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

 
Date: March 11th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15581 7398 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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


073/19:14:09 000 0 0 0 0 0 0
N/A 0 0 0 0 224 5
000/00:00:00 000 0 0 0 0 215 4

074/01:07:11 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 215 5

074/14:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 5
000/00:00:00 000 0 0 0 0 215 6

082/14:09:43 786 0 6 2 1 2 1
N/A 2 0 0 0 224 1
000/00:05:27 573 0 3 -0 0 217 1

082/22:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 1
000/00:00:00 000 0 0 0 0 217 0

Coasting Arc #1 (Orbit 6)
---------------------------------------

Vector Time (GMT): 2019/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900065
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2044728
34                 A    =         6790763
14  meter
 Y    =        6021032
95  meter          E    =           
0008434
 Z    =       -2384376
02                 I    =           51
95846
 XDOT =      -5423
466064                 Wp   =           66
91663
 YDOT =        290
590386  meter/sec      RA   =          125
81904  deg
 ZDOT =       5403
079903                 TA   =          266
60826
                                          MA   =          266
70474
                                          Ha   =            224
437  n
mi
                                          Hp   =            215
406

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6708426
31                 X    =        -2100323
31
 Y    =       19754045
11  feet           Y    =         5997856
28  meter
 Z    =       -7822755
95                 Z    =        -2394444
14
 XDOT =     -17793
523831                 XDOT =       -5452
557556
 YDOT =        953
380531  feet/sec       YDOT =         229
779266  meter/sec
 ZDOT =      17726
640101                 ZDOT =        5376
664109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10624845
33                 X    =        -3238452
86
 Y    =       17933645
29  feet           Y    =         5466175
08  meter
 Z    =       -7868787
76                 Z    =        -2398406
51
 XDOT =     -16409
901431                 XDOT =       -5001
737956
 YDOT =      -2022
875918  feet/sec       YDOT =        -616
572580  meter/sec
 ZDOT =      17607
113534                 ZDOT =        5366
648205


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   19070
50479253  
00016717  00000-0  10270-3 0  9009
2 25544  51
6382 126
8816 0003713  97
5397 262
6177 15
52796877    78


Satellite: ISS
Catalog Number: 25544
Epoch time:      19070
50479253   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:       126
8816  deg
Eccentricity:     
0003713     
Arg of perigee:    97
5397  deg
Mean anomaly:     262
6177  deg
Mean motion:   15
52796877  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:               7
Checksum:              331


Coasting Arc #2 (Orbit 22)
---------------------------------------

Vector Time (GMT): 2019/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900065
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2624901
09                 A    =         6792538
80  meter
 Y    =       -6149291
89  meter          E    =           
0017175
 Z    =        1154645
23                 I    =           51
98410
 XDOT =       4812
055481                 Wp   =          117
29309
 YDOT =        935
564436  meter/sec      RA   =          120
87444  deg
 ZDOT =      -5897
478657                 TA   =           50
23262
                                          MA   =           50
08147
                                          Ha   =            224
418  n
mi
                                          Hp   =            215
344

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8611880
20                 X    =         2687860
50
 Y    =      -20174842
16  feet           Y    =        -6119586
29  meter
 Z    =        3788206
13                 Z    =         1167549
40
 XDOT =      15787
583599                 XDOT =        4829
882728
 YDOT =       3069
437125  feet/sec       YDOT =         989
475410  meter/sec
 ZDOT =     -19348
683259                 ZDOT =       -5874
060310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12290104
02                 X    =         3746023
71
 Y    =      -18157434
54  feet           Y    =        -5534386
05  meter
 Z    =        3847097
17                 Z    =         1172595
22
 XDOT =      13710
769562                 XDOT =        4179
042562
 YDOT =       5162
582801  feet/sec       YDOT =        1573
555238  meter/sec
 ZDOT =     -19242
809059                 ZDOT =       -5865
208201


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   19071
53450714  
00016717  00000-0  10270-3 0  9015
2 25544  51
6391 121
7578 0003748  98
1225 262
0352 15
52826415   231


Satellite: ISS
Catalog Number: 25544
Epoch time:      19071
53450714   =   yrday
fracday
Element set:     901
Inclination:       51
6391  deg
RA of node:       121
7578  deg
Eccentricity:     
0003748     
Arg of perigee:    98
1225  deg
Mean anomaly:     262
0352  deg
Mean motion:   15
52826415  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              23
Checksum:              290


