDOT =       6691
816227  meter/sec      RA   =          125
45265  deg
 ZDOT =      -1351
018430                 TA   =          153
66671
                                          MA   =          153
61344
                                          Ha   =            225
876  n
mi
                                          Hp   =            220
727

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13801294
21                 X    =         4219007
18
 Y    =        3707517
60  feet           Y    =         1177162
24  meter
 Z    =      -17103472
15                 Z    =        -5192674
47
 XDOT =     -11371
986034                 XDOT =       -3534
191209
 YDOT =      21954
777648  feet/sec       YDOT =        6652
674723  meter/sec
 ZDOT =      -4432
475163                 ZDOT =       -1368
020413

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6786471
83                 X    =        -2068516
62
 Y    =      -12701938
96  feet           Y    =        -3871551
00  meter
 Z    =      -17010429
59                 Z    =        -5184778
94
 XDOT =      22862
030760                 XDOT =        6968
346976
 YDOT =      -6195
137111  feet/sec       YDOT =       -1888
277792  meter/sec
 ZDOT =      -4510
326391                 ZDOT =       -1374
747484


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   19215
52442198  
00016717  00000-0  10270-3 0  9011
2 25544  51
6433 126
4199 0005988 215
1914 144
8843 15
51040774 22593


Satellite: ISS
Catalog Number: 25544
Epoch time:      19215
52442198   =   yrday
fracday
Element set:     901
Inclination:       51
6433  deg
RA of node:       126
4199  deg
Eccentricity:     
0005988     
Arg of perigee:   215
1914  deg
Mean anomaly:     144
8843  deg
Mean motion:   15
51040774  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2259
Checksum:              318


Coasting Arc #3 (Orbit 2274)
---------------------------------------

Vector Time (GMT): 2019/216/12:08:31
897
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3928715
75                 A    =         6786440
00  meter
 Y    =       -1532065
53  meter          E    =           
0006111
 Z    =        5318954
77                 I    =           51
95343
 XDOT =       3468
888827                 Wp   =          192
49033
 YDOT =      -6806
172522  meter/sec      RA   =          120
50751  deg
 ZDOT =        596
090168                 TA   =          251
80720
                                          MA   =          251
87373
                                          Ha   =            225
766  n
mi
                                          Hp   =            220
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12889487
38                 X    =        -3937127
78
 Y    =       -5026461
73  feet           Y    =        -1576046
29  meter
 Z    =       17450639
02                 Z    =         5299850
48
 XDOT =      11380
868854                 XDOT =        3541
844176
 YDOT =     -22329
962344  feet/sec       YDOT =       -6766
973057  meter/sec
 ZDOT =       1955
676405                 ZDOT =         613
117502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5423513
68                 X    =         1653086
97
 Y    =       12845726
31  feet           Y    =         3915377
38  meter
 Z    =       17363807
75                 Z    =         5292488
60
 XDOT =     -23020
637944                 XDOT =       -7016
690445
 YDOT =       6945
153511  feet/sec       YDOT =        2116
882790  meter/sec
 ZDOT =       2033
663511                 ZDOT =         619
860638


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   19216
55531431  
00016717  00000-0  10270-3 0  9025
2 25544  51
6428 121
3056 0006178 220
0454 140
0242 15
51055498 22757


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
55531431   =   yrday
fracday
Element set:     902
Inclination:       51
6428  deg
RA of node:       121
3056  deg
Eccentricity:     
0006178     
Arg of perigee:   220
0454  deg
Mean anomaly:     140
0242  deg
Mean motion:   15
51055498  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2275
Checksum:              276


Coasting Arc #4 (Orbit 2278)
---------------------------------------

Vector Time (GMT): 2019/216/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3803012
16                 A    =         6798138
74  meter
 Y    =        5581692
43  meter          E    =           
0007213
 Z    =         748550
60                 I    =           51
99243
 XDOT =      -3546
444480                 Wp   =           65
20547
 YDOT =      -3223
398446  meter/sec      RA   =          119
29929  deg
 ZDOT =       5975
963647                 TA   =          302
83093
                                          MA   =          302
90036
                                          Ha   =            225
771  n
mi
                                          Hp   =            220
850

