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

 
Date: September 12th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13923 1181 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


257/18:31:19 752 -1 3 2 0 2 0
N/A -0 3 -0 2 229 7
000/00:00:39 505 -1 4 -0 0 218 9

259/19:12:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 218 7

268/13:57:43 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 3

268/17:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

Coasting Arc #1 (Orbit 2875)
---------------------------------------

Vector Time (GMT): 2019/255/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3617952
07                 A    =         6798018
84  meter
 Y    =       -5329881
97  meter          E    =           
0020708
 Z    =        2134218
05                 I    =           51
29088
 XDOT =       3157
238656                 Wp   =           56
51149
 YDOT =       4346
525565  meter/sec      RA   =          288
77145  deg
 ZDOT =       5475
320698                 TA   =          327
25612
                                          MA   =          327
38430
                                          Ha   =            229
077  n
mi
                                          Hp   =            218
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11869921
48                 X    =         3666916
72
 Y    =      -17486489
41  feet           Y    =        -5289149
55  meter
 Z    =        7002027
74                 Z    =         2151911
83
 XDOT =      10358
394541                 XDOT =        3081
804132
 YDOT =      14260
254477  feet/sec       YDOT =        4381
410654  meter/sec
 ZDOT =      17963
650585                 ZDOT =        5490
473671

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13135453
84                 X    =        -4003686
33
 Y    =      -16522495
80  feet           Y    =        -5036056
72  meter
 Z    =        7082917
84                 Z    =         2158873
36
 XDOT =      15470
223669                 XDOT =        4715
324174
 YDOT =      -4530
875421  feet/sec       YDOT =       -1381
010828  meter/sec
 ZDOT =      18032
195520                 ZDOT =        5496
213195


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   19255
28934544  
00016717  00000-0  10270-3 0  9008
2 25544  51
6422 289
2458 0007959  32
3376 327
8261 15
50471300 28762


Satellite: ISS
Catalog Number: 25544
Epoch time:      19255
28934544   =   yrday
fracday
Element set:     900
Inclination:       51
6422  deg
RA of node:       289
2458  deg
Eccentricity:     
0007959     
Arg of perigee:    32
3376  deg
Mean anomaly:     327
8261  deg
Mean motion:   15
50471300  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2876
Checksum:              324


Coasting Arc #2 (Orbit 2890)
---------------------------------------

Vector Time (GMT): 2019/256/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3436485
16                 A    =         6797137
89  meter
 Y    =        5264477
54  meter          E    =           
0009453
 Z    =       -2597146
56                 I    =           51
27731
 XDOT =      -3163
611877                 Wp   =           67
92070
 YDOT =      -4628
575385  meter/sec      RA   =          283
79168  deg
 ZDOT =      -5208
046880                 TA   =          141
37968
                                          MA   =          141
31203
                                          Ha   =            229
290  n
mi
                                          Hp   =            218
308

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11274557
60                 X    =        -3482483
27
 Y    =       17271907
93  feet           Y    =         5225790
92  meter
 Z    =       -8520822
03                 Z    =        -2613951
75
 XDOT =     -10379
304060                 XDOT =       -3086
321107
 YDOT =     -15185
614780  feet/sec       YDOT =       -4663
521427  meter/sec
 ZDOT =     -17086
767978                 ZDOT =       -5223
226248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13383510
87                 X    =         4079294
11
 Y    =       15652505
18  feet           Y    =         4770883
58  meter
 Z    =       -8597649
63                 Z    =        -2620563
61
 XDOT =     -16331
738102                 XDOT =       -4977
913774
 YDOT =       4562
241949  feet/sec       YDOT =        1390
571346  meter/sec
 ZDOT =     -17155
422133                 ZDOT =       -5228
972666


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   19256
25617209  
00016717  00000-0  10270-3 0  9013
2 25544  51
6413 284
4531 0008102  35
8608 324
3085 15
50451933 28911


Satellite: ISS
Catalog Number: 25544
Epoch time:      19256
25617209   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:       284
4531  deg
Eccentricity:     
0008102     
Arg of perigee:    35
8608  deg
Mean anomaly:     324
3085  deg
Mean motion:   15
50451933  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2891
Checksum:              298