Coasting Arc #3 (Orbit 38)
---------------------------------------

Vector Time (GMT): 2019/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900065
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3033578
74                 A    =         6793292
65  meter
 Y    =        6071495
70  meter          E    =           
0014867
 Z    =          93187
52                 I    =           52
00209
 XDOT =      -4180
952438                 Wp   =           58
18120
 YDOT =      -2192
388905  meter/sec      RA   =          115
93409  deg
 ZDOT =       6040
157137                 TA   =          302
81703
                                          MA   =          302
96011
                                          Ha   =            224
528  n
mi
                                          Hp   =            215
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9952686
17                 X    =        -3101699
12
 Y    =       19919605
31  feet           Y    =         6037191
22  meter
 Z    =         305733
35                 Z    =           78285
75
 XDOT =     -13717
035559                 XDOT =       -4185
465436
 YDOT =      -7192
876985  feet/sec       YDOT =       -2239
168093  meter/sec
 ZDOT =      19816
788506                 ZDOT =        6019
836873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13278618
53                 X    =        -4047322
93
 Y    =       17876293
13  feet           Y    =         5448694
15  meter
 Z    =         237790
82                 Z    =           72478
64
 XDOT =     -11077
907036                 XDOT =       -3376
546065
 YDOT =      -8530
236077  feet/sec       YDOT =       -2600
015956  meter/sec
 ZDOT =      19725
032041                 ZDOT =        6012
189766


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   19072
56422196  
00016717  00000-0  10270-3 0  9023
2 25544  51
6391 116
6351 0003806  98
9616 261
1967 15
52765628   397


Satellite: ISS
Catalog Number: 25544
Epoch time:      19072
56422196   =   yrday
fracday
Element set:     902
Inclination:       51
6391  deg
RA of node:       116
6351  deg
Eccentricity:     
0003806     
Arg of perigee:    98
9616  deg
Mean anomaly:     261
1967  deg
Mean motion:   15
52765628  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              39
Checksum:              324


Coasting Arc #4 (Orbit 53)
---------------------------------------

Vector Time (GMT): 2019/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900065
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3360859
89                 A    =         6792353
18  meter
 Y    =       -5732869
43  meter          E    =           
0011986
 Z    =       -1387835
45                 I    =           52
01353
 XDOT =       3545
268681                 Wp   =          131
16375
 YDOT =       3481
389724  meter/sec      RA   =          110
99465  deg
 ZDOT =      -5835
825072                 TA   =           63
86948
                                          MA   =           63
74622
                                          Ha   =            224
482  n
mi
                                          Hp   =            215
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11026443
22                 X    =         3431457
97
 Y    =      -18808626
75  feet           Y    =        -5694891
28  meter
 Z    =       -4553265
91                 Z    =        -1371337
99
 XDOT =      11631
458926                 XDOT =        3534
422341
 YDOT =      11421
882298  feet/sec       YDOT =        3520
974463  meter/sec
 ZDOT =     -19146
407717                 ZDOT =       -5818
630100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13882517
37                 X    =         4231391
29
 Y    =      -16831557
90  feet           Y    =        -5130258
85  meter
 Z    =       -4478112
41                 Z    =        -1364928
66
 XDOT =       8585
316666                 XDOT =        2616
804520
 YDOT =      12118
670927  feet/sec       YDOT =        3693
770899  meter/sec
 ZDOT =     -19068
902658                 ZDOT =       -5812
201530


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   19073
52957514  
00016717  00000-0  10270-3 0  9038
2 25544  51
6396 111
8323 0003864 104
8647 255
2933 15
52816510   544


Satellite: ISS
Catalog Number: 25544
Epoch time:      19073
52957514   =   yrday
fracday
Element set:     903
Inclination:       51
6396  deg
RA of node:       111
8323  deg
Eccentricity:     
0003864     
Arg of perigee:   104
8647  deg
Mean anomaly:     255
2933  deg
Mean motion:   15
52816510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              54
Checksum:              306


Coasting Arc #5 (Orbit 58)
---------------------------------------

Vector Time (GMT): 2019/073/19:14:09
000
Vector Time (MET): N/A
Weight (LBS)     : 900065
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4230822
96                 A    =         6781378
39  meter
 Y    =        -415438
09  meter          E    =           
0006914
 Z    =        5278291
53                 I    =           51
97981
 XDOT =       1862
357330                 Wp   =          112
73031
 YDOT =      -7386
170168  meter/sec      RA   =          109
49861  deg
 ZDOT =        907
887501                 TA   =          328
60889
                                          MA   =          328
65014
                                          Ha   =            224
455  n
mi
                                          Hp   =            215
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13880652
77                 X    =        -4251501
81
 Y    =       -1362985
85  feet           Y    =         -462865
48  meter
 Z    =       17317229
44                 Z    =         5257689
72
 XDOT =       6110
096226                 XDOT =        1940
403179
 YDOT =     -24232
841759  feet/sec       YDOT =       -7364
907563  meter/sec
 ZDOT =       2978
633532                 ZDOT =         917
123975