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12477074
01                 X    =        -3868781
58
 Y    =       18312639
20  feet           Y    =         5538796
72  meter
 Z    =        2455874
66                 Z    =          729917
65
 XDOT =     -11635
316537                 XDOT =       -3539
163299
 YDOT =     -10575
454219  feet/sec       YDOT =       -3263
016628  meter/sec
 ZDOT =      19606
179944                 ZDOT =        5958
754327

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3016162
99                 X    =         -919326
48
 Y    =      -21962334
82  feet           Y    =        -6694119
65  meter
 Z    =        2370666
66                 Z    =          722579
20
 XDOT =      14218
537061                 XDOT =        4333
810096
 YDOT =        170
684567  feet/sec       YDOT =          52
024656  meter/sec
 ZDOT =      19528
095730                 ZDOT =        5952
163579


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   19216
81303731  
00016717  00000-0  10270-3 0  9035
2 25544  51
6389 120
0223 0006359 219
1229 140
9463 15
51026663 22795


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
81303731   =   yrday
fracday
Element set:     903
Inclination:       51
6389  deg
RA of node:       120
0223  deg
Eccentricity:     
0006359     
Arg of perigee:   219
1229  deg
Mean anomaly:     140
9463  deg
Mean motion:   15
51026663  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2279
Checksum:              294


Coasting Arc #5 (Orbit 2293)
---------------------------------------

Vector Time (GMT): 2019/217/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952577
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3718363
99                 A    =         6797404
00  meter
 Y    =       -5498146
68  meter          E    =           
0011249
 Z    =       -1432306
06                 I    =           52
00678
 XDOT =       3296
774172                 Wp   =          175
05853
 YDOT =       3742
404282  meter/sec      RA   =          114
36652  deg
 ZDOT =      -5821
474714                 TA   =           20
46635
                                          MA   =           20
42132
                                          Ha   =            225
552  n
mi
                                          Hp   =            220
912

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12199356
92                 X    =         3786526
74
 Y    =      -18038538
98  feet           Y    =        -5456184
19  meter
 Z    =       -4699166
87                 Z    =        -1414078
39
 XDOT =      10816
188229                 XDOT =        3282
957600
 YDOT =      12278
229272  feet/sec       YDOT =        3779
193926  meter/sec
 ZDOT =     -19099
326488                 ZDOT =       -5805
493972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3398007
08                 X    =         1035712
56
 Y    =       21527734
33  feet           Y    =         6561653
42  meter
 Z    =       -4615795
62                 Z    =        -1406894
51
 XDOT =     -14810
199903                 XDOT =       -4514
148931
 YDOT =      -1731
666262  feet/sec       YDOT =        -527
811877  meter/sec
 ZDOT =     -19026
873841                 ZDOT =       -5799
391147


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   19217
77949514  
00016717  00000-0  10270-3 0  9047
2 25544  51
6399 115
2267 0006119 223
6999 136
3668 15
51068141 22948


Satellite: ISS
Catalog Number: 25544
Epoch time:      19217
77949514   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:       115
2267  deg
Eccentricity:     
0006119     
Arg of perigee:   223
6999  deg
Mean anomaly:     136
3668  deg
Mean motion:   15
51068141  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2294
Checksum:              339


Coasting Arc #6 (Orbit 2307)
---------------------------------------

Vector Time (GMT): 2019/218/16:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -452472
17                 A    =         6796233
49  meter
 Y    =        6404651
43  meter          E    =           
0000526
 Z    =       -2227239
15                 I    =           52
01411
 XDOT =      -5111
019620                 Wp   =          298
90770
 YDOT =       1548
201728  meter/sec      RA   =          109
75782  deg
 ZDOT =       5489
602482                 TA   =           36
52158
                                          MA   =           36
51800
                                          Ha   =            225
371  n
mi
                                          Hp   =            221
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1484488
75                 X    =         -513238
62
 Y    =       21012635
93  feet           Y    =         6399251
84  meter
 Z    =       -7307215
05                 Z    =        -2229584
55
 XDOT =     -16768
437072                 XDOT =       -5154
617352
 YDOT =       5079
401996  feet/sec       YDOT =        1490
802850  meter/sec
 ZDOT =      18010
506831                 ZDOT =        5464
669466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5046621
65                 X    =        -1538210
28
 Y    =      -20447563
52  feet           Y    =        -6232417
36  meter
 Z    =       -7318382
56                 Z    =        -2230643
01
 XDOT =      13041
585185                 XDOT =        3975
075164
 YDOT =      -9625
101613  feet/sec       YDOT =       -2933
730972  meter/sec
 ZDOT =      17896
904797                 ZDOT =        5454
976582