Coasting Arc #3 (Orbit 2906)
---------------------------------------

Vector Time (GMT): 2019/257/05:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3230093
42                 A    =         6796129
33  meter
 Y    =       -5161039
46  meter          E    =           
0019666
 Z    =        2994044
03                 I    =           51
26744
 XDOT =       3242
693813                 Wp   =           66
91883
 YDOT =       4900
680441  meter/sec      RA   =          278
81053  deg
 ZDOT =       4930
971004                 TA   =          327
53170
                                          MA   =          327
65252
                                          Ha   =            229
199  n
mi
                                          Hp   =            218
232

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10597419
37                 X    =         3273022
26
 Y    =      -16932544
16  feet           Y    =        -5124677
95  meter
 Z    =        9822979
11                 Z    =         3009839
31
 XDOT =      10638
759229                 XDOT =        3163
700190
 YDOT =      16078
347904  feet/sec       YDOT =        4936
501343  meter/sec
 ZDOT =      16177
726392                 ZDOT =        4946
530359

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13506729
37                 X    =        -4116851
11
 Y    =      -14668358
10  feet           Y    =        -4470915
55  meter
 Z    =        9895190
74                 Z    =         3016054
14
 XDOT =      17236
829838                 XDOT =        5253
785735
 YDOT =      -4870
666418  feet/sec       YDOT =       -1484
579124  meter/sec
 ZDOT =      16248
099354                 ZDOT =        4952
420683


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   19257
28745133  
00016717  00000-0  10270-3 0  9026
2 25544  51
6415 279
3409 0007995  39
8181 320
3555 15
50474694 29074


Satellite: ISS
Catalog Number: 25544
Epoch time:      19257
28745133   =   yrday
fracday
Element set:     902
Inclination:       51
6415  deg
RA of node:       279
3409  deg
Eccentricity:     
0007995     
Arg of perigee:    39
8181  deg
Mean anomaly:     320
3555  deg
Mean motion:   15
50474694  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2907
Checksum:              334


Coasting Arc #4 (Orbit 2914)
---------------------------------------

Vector Time (GMT): 2019/257/18:31:39
505
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1197216
02                 A    =         6800970
79  meter
 Y    =        6666443
37  meter          E    =           
0012600
 Z    =        -602494
48                 I    =           51
27686
 XDOT =      -4641
417633                 Wp   =          104
04771
 YDOT =      -1360
267347  meter/sec      RA   =          276
09105  deg
 ZDOT =      -5935
976871                 TA   =           82
47340
                                          MA   =           82
33028
                                          Ha   =            229
736  n
mi
                                          Hp   =            218
926

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3927874
09                 X    =        -1268746
56
 Y    =       21871533
36  feet           Y    =         6652655
24  meter
 Z    =       -1976687
93                 Z    =         -608484
52
 XDOT =     -15227
748139                 XDOT =       -4597
028176
 YDOT =      -4462
819380  feet/sec       YDOT =       -1411
923373  meter/sec
 ZDOT =     -19474
989734                 ZDOT =       -5958
415112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21902697
56                 X    =        -6675942
22
 Y    =       -3735451
35  feet           Y    =        -1138565
57  meter
 Z    =       -2004421
25                 Z    =         -610947
60
 XDOT =       4067
978091                 XDOT =        1239
919722
 YDOT =     -13534
982765  feet/sec       YDOT =       -4125
462747  meter/sec
 ZDOT =     -19576
910519                 ZDOT =       -5967
042326


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   19257
80310003  
00016717  00000-0  10270-3 0  9039
2 25544  51
6411 276
7887 0007247  45
9053 314
2693 15
50076097 29156


Satellite: ISS
Catalog Number: 25544
Epoch time:      19257
80310003   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:       276
7887  deg
Eccentricity:     
0007247     
Arg of perigee:    45
9053  deg
Mean anomaly:     314
2693  deg
Mean motion:   15
50076097  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2915
Checksum:              309