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1032482
23                 X    =          314700
58
 Y    =       14024378
08  feet           Y    =         4274630
44  meter
 Z    =       17224038
06                 Z    =         5249886
80
 XDOT =     -23891
886492                 XDOT =       -7282
247003
 YDOT =      -1965
768696  feet/sec       YDOT =        -599
166299  meter/sec
 ZDOT =       3021
080669                 ZDOT =         920
825388


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   19073
85135934  
00016717  00000-0  10270-3 0  9049
2 25544  51
6387 110
2329 0003534 104
4456 255
7088 15
52840519   598


Satellite: ISS
Catalog Number: 25544
Epoch time:      19073
85135934   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:       110
2329  deg
Eccentricity:     
0003534     
Arg of perigee:   104
4456  deg
Mean anomaly:     255
7088  deg
Mean motion:   15
52840519  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              59
Checksum:              311


Coasting Arc #6 (Orbit 62)
---------------------------------------

Vector Time (GMT): 2019/074/01:07:11
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2944181
49                 A    =         6792616
39  meter
 Y    =        6001574
22  meter          E    =           
0016200
 Z    =        1168606
84                 I    =           52
01826
 XDOT =      -3842
194596                 Wp   =           67
13559
 YDOT =      -3044
317991  meter/sec      RA   =          108
28629  deg
 ZDOT =       5895
914052                 TA   =          305
48385
                                          MA   =          305
63491
                                          Ha   =            224
349  n
mi
                                          Hp   =            215
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9659388
09                 X    =        -3016750
37
 Y    =       19690204
14  feet           Y    =         5968244
62  meter
 Z    =        3834011
94                 Z    =         1154128
70
 XDOT =     -12605
625315                 XDOT =       -3836
505469
 YDOT =      -9987
919919  feet/sec       YDOT =       -3087
252021  meter/sec
 ZDOT =      19343
550039                 ZDOT =        5877
264210

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6752649
17                 X    =         2058207
47
 Y    =      -20878499
80  feet           Y    =        -6363766
74  meter
 Z    =        3767962
35                 Z    =         1148474
92
 XDOT =      12516
051335                 XDOT =        3814
892447
 YDOT =       7559
136803  feet/sec       YDOT =        2304
024898  meter/sec
 ZDOT =      19259
422615                 ZDOT =        5870
272013


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   19074
10878636  
00016717  00000-0  10270-3 0  9052
2 25544  51
6373 108
9504 0003520 106
6925 253
4613 15
52807918   632


Satellite: ISS
Catalog Number: 25544
Epoch time:      19074
10878636   =   yrday
fracday
Element set:     905
Inclination:       51
6373  deg
RA of node:       108
9504  deg
Eccentricity:     
0003520     
Arg of perigee:   106
6925  deg
Mean anomaly:     253
4613  deg
Mean motion:   15
52807918  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              63
Checksum:              308


Coasting Arc #7 (Orbit 70)
---------------------------------------

Vector Time (GMT): 2019/074/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3871180
92                 A    =         6781351
87  meter
 Y    =        1646020
96  meter          E    =           
0018464
 Z    =       -5334902
13                 I    =           51
98595
 XDOT =      -2406
142780                 Wp   =           96
61182
 YDOT =       7247
971488  meter/sec      RA   =          105
49187  deg
 ZDOT =        489
686064                 TA   =          178
05044
                                          MA   =          178
04323
                                          Ha   =            224
468  n
mi
                                          Hp   =            215
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12700724
79                 X    =         3878400
67
 Y    =        5400331
22  feet           Y    =         1689351
34  meter
 Z    =      -17502959
74                 Z    =        -5316080
11
 XDOT =      -7894
169226                 XDOT =       -2489
391421
 YDOT =      23779
434016  feet/sec       YDOT =        7220
598867  meter/sec
 ZDOT =       1606
581575                 ZDOT =         477
795531

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13766702
93                 X    =         4196091
05
 Y    =       -1979721
01  feet           Y    =         -603418
96  meter
 Z    =      -17417927
04                 Z    =        -5308984
16
 XDOT =       5338
267460                 XDOT =        1627
103922
 YDOT =      23447
949898  feet/sec       YDOT =        7146
935129  meter/sec
 ZDOT =       1552
120802                 ZDOT =         473
086420