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   19218
68152018  
00016717  00000-0  10270-3 0  9054
2 25544  51
6395 110
7521 0006203 227
9580 132
1044 15
51034662 23083


Satellite: ISS
Catalog Number: 25544
Epoch time:      19218
68152018   =   yrday
fracday
Element set:     905
Inclination:       51
6395  deg
RA of node:       110
7521  deg
Eccentricity:     
0006203     
Arg of perigee:   227
9580  deg
Mean anomaly:     132
1044  deg
Mean motion:   15
51034662  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2308
Checksum:              281


Coasting Arc #7 (Orbit 2323)
---------------------------------------

Vector Time (GMT): 2019/219/16:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         470767
13                 A    =         6797134
39  meter
 Y    =       -6586821
97  meter          E    =           
0012385
 Z    =        1576390
66                 I    =           52
02787
 XDOT =       4935
929973                 Wp   =          143
91455
 YDOT =      -1032
499112  meter/sec      RA   =          104
82605  deg
 ZDOT =      -5774
993669                 TA   =           18
95526
                                          MA   =           18
90921
                                          Ha   =            225
078  n
mi
                                          Hp   =            221
289

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1544511
57                 X    =          536730
71
 Y    =      -21610308
31  feet           Y    =        -6581188
75  meter
 Z    =        5171885
37                 Z    =         1578837
46
 XDOT =      16193
995976                 XDOT =        4975
160299
 YDOT =      -3387
464277  feet/sec       YDOT =        -977
082540  meter/sec
 ZDOT =     -18946
829623                 ZDOT =       -5750
921726

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5519388
14                 X    =         1682309
51
 Y    =       20947710
07  feet           Y    =         6384862
03  meter
 Z    =        5183544
82                 Z    =         1579944
46
 XDOT =     -12837
157449                 XDOT =       -3912
765590
 YDOT =       8054
424075  feet/sec       YDOT =        2454
988458  meter/sec
 ZDOT =     -18837
177750                 ZDOT =       -5741
571778


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   19219
71240285  
00016717  00000-0  10270-3 0  9064
2 25544  51
6396 105
6372 0006212 234
2067 125
8507 15
51086481 23249


Satellite: ISS
Catalog Number: 25544
Epoch time:      19219
71240285   =   yrday
fracday
Element set:     906
Inclination:       51
6396  deg
RA of node:       105
6372  deg
Eccentricity:     
0006212     
Arg of perigee:   234
2067  deg
Mean anomaly:     125
8507  deg
Mean motion:   15
51086481  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2324
Checksum:              297


Coasting Arc #8 (Orbit 2332)
---------------------------------------

Vector Time (GMT): 2019/220/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4103635
17                 A    =         6790773
76  meter
 Y    =       -3344974
53  meter          E    =           
0002772
 Z    =       -4254521
89                 I    =           52
01139
 XDOT =       1540
522078                 Wp   =          106
63054
 YDOT =       6547
815999  meter/sec      RA   =          101
94257  deg
 ZDOT =      -3664
854669                 TA   =          126
00640
                                          MA   =          125
98070
                                          Ha   =            225
190  n
mi
                                          Hp   =            221
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13463369
99                 X    =         4161400
58
 Y    =      -10974325
89  feet           Y    =        -3298761
64  meter
 Z    =      -13958405
14                 Z    =        -4234447
97
 XDOT =       5054
206294                 XDOT =        1484
989703
 YDOT =      21482
335956  feet/sec       YDOT =        6564
732850  meter/sec
 ZDOT =     -12023
801407                 ZDOT =       -3657
506060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -481933
80                 X    =         -146893
42
 Y    =      -17436052
97  feet           Y    =        -5314508
95  meter
 Z    =      -13866759
93                 Z    =        -4226588
43
 XDOT =      18911
306384                 XDOT =        5764
166186
 YDOT =       9006
342714  feet/sec       YDOT =        2745
133259  meter/sec
 ZDOT =     -11990
879791                 ZDOT =       -3654
820160