Coasting Arc #5 (Orbit 2930)
---------------------------------------

Vector Time (GMT): 2019/258/18:31:39
505
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         886319
56                 A    =         6800769
19  meter
 Y    =       -6665828
43  meter          E    =           
0020768
 Z    =         943623
69                 I    =           51
27373
 XDOT =       4691
246439                 Wp   =           52
98312
 YDOT =       1467
787443  meter/sec      RA   =          271
11281  deg
 ZDOT =       5884
579135                 TA   =          317
27757
                                          MA   =          317
43885
                                          Ha   =            229
781  n
mi
                                          Hp   =            218
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2907872
56                 X    =          956209
30
 Y    =      -21869515
84  feet           Y    =        -6655526
10  meter
 Z    =        3095878
24                 Z    =          948099
56
 XDOT =      15391
228474                 XDOT =        4645
900494
 YDOT =       4815
575601  feet/sec       YDOT =        1519
995353  meter/sec
 ZDOT =      19306
361990                 ZDOT =        5907
257184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21935551
94                 X    =         6685956
23
 Y    =        2331005
64  feet           Y    =          710490
52  meter
 Z    =        3116710
11                 Z    =          949973
24
 XDOT =      -4257
910245                 XDOT =       -1297
811043
 YDOT =      13778
520423  feet/sec       YDOT =        4199
693025  meter/sec
 ZDOT =      19409
367687                 ZDOT =        5915
975271


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   19258
83461990  
00016717  00000-0  10270-3 0  9046
2 25544  51
6411 271
6777 0007328  49
0178 311
1606 15
50073440 29318


Satellite: ISS
Catalog Number: 25544
Epoch time:      19258
83461990   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:       271
6777  deg
Eccentricity:     
0007328     
Arg of perigee:    49
0178  deg
Mean anomaly:     311
1606  deg
Mean motion:   15
50073440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2931
Checksum:              308


Coasting Arc #6 (Orbit 2945)
---------------------------------------

Vector Time (GMT): 2019/259/18:31:39
505
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -626824
68                 A    =         6800373
87  meter
 Y    =        6638189
44  meter          E    =           
0011463
 Z    =       -1337943
87                 I    =           51
27391
 XDOT =      -4755
022749                 Wp   =          102
66164
 YDOT =      -1605
245911  meter/sec      RA   =          266
13462  deg
 ZDOT =      -5781
267657                 TA   =           91
94500
                                          MA   =           91
81371
                                          Ha   =            229
850  n
mi
                                          Hp   =            218
746

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2056511
40                 X    =         -694509
22
 Y    =       21778836
74  feet           Y    =         6630801
26  meter
 Z    =       -4389579
61                 Z    =        -1341153
84
 XDOT =     -15600
468335                 XDOT =       -4708
636677
 YDOT =      -5266
554826  feet/sec       YDOT =       -1658
161165  meter/sec
 ZDOT =     -18967
413574                 ZDOT =       -5804
253070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21845116
18                 X    =        -6658391
41
 Y    =       -1097922
29  feet           Y    =         -334646
71  meter
 Z    =       -4404638
89                 Z    =        -1342533
94
 XDOT =       4524
195320                 XDOT =        1378
974734
 YDOT =     -14089
530484  feet/sec       YDOT =       -4294
488891  meter/sec
 ZDOT =     -19071
810425                 ZDOT =       -5813
087817


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   19259
80166759  
00016717  00000-0  10270-3 0  9050
2 25544  51
6420 266
8860 0007307  53
0070 307
1748 15
50073767 29460


Satellite: ISS
Catalog Number: 25544
Epoch time:      19259
80166759   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:       266
8860  deg
Eccentricity:     
0007307     
Arg of perigee:    53
0070  deg
Mean anomaly:     307
1748  deg
Mean motion:   15
50073767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2946
Checksum:              324


Coasting Arc #7 (Orbit 2945)
---------------------------------------

Vector Time (GMT): 2019/259/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1153315
94                 A    =         6800775
82  meter
 Y    =       -6640643
84  meter          E    =           
0017314
 Z    =        -853430
99                 I    =           51
27574
 XDOT =       4635
096150                 Wp   =           44
88937
 YDOT =      -1552
536090  meter/sec      RA   =          265
97472  deg
 ZDOT =       5902
183507                 TA   =          305
84485
                                          MA   =          306
00556
                                          Ha   =            229
794  n
mi
                                          Hp   =            218
728

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3783844
96                 X    =        -1074827
11
 Y    =      -21786889
23  feet           Y    =        -6653102
26  meter
 Z    =       -2799970
44                 Z    =         -858842
08
 XDOT =      15207
008366                 XDOT =        4623
442874
 YDOT =      -5093
622343  feet/sec       YDOT =       -1500
767726  meter/sec
 ZDOT =      19364
119118                 ZDOT =        5924
671046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20447998
50                 X    =         6232549
94
 Y    =       -8410090
56  feet           Y    =        -2563395
60  meter
 Z    =       -2824109
33                 Z    =         -860788
52
 XDOT =       7634
108707                 XDOT =        2326
876334
 YDOT =      12117
887638  feet/sec       YDOT =        3693
532152  meter/sec
 ZDOT =      19466
473034                 ZDOT =        5933
380981