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   19074
62364219  
00016717  00000-0  10270-3 0  9067
2 25544  51
6372 106
3898 0003807 107
4569 252
7000 15
52784653   711


Satellite: ISS
Catalog Number: 25544
Epoch time:      19074
62364219   =   yrday
fracday
Element set:     906
Inclination:       51
6372  deg
RA of node:       106
3898  deg
Eccentricity:     
0003807     
Arg of perigee:   107
4569  deg
Mean anomaly:     252
7000  deg
Mean motion:   15
52784653  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              71
Checksum:              312


Coasting Arc #8 (Orbit 86)
---------------------------------------

Vector Time (GMT): 2019/075/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3498679
31                 A    =         6782372
48  meter
 Y    =       -2834846
89  meter          E    =           
0008372
 Z    =        5065359
34                 I    =           51
99744
 XDOT =       2799
643938                 Wp   =           76
87545
 YDOT =      -6881
580479  meter/sec      RA   =          100
53075  deg
 ZDOT =      -1913
068353                 TA   =           31
59894
                                          MA   =           31
54870
                                          Ha   =            224
515  n
mi
                                          Hp   =            215
451

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11478606
65                 X    =        -3491323
58
 Y    =       -9300678
76  feet           Y    =        -2873930
18  meter
 Z    =       16618632
99                 Z    =         5048382
31
 XDOT =       9185
183522                 XDOT =        2885
680141
 YDOT =     -22577
363776  feet/sec       YDOT =       -6849
791940  meter/sec
 ZDOT =      -6276
470975                 ZDOT =       -1899
259617

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14756886
96                 X    =        -4497899
15
 Y    =       -1742040
80  feet           Y    =         -530974
04  meter
 Z    =       16542054
88                 Z    =         5042018
33
 XDOT =      -4271
232926                 XDOT =       -1301
871796
 YDOT =     -22959
696134  feet/sec       YDOT =       -6998
115382  meter/sec
 ZDOT =      -6213
345212                 ZDOT =       -1893
827620


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   19075
65334940  
00016717  00000-0  10270-3 0  9070
2 25544  51
6371 101
2666 0003704 109
9749 250
1802 15
52811057   878


Satellite: ISS
Catalog Number: 25544
Epoch time:      19075
65334940   =   yrday
fracday
Element set:     907
Inclination:       51
6371  deg
RA of node:       101
2666  deg
Eccentricity:     
0003704     
Arg of perigee:   109
9749  deg
Mean anomaly:     250
1802  deg
Mean motion:   15
52811057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:              87
Checksum:              302


Coasting Arc #9 (Orbit 101)
---------------------------------------

Vector Time (GMT): 2019/076/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3171404
26                 A    =         6784640
11  meter
 Y    =        3944084
22  meter          E    =           
0013305
 Z    =       -4531879
66                 I    =           52
00931
 XDOT =      -3127
383906                 Wp   =          110
88995
 YDOT =       6203
934566  meter/sec      RA   =           95
57406  deg
 ZDOT =       3213
721125                 TA   =          191
28312
                                          MA   =          191
31298
                                          Ha   =            224
416  n
mi
                                          Hp   =            215
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10404869
62                 X    =         3149077
68
 Y    =       12939908
84  feet           Y    =         3979423
94  meter
 Z    =      -14868371
59                 Z    =        -4516528
92
 XDOT =     -10260
445887                 XDOT =       -3212
135839
 YDOT =      20354
116029  feet/sec       YDOT =        6168
488308  meter/sec
 ZDOT =      10543
704477                 ZDOT =        3198
323468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15856290
84                 X    =         4832997
45
 Y    =        5131382
34  feet           Y    =         1564045
34  meter
 Z    =      -14799256
15                 Z    =        -4510813
27
 XDOT =       2794
850118                 XDOT =         851
870316
 YDOT =      21541
406526  feet/sec       YDOT =        6565
820709  meter/sec
 ZDOT =      10473
435933                 ZDOT =        3192
303272


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   19076
61869924  
00016717  00000-0  10270-3 0  9083
2 25544  51
6367  96
4642 0003716 111
9583 248
1964 15
52787249  1023


Satellite: ISS
Catalog Number: 25544
Epoch time:      19076
61869924   =   yrday
fracday
Element set:     908
Inclination:       51
6367  deg
RA of node:        96
4642  deg
Eccentricity:     
0003716     
Arg of perigee:   111
9583  deg
Mean anomaly:     248
1964  deg
Mean motion:   15
52787249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             102
Checksum:              340