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   19220
29227698  
00016717  00000-0  10270-3 0  9073
2 25544  51
6400 102
7619 0006018 234
2826 125
7765 15
51041346 23330


Satellite: ISS
Catalog Number: 25544
Epoch time:      19220
29227698   =   yrday
fracday
Element set:     907
Inclination:       51
6400  deg
RA of node:       102
7619  deg
Eccentricity:     
0006018     
Arg of perigee:   234
2826  deg
Mean anomaly:     125
7765  deg
Mean motion:   15
51041346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2333
Checksum:              297


Coasting Arc #9 (Orbit 2348)
---------------------------------------

Vector Time (GMT): 2019/221/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4004875
41                 A    =         6789241
08  meter
 Y    =        2934503
38  meter          E    =           
0007138
 Z    =        4631987
17                 I    =           52
01380
 XDOT =      -1532
313728                 Wp   =          160
35481
 YDOT =      -6871
856853  meter/sec      RA   =           97
00487  deg
 ZDOT =       3020
785145                 TA   =          259
58717
                                          MA   =          259
66762
                                          Ha   =            224
895  n
mi
                                          Hp   =            221
468

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13139355
03                 X    =        -4059891
64
 Y    =        9627635
76  feet           Y    =         2889410
18  meter
 Z    =       15196808
29                 Z    =         4612399
70
 XDOT =      -5027
276010                 XDOT =       -1470
029923
 YDOT =     -22545
462115  feet/sec       YDOT =       -6888
644180  meter/sec
 ZDOT =       9910
712419                 ZDOT =        3013
492699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -114340
35                 X    =          -34850
94
 Y    =       16371636
09  feet           Y    =         4990074
68  meter
 Z    =       15107397
56                 Z    =         4604734
78
 XDOT =     -19971
376917                 XDOT =       -6087
275684
 YDOT =      -9278
783595  feet/sec       YDOT =       -2828
173240  meter/sec
 ZDOT =       9878
087689                 ZDOT =        3010
841127


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   19221
32315546  
00016717  00000-0  10270-3 0  9089
2 25544  51
6413  97
6476 0006232 238
7782 121
2759 15
51083630 23498


Satellite: ISS
Catalog Number: 25544
Epoch time:      19221
32315546   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:        97
6476  deg
Eccentricity:     
0006232     
Arg of perigee:   238
7782  deg
Mean anomaly:     121
2759  deg
Mean motion:   15
51083630  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2349
Checksum:              311


Coasting Arc #10 (Orbit 2363)
---------------------------------------

Vector Time (GMT): 2019/222/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3952656
02                 A    =         6788085
20  meter
 Y    =       -2461956
07  meter          E    =           
0006302
 Z    =       -4944625
46                 I    =           52
01268
 XDOT =       1550
991188                 Wp   =           83
10414
 YDOT =       7133
713357  meter/sec      RA   =           92
06443  deg
 ZDOT =      -2313
864674                 TA   =          164
36407
                                          MA   =          164
34460
                                          Ha   =            224
774  n
mi
                                          Hp   =            221
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12968031
56                 X    =         4003910
51
 Y    =       -8077283
70  feet           Y    =        -2417467
79  meter
 Z    =      -16222524
48                 Z    =        -4925300
84
 XDOT =       5088
553765                 XDOT =        1482
344016
 YDOT =      23404
571382  feet/sec       YDOT =        7150
673954  meter/sec
 ZDOT =      -7591
419535                 ZDOT =       -2306
496886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1000471
88                 X    =          304943
83
 Y    =      -15338345
54  feet           Y    =        -4675127
72  meter
 Z    =      -16134338
14                 Z    =        -4917746
26
 XDOT =      20929
899877                 XDOT =        6379
433482
 YDOT =       9309
728373  feet/sec       YDOT =        2837
605208  meter/sec
 ZDOT =      -7558
488314                 ZDOT =       -2303
827238