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   19259
80166719  
00016717  00000-0  10270-3 0  9067
2 25544  51
6423 266
8863 0007321  52
4335 307
7479 15
50091330 29462


Satellite: ISS
Catalog Number: 25544
Epoch time:      19259
80166719   =   yrday
fracday
Element set:     906
Inclination:       51
6423  deg
RA of node:       266
8863  deg
Eccentricity:     
0007321     
Arg of perigee:    52
4335  deg
Mean anomaly:     307
7479  deg
Mean motion:   15
50091330  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2946
Checksum:              323


Coasting Arc #8 (Orbit 2961)
---------------------------------------

Vector Time (GMT): 2019/260/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1416611
24                 A    =         6801090
25  meter
 Y    =        6632645
98  meter          E    =           
0016538
 Z    =         450689
89                 I    =           51
27968
 XDOT =      -4610
990229                 Wp   =          105
28215
 YDOT =       1401
576683  meter/sec      RA   =          260
99778  deg
 ZDOT =      -5953
974860                 TA   =           69
84274
                                          MA   =           69
66492
                                          Ha   =            229
899  n
mi
                                          Hp   =            218
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4647674
66                 X    =         1340148
56
 Y    =       21760649
53  feet           Y    =         6648060
04  meter
 Z    =        1478641
36                 Z    =          457384
99
 XDOT =     -15127
920700                 XDOT =       -4597
398998
 YDOT =       4598
348696  feet/sec       YDOT =        1350
088781  meter/sec
 ZDOT =     -19534
038253                 ZDOT =       -5976
340640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20070420
76                 X    =        -6117464
25
 Y    =        9602883
24  feet           Y    =         2926958
81  meter
 Z    =        1508632
52                 Z    =          459831
19
 XDOT =      -7279
696502                 XDOT =       -2218
851494
 YDOT =     -12039
484232  feet/sec       YDOT =       -3669
634794  meter/sec
 ZDOT =     -19635
826754                 ZDOT =       -5984
999995


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   19260
83318589  
00016717  00000-0  10270-3 0  9077
2 25544  51
6420 261
7759 0007255  57
3635 302
8215 15
50060351 29621


Satellite: ISS
Catalog Number: 25544
Epoch time:      19260
83318589   =   yrday
fracday
Element set:     907
Inclination:       51
6420  deg
RA of node:       261
7759  deg
Eccentricity:     
0007255     
Arg of perigee:    57
3635  deg
Mean anomaly:     302
8215  deg
Mean motion:   15
50060351  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2962
Checksum:              312


Coasting Arc #9 (Orbit 2976)
---------------------------------------

Vector Time (GMT): 2019/261/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1724641
54                 A    =         6801072
24  meter
 Y    =       -6569547
28  meter          E    =           
0018917
 Z    =        -107880
92                 I    =           51
28703
 XDOT =       4615
878271                 Wp   =           50
11234
 YDOT =      -1298
273221  meter/sec      RA   =          256
02003  deg
 ZDOT =       5979
613764                 TA   =          308
72145
                                          MA   =          308
89042
                                          Ha   =            229
817  n
mi
                                          Hp   =            218
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5658272
75                 X    =        -1650526
75
 Y    =      -21553632
82  feet           Y    =        -6588419
05  meter
 Z    =        -353940
02                 Z    =         -116078
16
 XDOT =      15143
957582                 XDOT =        4601
006902
 YDOT =      -4259
426579  feet/sec       YDOT =       -1246
737911  meter/sec
 ZDOT =      19618
155394                 ZDOT =        6002
000200

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19446463
60                 X    =         5927282
10
 Y    =      -10880384
07  feet           Y    =        -3316341
07  meter
 Z    =        -390778
42                 Z    =         -119109
26
 XDOT =       7093
410415                 XDOT =        2162
071495
 YDOT =      12045
692517  feet/sec       YDOT =        3671
527079  meter/sec
 ZDOT =      19720
031866                 ZDOT =        6010
665713


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   19261
80023220  
00016717  00000-0  10270-3 0  9081
2 25544  51
6427 256
9844 0007210  58
9060 301
2797 15
50095818 29779