Coasting Arc #10 (Orbit 117)
---------------------------------------

Vector Time (GMT): 2019/077/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2839417
10                 A    =         6787372
78  meter
 Y    =       -4917195
49  meter          E    =           
0014972
 Z    =        3705138
90                 I    =           52
02061
 XDOT =       3456
363175                 Wp   =           92
10653
 YDOT =      -5287
208296  meter/sec      RA   =           90
62196  deg
 ZDOT =      -4353
450628                 TA   =           44
00209
                                          MA   =           43
88300
                                          Ha   =            224
375  n
mi
                                          Hp   =            215
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9315672
90                 X    =        -2802217
79
 Y    =      -16132531
13  feet           Y    =        -4948739
50  meter
 Z    =       12155967
52                 Z    =         3691437
12
 XDOT =      11339
774195                 XDOT =        3536
375624
 YDOT =     -17346
483911  feet/sec       YDOT =       -5248
109845  meter/sec
 ZDOT =     -14282
974500                 ZDOT =       -4336
466399

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16808594
26                 X    =        -5123259
53
 Y    =       -8124302
52  feet           Y    =        -2476287
41  meter
 Z    =       12094409
31                 Z    =         3686375
96
 XDOT =       -806
496631                 XDOT =        -245
820173
 YDOT =     -19550
472974  feet/sec       YDOT =       -5958
984163  meter/sec
 ZDOT =     -14205
600018                 ZDOT =       -4329
866885


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   19077
64840420  
00016717  00000-0  10270-3 0  9098
2 25544  51
6364  91
3407 0003601 116
0774 244
0749 15
52821166  1184


Satellite: ISS
Catalog Number: 25544
Epoch time:      19077
64840420   =   yrday
fracday
Element set:     909
Inclination:       51
6364  deg
RA of node:        91
3407  deg
Eccentricity:     
0003601     
Arg of perigee:   116
0774  deg
Mean anomaly:     244
0749  deg
Mean motion:   15
52821166  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             118
Checksum:              296


Coasting Arc #11 (Orbit 132)
---------------------------------------

Vector Time (GMT): 2019/078/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2543258
32                 A    =         6790121
59  meter
 Y    =        5689858
55  meter          E    =           
0007356
 Z    =       -2699727
40                 I    =           52
02969
 XDOT =      -3768
904431                 Wp   =           81
77408
 YDOT =       4153
600157  meter/sec      RA   =           85
67582  deg
 ZDOT =       5216
667515                 TA   =          247
94674
                                          MA   =          248
02488
                                          Ha   =            224
342  n
mi
                                          Hp   =            215
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8344023
35                 X    =         2492557
25
 Y    =       18667514
91  feet           Y    =         5718015
24  meter
 Z    =       -8857373
35                 Z    =        -2687497
21
 XDOT =     -12365
172019                 XDOT =       -3840
410324
 YDOT =      13627
297103  feet/sec       YDOT =        4111
054428  meter/sec
 ZDOT =      17115
050901                 ZDOT =        5198
185729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17584520
05                 X    =         5359761
71
 Y    =       10481010
44  feet           Y    =         3194611
98  meter
 Z    =       -8802555
08                 Z    =        -2683018
79
 XDOT =      -1651
541968                 XDOT =        -503
389992
 YDOT =      17038
048255  feet/sec       YDOT =        5193
197108  meter/sec
 ZDOT =      17030
997847                 ZDOT =        5191
048144


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   19078
61375039  
00016717  00000-0  10270-3 0  9107
2 25544  51
6371  86
5377 0003681 118
4671 241
6852 15
52807553  1333


Satellite: ISS
Catalog Number: 25544
Epoch time:      19078
61375039   =   yrday
fracday
Element set:     910
Inclination:       51
6371  deg
RA of node:        86
5377  deg
Eccentricity:     
0003681     
Arg of perigee:   118
4671  deg
Mean anomaly:     241
6852  deg
Mean motion:   15
52807553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             133
Checksum:              314