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   19222
28960440  
00016717  00000-0  10270-3 0  9095
2 25544  51
6414  92
8517 0005986 243
0463 117
0077 15
51050264 23642


Satellite: ISS
Catalog Number: 25544
Epoch time:      19222
28960440   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:        92
8517  deg
Eccentricity:     
0005986     
Arg of perigee:   243
0463  deg
Mean anomaly:     117
0077  deg
Mean motion:   15
51050264  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2364
Checksum:              301


Coasting Arc #11 (Orbit 2379)
---------------------------------------

Vector Time (GMT): 2019/223/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3939001
50                 A    =         6787052
38  meter
 Y    =        1976923
13  meter          E    =           
0005415
 Z    =        5164046
41                 I    =           52
00961
 XDOT =      -1601
523970                 Wp   =          197
96220
 YDOT =      -7324
002690  meter/sec      RA   =           87
12502  deg
 ZDOT =       1577
637587                 TA   =          236
86536
                                          MA   =          236
91733
                                          Ha   =            224
505  n
mi
                                          Hp   =            221
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12923233
26                 X    =        -3985898
95
 Y    =        6485968
26  feet           Y    =         1932611
86  meter
 Z    =       16942409
47                 Z    =         5144798
74
 XDOT =      -5254
343733                 XDOT =       -1527
169006
 YDOT =     -24028
880217  feet/sec       YDOT =       -7341
496423  meter/sec
 ZDOT =       5175
976335                 ZDOT =        1570
038181

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2026046
86                 X    =         -617539
08
 Y    =       14420138
34  feet           Y    =         4395258
17  meter
 Z    =       16854605
46                 Z    =         5137283
75
 XDOT =     -21754
511553                 XDOT =       -6630
775121
 YDOT =      -9084
262309  feet/sec       YDOT =       -2768
883152  meter/sec
 ZDOT =       5142
020395                 ZDOT =        1567
287816


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   19223
32047931  
00016717  00000-0  10270-3 0  9104
2 25544  51
6414  87
7380 0006127 247
5453 112
5049 15
51081826 23804


Satellite: ISS
Catalog Number: 25544
Epoch time:      19223
32047931   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:        87
7380  deg
Eccentricity:     
0006127     
Arg of perigee:   247
5453  deg
Mean anomaly:     112
5049  deg
Mean motion:   15
51081826  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2380
Checksum:              292


Coasting Arc #12 (Orbit 2394)
---------------------------------------

Vector Time (GMT): 2019/224/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3982293
38                 A    =         6786529
49  meter
 Y    =       -1460825
28  meter          E    =           
0008717
 Z    =       -5305026
69                 I    =           52
00511
 XDOT =       1655
536699                 Wp   =           92
76773
 YDOT =       7432
621670  meter/sec      RA   =           82
18267  deg
 ZDOT =       -805
489403                 TA   =          169
57043
                                          MA   =          169
55234
                                          Ha   =            224
369  n
mi
                                          Hp   =            221
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13065267
00                 X    =         4024101
17
 Y    =       -4792733
86  feet           Y    =        -1416058
37  meter
 Z    =      -17404943
20                 Z    =        -5285581
11
 XDOT =       5431
550851                 XDOT =        1576
212490
 YDOT =      24385
241701  feet/sec       YDOT =        7450
691569  meter/sec
 ZDOT =      -2642
681769                 ZDOT =        -797
639748

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3270232
52                 X    =          996766
87
 Y    =      -13640223
84  feet           Y    =        -4157540
23  meter
 Z    =      -17316276
17                 Z    =        -5278000
98
 XDOT =      22352
541427                 XDOT =        6813
054627
 YDOT =       8662
882053  feet/sec       YDOT =        2640
446450  meter/sec
 ZDOT =      -2607
607810                 ZDOT =        -794
798861


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   19224
28692507  
00016717  00000-0  10270-3 0  9116
2 25544  51
6418  82
9422 0006068 250
9964 109
0530 15
51053602 23954


