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

 
Date: January 7th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


010/09:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 216 3

016/05:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 216 2

018/18:04:49 685 2 7 2 9 2 9
N/A 0 7 0 0 220 9
000/00:07:35 370 -0 6 -0 0 217 7

020/01:03:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 217 7

Coasting Arc #1 (Orbit 3027)
---------------------------------------

Vector Time (GMT): 2019/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4063778
34                 A    =         6778543
26  meter
 Y    =        -992253
85  meter          E    =           
0012196
 Z    =       -5344310
40                 I    =           51
99840
 XDOT =       1538
917868                 Wp   =           91
89651
 YDOT =       7499
491326  meter/sec      RA   =           79
70807  deg
 ZDOT =       -223
043941                 TA   =          175
99043
                                          MA   =          175
98065
                                          Ha   =            220
703  n
mi
                                          Hp   =            216
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13332606
11                 X    =         4100531
26
 Y    =       -3255426
02  feet           Y    =         -946603
82  meter
 Z    =      -17533826
79                 Z    =        -5324481
24
 XDOT =       5048
943137                 XDOT =        1456
025482
 YDOT =      24604
630334  feet/sec       YDOT =        7516
237119  meter/sec
 ZDOT =       -731
771461                 ZDOT =        -215
769143

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6813097
06                 X    =         2076631
99
 Y    =       12044651
73  feet           Y    =         3671209
85  meter
 Z    =      -17444177
80                 Z    =        -5316985
39
 XDOT =     -21403
886185                 XDOT =       -6523
904509
 YDOT =      11097
536579  feet/sec       YDOT =        3382
529149  meter/sec
 ZDOT =       -699
864534                 ZDOT =        -213
318710


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   19007
51645976  
00016717  00000-0  10270-3 0  9007
2 25544  51
6412  80
4578 0002789 252
3091 107
7757 15
53725750 30288


Satellite: ISS
Catalog Number: 25544
Epoch time:      19007
51645976   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:        80
4578  deg
Eccentricity:     
0002789     
Arg of perigee:   252
3091  deg
Mean anomaly:     107
7757  deg
Mean motion:   15
53725750  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3028
Checksum:              319


Coasting Arc #2 (Orbit 3043)
---------------------------------------

Vector Time (GMT): 2019/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4351910
49                 A    =         6779195
85  meter
 Y    =        -636280
02  meter          E    =           
0002502
 Z    =        5158232
81                 I    =           51
99404
 XDOT =       -768
345055                 Wp   =           30
55291
 YDOT =      -7467
257158  meter/sec      RA   =           74
73733  deg
 ZDOT =      -1566
913708                 TA   =           74
49073
                                          MA   =           74
46311
                                          Ha   =            220
745  n
mi
                                          Hp   =            216
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14277921
56                 X    =        -4369527
38
 Y    =       -2087532
88  feet           Y    =         -685045
05  meter
 Z    =       16923335
98                 Z    =         5137050
38
 XDOT =      -2520
817110                 XDOT =        -677
175921
 YDOT =     -24498
875190  feet/sec       YDOT =       -7475
339436  meter/sec
 ZDOT =      -5140
793006                 ZDOT =       -1570
425181

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2179276
91                 X    =         -664243
60
 Y    =      -14376813
38  feet           Y    =        -4382052
72  meter
 Z    =       16827778
45                 Z    =         5129106
87
 XDOT =      21675
258154                 XDOT =        6606
618685
 YDOT =      -9329
626522  feet/sec       YDOT =       -2843
670164  meter/sec
 ZDOT =      -5155
703757                 ZDOT =       -1571
458505


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   19008
54554586  
00016717  00000-0  10270-3 0  9018
2 25544  51
6411  75
3312 0002783 256
7006 103
3836 15
53774800 30442


Satellite: ISS
Catalog Number: 25544
Epoch time:      19008
54554586   =   yrday
fracday
Element set:     901
Inclination:       51
6411  deg
RA of node:        75
3312  deg
Eccentricity:     
0002783     
Arg of perigee:   256
7006  deg
Mean anomaly:     103
3836  deg
Mean motion:   15
53774800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3044
Checksum:              294