Satellite: ISS
Catalog Number: 25544
Epoch time:      19261
80023220   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:       256
9844  deg
Eccentricity:     
0007210     
Arg of perigee:    58
9060  deg
Mean anomaly:     301
2797  deg
Mean motion:   15
50095818  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2977
Checksum:              314


Coasting Arc #10 (Orbit 2992)
---------------------------------------

Vector Time (GMT): 2019/262/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1977902
11                 A    =         6801149
57  meter
 Y    =        6497140
14  meter          E    =           
0015227
 Z    =        -299453
79                 I    =           51
29668
 XDOT =      -4659
300129                 Wp   =          110
09262
 YDOT =       1155
023484  meter/sec      RA   =          251
04375  deg
 ZDOT =      -5967
973318                 TA   =           73
14316
                                          MA   =           72
97622
                                          Ha   =            229
941  n
mi
                                          Hp   =            218
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6489180
15                 X    =         1906556
81
 Y    =       21316076
56  feet           Y    =         6518859
50  meter
 Z    =        -982459
94                 Z    =         -290019
43
 XDOT =     -15286
417745                 XDOT =       -4642
880200
 YDOT =       3789
447127  feet/sec       YDOT =        1103
011372  meter/sec
 ZDOT =     -19579
964953                 ZDOT =       -5990
566903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18802857
67                 X    =        -5731111
02
 Y    =       11959046
39  feet           Y    =         3645117
34  meter
 Z    =        -939978
42                 Z    =         -286505
42
 XDOT =      -6830
476158                 XDOT =       -2081
929133
 YDOT =     -12218
156417  feet/sec       YDOT =       -3724
094076  meter/sec
 ZDOT =     -19682
777479                 ZDOT =       -5999
310576


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   19262
83174813  
00016717  00000-0  10270-3 0  9091
2 25544  51
6433 251
8736 0007188  63
8273 296
3616 15
50057762 29933


Satellite: ISS
Catalog Number: 25544
Epoch time:      19262
83174813   =   yrday
fracday
Element set:     909
Inclination:       51
6433  deg
RA of node:       251
8736  deg
Eccentricity:     
0007188     
Arg of perigee:    63
8273  deg
Mean anomaly:     296
3616  deg
Mean motion:   15
50057762  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2993
Checksum:              338


Coasting Arc #11 (Orbit 3008)
---------------------------------------

Vector Time (GMT): 2019/263/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916777
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2264429
81                 A    =         6800889
89  meter
 Y    =       -6371081
29  meter          E    =           
0020233
 Z    =         642732
91                 I    =           51
30754
 XDOT =       4728
789078                 Wp   =           56
87189
 YDOT =      -1069
053282  meter/sec      RA   =          246
06719  deg
 ZDOT =       5937
926602                 TA   =          310
09188
                                          MA   =          310
26908
                                          Ha   =            229
887  n
mi
                                          Hp   =            218
506

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7429231
65                 X    =        -2196140
31
 Y    =      -20902497
66  feet           Y    =        -6396021
88  meter
 Z    =        2108703
76                 Z    =          631899
16
 XDOT =      15514
399863                 XDOT =        4711
548631
 YDOT =      -3507
392659  feet/sec       YDOT =       -1016
268790  meter/sec
 ZDOT =      19481
386490                 ZDOT =        5960
855697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17928677
93                 X    =         5464661
03
 Y    =      -13071882
20  feet           Y    =        -3984309
69  meter
 Z    =        2059836
47                 Z    =          627838
16
 XDOT =       6776
416722                 XDOT =        2065
451817
 YDOT =      12446
709064  feet/sec       YDOT =        3793
756923  meter/sec
 ZDOT =      19585
725198                 ZDOT =        5969
729040


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   19263
86326051  
00016717  00000-0  10270-3 0  9100
2 25544  51
6427 246
7625 0007268  65
7804 294
4105 15
50104961 30091


Satellite: ISS
Catalog Number: 25544
Epoch time:      19263
86326051   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:       246
7625  deg
Eccentricity:     
0007268     
Arg of perigee:    65
7804  deg
Mean anomaly:     294
4105  deg
Mean motion:   15
50104961  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3009
Checksum:              305