Satellite: ISS
Catalog Number: 25544
Epoch time:      19224
28692507   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:        82
9422  deg
Eccentricity:     
0006068     
Arg of perigee:   250
9964  deg
Mean anomaly:     109
0530  deg
Mean motion:   15
51053602  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2395
Checksum:              304


Coasting Arc #13 (Orbit 2410)
---------------------------------------

Vector Time (GMT): 2019/225/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4070064
62                 A    =         6786232
15  meter
 Y    =         950738
69  meter          E    =           
0003866
 Z    =        5349429
16                 I    =           51
99931
 XDOT =      -1710
516050                 Wp   =          246
72078
 YDOT =      -7467
826113  meter/sec      RA   =           77
24105  deg
 ZDOT =         24
332950                 TA   =          203
03961
                                          MA   =          203
05695
                                          Ha   =            224
113  n
mi
                                          Hp   =            221
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13353230
37                 X    =        -4106377
55
 Y    =        3119221
42  feet           Y    =          905021
04  meter
 Z    =       17550620
60                 Z    =         5329570
59
 XDOT =      -5611
929298                 XDOT =       -1626
999734
 YDOT =     -24500
741842  feet/sec       YDOT =       -7486
487339  meter/sec
 ZDOT =         79
832513                 ZDOT =          16
226522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4602007
82                 X    =        -1402691
98
 Y    =       13039498
91  feet           Y    =         3974439
27  meter
 Z    =       17460113
96                 Z    =         5321842
73
 XDOT =     -22731
176214                 XDOT =       -6928
462510
 YDOT =      -8087
358641  feet/sec       YDOT =       -2465
026914  meter/sec
 ZDOT =         43
602785                 ZDOT =          13
290129


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   19225
31779532  
00016717  00000-0  10270-3 0  9126
2 25544  51
6423  77
8281 0006151 256
1285 103
9182 15
51082947 24112


Satellite: ISS
Catalog Number: 25544
Epoch time:      19225
31779532   =   yrday
fracday
Element set:     912
Inclination:       51
6423  deg
RA of node:        77
8281  deg
Eccentricity:     
0006151     
Arg of perigee:   256
1285  deg
Mean anomaly:     103
9182  deg
Mean motion:   15
51082947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2411
Checksum:              302


Coasting Arc #14 (Orbit 2425)
---------------------------------------

Vector Time (GMT): 2019/226/06:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937301
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4213882
92                 A    =         6786505
01  meter
 Y    =        -443231
75  meter          E    =           
0008943
 Z    =       -5308927
77                 I    =           51
99109
 XDOT =       1742
222200                 Wp   =          106
55381
 YDOT =       7417
171573  meter/sec      RA   =           72
29719  deg
 ZDOT =        762
203130                 TA   =          170
71241
                                          MA   =          170
69586
                                          Ha   =            223
895  n
mi
                                          Hp   =            221
886

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13825075
21                 X    =         4244313
31
 Y    =       -1454172
41  feet           Y    =         -395938
81  meter
 Z    =      -17417742
04                 Z    =        -5288384
89
 XDOT =       5715
952101                 XDOT =        1655
449495
 YDOT =      24334
552406  feet/sec       YDOT =        7436
169123  meter/sec
 ZDOT =       2500
666438                 ZDOT =         770
455516

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6042835
42                 X    =         1841856
24
 Y    =      -12648421
49  feet           Y    =        -3855238
87  meter
 Z    =      -17324163
29                 Z    =        -5280404
97
 XDOT =      22804
774114                 XDOT =        6950
895150
 YDOT =       7413
066172  feet/sec       YDOT =        2259
502569  meter/sec
 ZDOT =       2537
556391                 ZDOT =         773
447188


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   19226
28423585  
00016717  00000-0  10270-3 0  9138
2 25544  51
6419  73
0320 0005990 259
9045 100
1431 15
51058627 24264


Satellite: ISS
Catalog Number: 25544
Epoch time:      19226
28423585   =   yrday
fracday
Element set:     913
Inclination:       51
6419  deg
RA of node:        73
0320  deg
Eccentricity:     
0005990     
Arg of perigee:   259
9045  deg
Mean anomaly:     100
1431  deg
Mean motion:   15
51058627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2426
Checksum:              296