Coasting Arc #12 (Orbit 148)
---------------------------------------

Vector Time (GMT): 2019/079/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2200444
43                 A    =         6792208
40  meter
 Y    =       -6240342
31  meter          E    =           
0017430
 Z    =        1495386
50                 I    =           52
03334
 XDOT =       4122
959575                 Wp   =          118
91254
 YDOT =      -2854
787648  meter/sec      RA   =           80
73400  deg
 ZDOT =      -5803
599675                 TA   =           44
85061
                                          MA   =           44
70987
                                          Ha   =            224
278  n
mi
                                          Hp   =            215
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7219305
86                 X    =        -2137763
28
 Y    =      -20473564
02  feet           Y    =        -6264598
55  meter
 Z    =        4906123
67                 Z    =         1484850
78
 XDOT =      13526
770258                 XDOT =        4182
766530
 YDOT =      -9366
101206  feet/sec       YDOT =       -2808
348220  meter/sec
 ZDOT =     -19040
681347                 ZDOT =       -5783
426474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17890909
08                 X    =        -5453149
09
 Y    =      -12315046
71  feet           Y    =        -3753626
24  meter
 Z    =        4859037
64                 Z    =         1481034
67
 XDOT =       4654
838621                 XDOT =        1418
794812
 YDOT =     -14294
813091  feet/sec       YDOT =       -4357
059030  meter/sec
 ZDOT =     -18949
092336                 ZDOT =       -5775
683344


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   19079
64345076  
00016717  00000-0  10270-3 0  9110
2 25544  51
6373  81
4136 0003567 121
2610 238
8892 15
52821119  1493


Satellite: ISS
Catalog Number: 25544
Epoch time:      19079
64345076   =   yrday
fracday
Element set:     911
Inclination:       51
6373  deg
RA of node:        81
4136  deg
Eccentricity:     
0003567     
Arg of perigee:   121
2610  deg
Mean anomaly:     238
8892  deg
Mean motion:   15
52821119  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             149
Checksum:              307


Coasting Arc #13 (Orbit 163)
---------------------------------------

Vector Time (GMT): 2019/080/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1852931
06                 A    =         6793077
09  meter
 Y    =        6526611
82  meter          E    =           
0012591
 Z    =        -249590
43                 I    =           52
02954
 XDOT =      -4481
151493                 Wp   =           59
92220
 YDOT =       1494
135884  meter/sec      RA   =           75
79582  deg
 ZDOT =       6035
935334                 TA   =          297
40488
                                          MA   =          297
53291
                                          Ha   =            224
218  n
mi
                                          Hp   =            215
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6079170
15                 X    =         1781023
29
 Y    =       21412768
45  feet           Y    =         6546930
50  meter
 Z    =        -818866
23                 Z    =         -240765
23
 XDOT =     -14701
940594                 XDOT =       -4526
845340
 YDOT =       4902
020618  feet/sec       YDOT =        1443
769886  meter/sec
 ZDOT =      19802
937449                 ZDOT =        6014
056525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17731565
67                 X    =         5404581
22
 Y    =       13457985
12  feet           Y    =         4101993
87  meter
 Z    =        -779563
77                 Z    =         -237611
04
 XDOT =      -7928
425340                 XDOT =       -2416
584044
 YDOT =      11540
955597  feet/sec       YDOT =        3517
683266  meter/sec
 ZDOT =      19703
759422                 ZDOT =        6005
705872


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   19080
60879384  
00016717  00000-0  10270-3 0  9123
2 25544  51
6370  76
6110 0003600 126
2933 233
8552 15
52830598  1645


Satellite: ISS
Catalog Number: 25544
Epoch time:      19080
60879384   =   yrday
fracday
Element set:     912
Inclination:       51
6370  deg
RA of node:        76
6110  deg
Eccentricity:     
0003600     
Arg of perigee:   126
2933  deg
Mean anomaly:     233
8552  deg
Mean motion:   15
52830598  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             164
Checksum:              302


Coasting Arc #14 (Orbit 179)
---------------------------------------

Vector Time (GMT): 2019/081/14:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915337
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1400575
16                 A    =         6792629
26  meter
 Y    =       -6556282
01  meter          E    =           
0012945
 Z    =       -1059084
39                 I    =           52
02056
 XDOT =       4864
653186                 Wp   =          138
26440
 YDOT =        -90
392006  meter/sec      RA   =           70
85716  deg
 ZDOT =      -5924
494261                 TA   =           53
15327
                                          MA   =           53
03463
                                          Ha   =            224
139  n
mi
                                          Hp   =            215
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4595062
85                 X    =        -1322012
42
 Y    =      -21510111
57  feet           Y    =        -6571505
09  meter
 Z    =       -3474686
32                 Z    =        -1065696
15
 XDOT =      15960
148249                 XDOT =        4894
080299
 YDOT =       -296
561701  feet/sec       YDOT =         -35
828313  meter/sec
 ZDOT =     -19437
317130                 ZDOT =       -5900
792146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16827107
72                 X    =        -5128902
43
 Y    =      -14157814
78  feet           Y    =        -4315301
94  meter
 Z    =       -3503951
18                 Z    =        -1068004
32
 XDOT =      11476
517965                 XDOT =        3498
042676
 YDOT =      -8897
199377  feet/sec       YDOT =       -2711
866370  meter/sec
 ZDOT =     -19330
027888                 ZDOT =       -5891
792500