Coasting Arc #12 (Orbit 3023)
---------------------------------------

Vector Time (GMT): 2019/264/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2489051
73                 A    =         6800734
54  meter
 Y    =        6239908
08  meter          E    =           
0013773
 Z    =       -1046033
19                 I    =           51
32048
 XDOT =      -4833
114118                 Wp   =          112
13613
 YDOT =        956
425505  meter/sec      RA   =          241
09264  deg
 ZDOT =      -5862
427906                 TA   =           79
23015
                                          MA   =           79
07513
                                          Ha   =            229
987  n
mi
                                          Hp   =            218
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8166180
22                 X    =         2424171
37
 Y    =       20472139
37  feet           Y    =         6267379
61  meter
 Z    =       -3431867
41                 Z    =        -1034099
96
 XDOT =     -15856
673616                 XDOT =       -4814
973296
 YDOT =       3137
878955  feet/sec       YDOT =         902
479489  meter/sec
 ZDOT =     -19233
687356                 ZDOT =       -5885
861510

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17066567
95                 X    =        -5201889
91
 Y    =       13960452
76  feet           Y    =         4255146
00  meter
 Z    =       -3377975
82                 Z    =        -1029607
03
 XDOT =      -6697
942690                 XDOT =       -2041
532932
 YDOT =     -12813
619341  feet/sec       YDOT =       -3905
591175  meter/sec
 ZDOT =     -19340
321701                 ZDOT =       -5894
930055


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   19264
83030568  
00016717  00000-0  10270-3 0  9114
2 25544  51
6420 241
9715 0007174  70
5747 289
6179 15
50057914 30246


Satellite: ISS
Catalog Number: 25544
Epoch time:      19264
83030568   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:       241
9715  deg
Eccentricity:     
0007174     
Arg of perigee:    70
5747  deg
Mean anomaly:     289
6179  deg
Mean motion:   15
50057914  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3024
Checksum:              314


Coasting Arc #13 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2019/265/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2737318
59                 A    =         6800239
37  meter
 Y    =       -6059386
16  meter          E    =           
0020811
 Z    =        1381736
57                 I    =           51
33639
 XDOT =       4957
451412                 Wp   =           64
66849
 YDOT =       -908
609829  meter/sec      RA   =          236
11787  deg
 ZDOT =       5776
896162                 TA   =          310
43572
                                          MA   =          310
61705
                                          Ha   =            229
878  n
mi
                                          Hp   =            218
457

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8980704
05                 X    =        -2676069
08
 Y    =      -19879875
84  feet           Y    =        -6089654
28  meter
 Z    =        4533256
46                 Z    =         1368588
55
 XDOT =      16264
604370                 XDOT =        4939
182232
 YDOT =      -2981
003377  feet/sec       YDOT =        -853
274132  meter/sec
 ZDOT =      18953
071398                 ZDOT =        5800
933349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16001727
85                 X    =         4877326
65
 Y    =      -14843943
15  feet           Y    =        -4524433
87  meter
 Z    =        4473810
51                 Z    =         1363617
44
 XDOT =       6855
218897                 XDOT =        2089
470720
 YDOT =      13194
853877  feet/sec       YDOT =        4021
791462  meter/sec
 ZDOT =      19062
458171                 ZDOT =        5810
237250


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   19265
86181639  
00016717  00000-0  10270-3 0  9125
2 25544  51
6419 236
8604 0007136  72
8866 287
3066 15
50116384 30404


Satellite: ISS
Catalog Number: 25544
Epoch time:      19265
86181639   =   yrday
fracday
Element set:     912
Inclination:       51
6419  deg
RA of node:       236
8604  deg
Eccentricity:     
0007136     
Arg of perigee:    72
8866  deg
Mean anomaly:     287
3066  deg
Mean motion:   15
50116384  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              323


Coasting Arc #14 (Orbit 3054)
---------------------------------------

Vector Time (GMT): 2019/266/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2916389
43                 A    =         6799827
76  meter
 Y    =        5880836
81  meter          E    =           
0012291
 Z    =       -1773827
74                 I    =           51
35403
 XDOT =      -5109
979123                 Wp   =          110
26053
 YDOT =        844
147180  meter/sec      RA   =          231
14406  deg
 ZDOT =      -5638
866339                 TA   =           89
25180
                                          MA   =           89
11097
                                          Ha   =            229
964  n
mi
                                          Hp   =            218
498