Coasting Arc #15 (Orbit 2440)
---------------------------------------

Vector Time (GMT): 2019/227/05:47:34
629
Vector Time (MET): N/A
Weight (LBS)     : 937115
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4647146
89                 A    =         6791863
02  meter
 Y    =        2589535
88  meter          E    =           
0002854
 Z    =       -4224197
74                 I    =           51
99392
 XDOT =       -359
316606                 Wp   =          180
15597
 YDOT =       6693
884121  meter/sec      RA   =           67
48071  deg
 ZDOT =       3705
439238                 TA   =          127
73385
                                          MA   =          127
70798
                                          Ha   =            223
689  n
mi
                                          Hp   =            222
883

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15246544
93                 X    =         4638362
90
 Y    =        8495852
63  feet           Y    =         2641454
51  meter
 Z    =      -13858916
47                 Z    =        -4201645
46
 XDOT =      -1178
860257                 XDOT =        -452
141381
 YDOT =      21961
562076  feet/sec       YDOT =        6689
346909  meter/sec
 ZDOT =      12156
952882                 ZDOT =        3703
468522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16437156
36                 X    =         5010045
26
 Y    =       -6106193
25  feet           Y    =        -1861167
70  meter
 Z    =      -13756471
37                 Z    =        -4192972
47
 XDOT =      15398
204135                 XDOT =        4693
372620
 YDOT =      14063
019797  feet/sec       YDOT =        4286
408434  meter/sec
 ZDOT =      12147
353301                 ZDOT =        3702
513286


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   19227
25067459  
00016717  00000-0  10270-3 0  9141
2 25544  51
6411  68
2370 0007402 268
3606  91
6697 15
50710502 24415


Satellite: ISS
Catalog Number: 25544
Epoch time:      19227
25067459   =   yrday
fracday
Element set:     914
Inclination:       51
6411  deg
RA of node:        68
2370  deg
Eccentricity:     
0007402     
Arg of perigee:   268
3606  deg
Mean anomaly:      91
6697  deg
Mean motion:   15
50710502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2441
Checksum:              300


Coasting Arc #16 (Orbit 2442)
---------------------------------------

Vector Time (GMT): 2019/227/08:49:34
515
Vector Time (MET): N/A
Weight (LBS)     : 936929
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4598658
26                 A    =         6790271
47  meter
 Y    =        1030676
00  meter          E    =           
0004193
 Z    =       -4891828
96                 I    =           51
98603
 XDOT =        992
985152                 Wp   =          147
67027
 YDOT =       7189
763086  meter/sec      RA   =           66
86390  deg
 ZDOT =       2445
832142                 TA   =          146
25457
                                          MA   =          146
22787
                                          Ha   =            224
019  n
mi
                                          Hp   =            223
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15087461
48                 X    =         4610552
39
 Y    =        3381482
93  feet           Y    =         1082168
01  meter
 Z    =      -16049307
62                 Z    =        -4869462
03
 XDOT =       3257
825303                 XDOT =         900
633137
 YDOT =      23588
461569  feet/sec       YDOT =        7200
350936  meter/sec
 ZDOT =       8024
383667                 ZDOT =        2450
431384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2048370
92                 X    =          624343
46
 Y    =      -15431321
24  feet           Y    =        -4703466
71  meter
 Z    =      -15947560
86                 Z    =        -4860816
55
 XDOT =      22096
448652                 XDOT =        6734
997549
 YDOT =      -5389
126512  feet/sec       YDOT =       -1642
605761  meter/sec
 ZDOT =       8044
651731                 ZDOT =        2452
009847


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   19227
37956152  
00016717  00000-0  10270-3 0  9152
2 25544  51
6433  67
5990 0008949 269
9492  90
0634 15
50382566 24437


Satellite: ISS
Catalog Number: 25544
Epoch time:      19227
37956152   =   yrday
fracday
Element set:     915
Inclination:       51
6433  deg
RA of node:        67
5990  deg
Eccentricity:     
0008949     
Arg of perigee:   269
9492  deg
Mean anomaly:      90
0634  deg
Mean motion:   15
50382566  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2443
Checksum:              343