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   19081
63849120  
00016717  00000-0  10270-3 0  9133
2 25544  51
6387  71
4872 0003452 129
6862 230
4595 15
52827333  1805


Satellite: ISS
Catalog Number: 25544
Epoch time:      19081
63849120   =   yrday
fracday
Element set:     913
Inclination:       51
6387  deg
RA of node:        71
4872  deg
Eccentricity:     
0003452     
Arg of perigee:   129
6862  deg
Mean anomaly:     230
4595  deg
Mean motion:   15
52827333  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             180
Checksum:              312


Coasting Arc #15 (Orbit 194)
---------------------------------------

Vector Time (GMT): 2019/082/14:12:27
573
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4611249
40                 A    =         6784282
49  meter
 Y    =         930103
08  meter          E    =           
0013301
 Z    =       -4901050
02                 I    =           51
97690
 XDOT =       1126
854900                 Wp   =          114
00809
 YDOT =       7173
820069  meter/sec      RA   =           65
95847  deg
 ZDOT =       2421
562854                 TA   =          179
66870
                                          MA   =          179
66782
                                          Ha   =            224
114  n
mi
                                          Hp   =            217
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15128771
00                 X    =         4624312
64
 Y    =        3051519
30  feet           Y    =          981741
77  meter
 Z    =      -16079560
44                 Z    =        -4878618
64
 XDOT =       3697
030511                 XDOT =        1034
788825
 YDOT =      23536
155082  feet/sec       YDOT =        7185
906856  meter/sec
 ZDOT =       7944
760020                 ZDOT =        2426
812261

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14438507
94                 X    =         4400857
22
 Y    =       -5742173
44  feet           Y    =        -1750214
46  meter
 Z    =      -15978131
26                 Z    =        -4870134
41
 XDOT =      15459
081482                 XDOT =        4711
928036
 YDOT =      16699
524293  feet/sec       YDOT =        5090
015005  meter/sec
 ZDOT =       7967
777535                 ZDOT =        2428
578593


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   19082
60383005  
00016717  00000-0  10270-3 0  9147
2 25544  51
6387  66
6844 0002111 155
3735 204
7517 15
52423009  1952


Satellite: ISS
Catalog Number: 25544
Epoch time:      19082
60383005   =   yrday
fracday
Element set:     914
Inclination:       51
6387  deg
RA of node:        66
6844  deg
Eccentricity:     
0002111     
Arg of perigee:   155
3735  deg
Mean anomaly:     204
7517  deg
Mean motion:   15
52423009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             195
Checksum:              293


Coasting Arc #16 (Orbit 200)
---------------------------------------

Vector Time (GMT): 2019/082/22:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1642051
25                 A    =         6785612
60  meter
 Y    =        4767246
83  meter          E    =           
0010418
 Z    =        4536280
45                 I    =           51
97520
 XDOT =      -5070
666941                 Wp   =          121
04221
 YDOT =      -4788
786360  meter/sec      RA   =           64
29489  deg
 ZDOT =       3186
488622                 TA   =          297
06600
                                          MA   =          297
17227
                                          Ha   =            224
126  n
mi
                                          Hp   =            217
048

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5387307
26                 X    =        -1717272
71
 Y    =       15640573
58  feet           Y    =         4748464
16  meter
 Z    =       14882809
87                 Z    =         4528120
74
 XDOT =     -16636
046395                 XDOT =       -5032
218749
 YDOT =     -15711
241338  feet/sec       YDOT =       -4845
274784  meter/sec
 ZDOT =      10454
358996                 ZDOT =        3161
951057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11112218
63                 X    =         3387004
24
 Y    =      -12299669
90  feet           Y    =        -3748939
39  meter
 Z    =       14845382
06                 Z    =         4524872
45
 XDOT =       8427
630826                 XDOT =        2568
741876
 YDOT =      20140
902618  feet/sec       YDOT =        6138
947118  meter/sec
 ZDOT =      10343
801286                 ZDOT =        3152
790632