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9568206
78                 X    =         2859027
73
 Y    =       19294084
02  feet           Y    =         5913129
15  meter
 Z    =       -5819644
80                 Z    =        -1759800
49
 XDOT =     -16765
023369                 XDOT =       -5091
648346
 YDOT =       2769
511744  feet/sec       YDOT =         787
106126  meter/sec
 ZDOT =     -18500
217646                 ZDOT =       -5663
644211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14993064
05                 X    =        -4569885
92
 Y    =       15484026
55  feet           Y    =         4719531
29  meter
 Z    =       -5756168
63                 Z    =        -1754480
20
 XDOT =      -7022
676713                 XDOT =       -2140
511862
 YDOT =     -13674
881132  feet/sec       YDOT =       -4168
103769  meter/sec
 ZDOT =     -18612
981145                 ZDOT =       -5673
236653


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   19266
82885795  
00016717  00000-0  10270-3 0  9137
2 25544  51
6417 232
0683 0007099  76
3987 283
7954 15
50076757 30559


Satellite: ISS
Catalog Number: 25544
Epoch time:      19266
82885795   =   yrday
fracday
Element set:     913
Inclination:       51
6417  deg
RA of node:       232
0683  deg
Eccentricity:     
0007099     
Arg of perigee:    76
3987  deg
Mean anomaly:     283
7954  deg
Mean motion:   15
50076757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3055
Checksum:              360


Coasting Arc #15 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2019/267/19:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3111157
01                 A    =         6799191
07  meter
 Y    =       -5659611
44  meter          E    =           
0020961
 Z    =        2096070
81                 I    =           51
37275
 XDOT =       5275
445178                 Wp   =           73
17380
 YDOT =       -848
875677  meter/sec      RA   =          226
17105  deg
 ZDOT =       5498
420308                 TA   =          310
10149
                                          MA   =          310
28502
                                          Ha   =            229
919  n
mi
                                          Hp   =            218
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10207208
04                 X    =        -3057819
89
 Y    =      -18568279
01  feet           Y    =        -5694104
28  meter
 Z    =        6876872
73                 Z    =         2081087
81
 XDOT =      17307
891004                 XDOT =        5257
837269
 YDOT =      -2785
025186  feet/sec       YDOT =        -789
980139  meter/sec
 ZDOT =      18039
436706                 ZDOT =        5524
003644

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13818707
86                 X    =         4211942
16
 Y    =      -16091615
73  feet           Y    =        -4904724
47  meter
 Z    =        6809014
34                 Z    =         2075387
57
 XDOT =       7436
404809                 XDOT =        2266
616186
 YDOT =      14124
270765  feet/sec       YDOT =        4305
077729  meter/sec
 ZDOT =      18155
876426                 ZDOT =        5533
911135


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   19267
86036584  
00016717  00000-0  10270-3 0  9147
2 25544  51
6403 226
9567 0007145  79
9210 280
2746 15
50121469 30717


Satellite: ISS
Catalog Number: 25544
Epoch time:      19267
86036584   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:       226
9567  deg
Eccentricity:     
0007145     
Arg of perigee:    79
9210  deg
Mean anomaly:     280
2746  deg
Mean motion:   15
50121469  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3071
Checksum:              318


Coasting Arc #16 (Orbit 3082)
---------------------------------------

Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         833328
38                 A    =         6790630
33  meter
 Y    =       -4576454
70  meter          E    =           
0012859
 Z    =        4937109
28                 I    =           51
36293
 XDOT =       6456
205483                 Wp   =          101
90066
 YDOT =       3525
586067  meter/sec      RA   =          222
28263  deg
 ZDOT =       2170
899350                 TA   =          326
81375
                                          MA   =          326
89434
                                          Ha   =            229
891  n
mi
                                          Hp   =            218
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2734017
00                 X    =          860460
04
 Y    =      -15014615
16  feet           Y    =        -4566983
83  meter
 Z    =       16197865
09                 Z    =         4941223
44
 XDOT =      21181
776519                 XDOT =        6405
756540
 YDOT =      11566
883421  feet/sec       YDOT =        3597
501967  meter/sec
 ZDOT =       7122
373197                 ZDOT =        2202
138301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5886866
87                 X    =         1794317
02
 Y    =       14058582
76  feet           Y    =         4285056
03  meter
 Z    =       16216824
60                 Z    =         4942888
14
 XDOT =     -23009
667810                 XDOT =       -7013
346749
 YDOT =       1227
494806  feet/sec       YDOT =         374
140417  meter/sec
 ZDOT =       7264
325217                 ZDOT =        2214
166326