Coasting Arc #17 (Orbit 2458)
---------------------------------------

Vector Time (GMT): 2019/228/08:49:34
515
Vector Time (MET): N/A
Weight (LBS)     : 936929
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4778065
69                 A    =         6790999
26  meter
 Y    =       -1176264
08  meter          E    =           
0004478
 Z    =        4683559
69                 I    =           51
97527
 XDOT =      -1141
995255                 Wp   =          339
07225
 YDOT =      -6988
710172  meter/sec      RA   =           61
92838  deg
 ZDOT =      -2917
027757                 TA   =          139
85890
                                          MA   =          139
82581
                                          Ha   =            224
894  n
mi
                                          Hp   =            224
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15676068
54                 X    =        -4787306
88
 Y    =       -3859134
11  feet           Y    =        -1229747
42  meter
 Z    =       15366009
48                 Z    =         4660327
72
 XDOT =      -3746
703593                 XDOT =       -1049
591626
 YDOT =     -22928
839146  feet/sec       YDOT =       -7000
964116  meter/sec
 ZDOT =      -9570
301041                 ZDOT =       -2922
350566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2197033
28                 X    =         -669655
74
 Y    =       16094760
88  feet           Y    =         4905683
12  meter
 Z    =       15260340
93                 Z    =         4651351
91
 XDOT =     -21248
813627                 XDOT =       -6476
638393
 YDOT =       6205
942318  feet/sec       YDOT =        1891
571219  meter/sec
 ZDOT =      -9593
874602                 ZDOT =       -2924
212979


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   19228
41088653  
00016717  00000-0  10270-3 0  9161
2 25544  51
6439  62
4871 0009063 274
4342  85
5773 15
50422030 24599


Satellite: ISS
Catalog Number: 25544
Epoch time:      19228
41088653   =   yrday
fracday
Element set:     916
Inclination:       51
6439  deg
RA of node:        62
4871  deg
Eccentricity:     
0009063     
Arg of perigee:   274
4342  deg
Mean anomaly:      85
5773  deg
Mean motion:   15
50422030  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2459
Checksum:              314


Coasting Arc #18 (Orbit 2473)
---------------------------------------

Vector Time (GMT): 2019/229/08:49:34
515
Vector Time (MET): N/A
Weight (LBS)     : 936929
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4977827
28                 A    =         6792029
93  meter
 Y    =        1288678
41  meter          E    =           
0001953
 Z    =       -4438226
81                 I    =           51
96155
 XDOT =       1253
053076                 Wp   =          195
68062
 YDOT =       6765
252310  meter/sec      RA   =           56
99137  deg
 ZDOT =       3367
575805                 TA   =          108
25969
                                          MA   =          108
23844
                                          Ha   =            225
304  n
mi
                                          Hp   =            224
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16331454
34                 X    =         4984604
97
 Y    =        4227947
53  feet           Y    =         1344381
79  meter
 Z    =      -14561111
57                 Z    =        -4414030
43
 XDOT =       4111
066521                 XDOT =        1160
951457
 YDOT =      22195
709678  feet/sec       YDOT =        6778
749925  meter/sec
 ZDOT =      11048
477051                 ZDOT =        3373
438721

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2207340
74                 X    =          672797
46
 Y    =      -16819993
74  feet           Y    =        -5126734
09  meter
 Z    =      -14451068
09                 Z    =        -4404685
55
 XDOT =      20318
069873                 XDOT =        6192
947697
 YDOT =      -6854
560379  feet/sec       YDOT =       -2089
270004  meter/sec
 ZDOT =      11074
522712                 ZDOT =        3375
514523


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   19229
37775307  
00016717  00000-0  10270-3 0  9177
2 25544  51
6437  57
6937 0009037 278
1068  81
9057 15
50390000 24746


Satellite: ISS
Catalog Number: 25544
Epoch time:      19229
37775307   =   yrday
fracday
Element set:     917
Inclination:       51
6437  deg
RA of node:        57
6937  deg
Eccentricity:     
0009037     
Arg of perigee:   278
1068  deg
Mean anomaly:      81
9057  deg
Mean motion:   15
50390000  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2474
Checksum:              327
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