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   19082
99006276  
00016717  00000-0  10270-3 0  9152
2 25544  51
6371  64
7617 0002161 160
1040 200
0197 15
52425435  2016


Satellite: ISS
Catalog Number: 25544
Epoch time:      19082
99006276   =   yrday
fracday
Element set:     915
Inclination:       51
6371  deg
RA of node:        64
7617  deg
Eccentricity:     
0002161     
Arg of perigee:   160
1040  deg
Mean anomaly:     200
0197  deg
Mean motion:   15
52425435  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             201
Checksum:              272


Coasting Arc #17 (Orbit 215)
---------------------------------------

Vector Time (GMT): 2019/083/22:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2252419
19                 A    =         6783553
42  meter
 Y    =       -3947306
82  meter          E    =           
0013306
 Z    =       -5047816
10                 I    =           51
95269
 XDOT =       5027
725952                 Wp   =           85
46816
 YDOT =       5417
195903  meter/sec      RA   =           59
33863  deg
 ZDOT =      -1996
203424                 TA   =          165
21520
                                          MA   =          165
17625
                                          Ha   =            224
122  n
mi
                                          Hp   =            217
051

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7389826
73                 X    =         2320911
25
 Y    =      -12950481
69  feet           Y    =        -3921736
15  meter
 Z    =      -16561076
43                 Z    =        -5036707
97
 XDOT =      16495
163884                 XDOT =        4976
472140
 YDOT =      17772
952439  feet/sec       YDOT =        5473
132706  meter/sec
 ZDOT =      -6549
223832                 ZDOT =       -1971
905482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11770824
23                 X    =        -3587747
23
 Y    =        9243852
26  feet           Y    =         2817526
17  meter
 Z    =      -16510380
37                 Z    =        -5032363
94
 XDOT =      -8089
272615                 XDOT =       -2465
610293
 YDOT =     -21782
173396  feet/sec       YDOT =       -6639
206451  meter/sec
 ZDOT =      -6439
832903                 ZDOT =       -1962
861069


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   19083
95564599  
00016717  00000-0  10270-3 0  9167
2 25544  51
6368  59
9604 0002390 159
8835 200
2412 15
52439534  2168


Satellite: ISS
Catalog Number: 25544
Epoch time:      19083
95564599   =   yrday
fracday
Element set:     916
Inclination:       51
6368  deg
RA of node:        59
9604  deg
Eccentricity:     
0002390     
Arg of perigee:   159
8835  deg
Mean anomaly:     200
2412  deg
Mean motion:   15
52439534  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             216
Checksum:              329


Coasting Arc #18 (Orbit 231)
---------------------------------------

Vector Time (GMT): 2019/084/22:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915117
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2894954
89                 A    =         6782548
32  meter
 Y    =        3085110
16  meter          E    =           
0004935
 Z    =        5298811
32                 I    =           51
93136
 XDOT =      -4897
841340                 Wp   =          136
73808
 YDOT =      -5855
111793  meter/sec      RA   =           54
37808  deg
 ZDOT =        729
212934                 TA   =          306
30146
                                          MA   =          306
34702
                                          Ha   =            224
209  n
mi
                                          Hp   =            217
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9497883
49                 X    =        -2954977
04
 Y    =       10121752
50  feet           Y    =         3052401
49  meter
 Z    =       17384551
57                 Z    =         5284602
71
 XDOT =     -16069
033268                 XDOT =       -4835
545921
 YDOT =     -19209
684361  feet/sec       YDOT =       -5909
534518  meter/sec
 ZDOT =       2392
430887                 ZDOT =         705
572699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12581660
36                 X    =         3834890
08
 Y    =       -6050196
59  feet           Y    =        -1844099
92  meter
 Z    =       17319908
82                 Z    =         5279108
21
 XDOT =       7775
756337                 XDOT =        2370
050531
 YDOT =      22751
185339  feet/sec       YDOT =        6934
561291  meter/sec
 ZDOT =       2286
079697                 ZDOT =         696
797092


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   19084
98560049  
00016717  00000-0  10270-3 0  9178
2 25544  51
6372  54
8386 0002325 164
3069 195
8155 15
52399157  2329


Satellite: ISS
Catalog Number: 25544
Epoch time:      19084
98560049   =   yrday
fracday
Element set:     917
Inclination:       51
6372  deg
RA of node:        54
8386  deg
Eccentricity:     
0002325     
Arg of perigee:   164
3069  deg
Mean anomaly:     195
8155  deg
Mean motion:   15
52399157  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             232
Checksum:              331
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