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   19268
63399877  
00016717  00000-0  10270-3 0  9151
2 25544  51
6404 223
1242 0007206  83
4082 276
7889 15
50132191 30837


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
63399877   =   yrday
fracday
Element set:     915
Inclination:       51
6404  deg
RA of node:       223
1242  deg
Eccentricity:     
0007206     
Arg of perigee:    83
4082  deg
Mean anomaly:     276
7889  deg
Mean motion:   15
50132191  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3083
Checksum:              322


Coasting Arc #17 (Orbit 3084)
---------------------------------------

Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950049
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1020283
94                 A    =         6790413
62  meter
 Y    =       -4454104
55  meter          E    =           
0012377
 Z    =        5013112
27                 I    =           51
36664
 XDOT =       6452
829493                 Wp   =          101
53448
 YDOT =       3665
428360  meter/sec      RA   =          221
63831  deg
 ZDOT =       1936
901155                 TA   =          329
56798
                                          MA   =          329
63976
                                          Ha   =            229
989  n
mi
                                          Hp   =            218
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3347388
27                 X    =         1045664
38
 Y    =      -14613203
90  feet           Y    =        -4442552
78  meter
 Z    =       16447218
74                 Z    =         5018130
34
 XDOT =      21170
700435                 XDOT =        6401
953673
 YDOT =      12025
683596  feet/sec       YDOT =        3737
304113  meter/sec
 ZDOT =       6354
662582                 ZDOT =        1968
122647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13760933
91                 X    =         4194332
66
 Y    =        5884573
13  feet           Y    =         1793617
89  meter
 Z    =       16470283
48                 Z    =         5020142
40
 XDOT =     -15298
948270                 XDOT =       -4663
119433
 YDOT =      17533
543942  feet/sec       YDOT =        5344
224193  meter/sec
 ZDOT =       6496
531031                 ZDOT =        1980
142658


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   19268
76293807  
00016717  00000-0  10270-3 0  9162
2 25544  51
6420 222
4859 0007327  83
5388 276
6596 15
50094554 30851


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
76293807   =   yrday
fracday
Element set:     916
Inclination:       51
6420  deg
RA of node:       222
4859  deg
Eccentricity:     
0007327     
Arg of perigee:    83
5388  deg
Mean anomaly:     276
6596  deg
Mean motion:   15
50094554  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3085
Checksum:              347


Coasting Arc #18 (Orbit 3099)
---------------------------------------

Vector Time (GMT): 2019/269/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965158
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1065679
22                 A    =         6789860
71  meter
 Y    =        4325852
49  meter          E    =           
0020678
 Z    =       -5142310
48                 I    =           51
39114
 XDOT =      -6656
211641                 Wp   =           81
24633
 YDOT =      -3442
705481  meter/sec      RA   =          216
66305  deg
 ZDOT =      -1518
858802                 TA   =          174
03948
                                          MA   =          174
01483
                                          Ha   =            229
926  n
mi
                                          Hp   =            218
288

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3496322
89                 X    =        -1088994
53
 Y    =       14192429
44  feet           Y    =         4313804
48  meter
 Z    =      -16871097
39                 Z    =        -5147544
16
 XDOT =     -21837
964701                 XDOT =       -6609
841859
 YDOT =     -11294
965489  feet/sec       YDOT =       -3516
880804  meter/sec
 ZDOT =      -4983
132554                 ZDOT =       -1551
079143

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13420756
83                 X    =        -4090646
68
 Y    =       -5720242
79  feet           Y    =        -1743530
00  meter
 Z    =      -16895128
37                 Z    =        -5149635
13
 XDOT =      14383
077999                 XDOT =        4383
962174
 YDOT =     -18615
880454  feet/sec       YDOT =       -5674
120362  meter/sec
 ZDOT =      -5129
580802                 ZDOT =       -1563
496228


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   19269
72997516  
00016717  00000-0  10270-3 0  9178
2 25544  51
6424 217
6940 0007153  86
0555 274
1413 15
50122480 31002


Satellite: ISS
Catalog Number: 25544
Epoch time:      19269
72997516   =   yrday
fracday
Element set:     917
Inclination:       51
6424  deg
RA of node:       217
6940  deg
Eccentricity:     
0007153     
Arg of perigee:    86
0555  deg
Mean anomaly:     274
1413  deg
Mean motion:   15
50122480  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3100
Checksum:              304
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