Coasting Arc #3 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2019/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4568879
55                 A    =         6781839
04  meter
 Y    =        2166490
16  meter          E    =           
0007449
 Z    =       -4526976
32                 I    =           51
99186
 XDOT =       -113
762986                 Wp   =          120
34621
 YDOT =       6953
405935  meter/sec      RA   =           69
77019  deg
 ZDOT =       3213
169875                 TA   =          181
81520
                                          MA   =          181
81791
                                          Ha   =            220
671  n
mi
                                          Hp   =            216
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14989762
30                 X    =         4566302
82
 Y    =        7107907
37  feet           Y    =         2217568
46  meter
 Z    =      -14852284
51                 Z    =        -4504788
92
 XDOT =       -373
238143                 XDOT =        -207
116984
 YDOT =      22813
011599  feet/sec       YDOT =        6951
611565  meter/sec
 ZDOT =      10541
895915                 ZDOT =        3212
391004

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2138486
53                 X    =         -651810
69
 Y    =       16540849
95  feet           Y    =         5041651
07  meter
 Z    =      -14752384
01                 Z    =        -4496526
65
 XDOT =     -20644
916717                 XDOT =       -6292
570615
 YDOT =       6728
254013  feet/sec       YDOT =        2050
771823  meter/sec
 ZDOT =      10537
492209                 ZDOT =        3211
827625


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   19009
51031552  
00016717  00000-0  10270-3 0  9020
2 25544  51
6401  70
5248 0002559 259
9208 100
1656 15
53761331 30592


Satellite: ISS
Catalog Number: 25544
Epoch time:      19009
51031552   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:        70
5248  deg
Eccentricity:     
0002559     
Arg of perigee:   259
9208  deg
Mean anomaly:     100
1656  deg
Mean motion:   15
53761331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3059
Checksum:              286


Coasting Arc #4 (Orbit 3072)
---------------------------------------

Vector Time (GMT): 2019/010/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4652323
57                 A    =         6780659
40  meter
 Y    =        1104698
14  meter          E    =           
0009024
 Z    =       -4816210
70                 I    =           51
97857
 XDOT =       1020
585536                 Wp   =          116
02267
 YDOT =       7125
448360  meter/sec      RA   =           65
31324  deg
 ZDOT =       2620
177588                 TA   =          179
71165
                                          MA   =          179
71113
                                          Ha   =            220
606  n
mi
                                          Hp   =            216
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15263528
77                 X    =         4663018
83
 Y    =        3624337
71  feet           Y    =         1156783
71  meter
 Z    =      -15801216
22                 Z    =        -4793585
81
 XDOT =       3348
377742                 XDOT =         928
103771
 YDOT =      23377
455249  feet/sec       YDOT =        7136
344020  meter/sec
 ZDOT =       8596
383163                 ZDOT =        2624
910888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8079213
10                 X    =        -2462544
15
 Y    =       13566532
47  feet           Y    =         4135079
10  meter
 Z    =      -15699206
37                 Z    =        -4785118
10
 XDOT =     -22295
734635                 XDOT =       -6795
739917
 YDOT =      -3306
072325  feet/sec       YDOT =       -1007
690845  meter/sec
 ZDOT =       8616
837495                 ZDOT =        2626
412068


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   19010
41076376  
00016717  00000-0  10270-3 0  9035
2 25544  51
6417  66
0374 0002646 261
1351  98
9502 15
53777853 30736


Satellite: ISS
Catalog Number: 25544
Epoch time:      19010
41076376   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:        66
0374  deg
Eccentricity:     
0002646     
Arg of perigee:   261
1351  deg
Mean anomaly:      98
9502  deg
Mean motion:   15
53777853  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3073
Checksum:              305


Coasting Arc #5 (Orbit 3088)
---------------------------------------

Vector Time (GMT): 2019/011/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4942485
45                 A    =         6784026
47  meter
 Y    =       -2506569
41  meter          E    =           
0008687
 Z    =        3907010
07                 I    =           51
97482
 XDOT =         20
374774                 Wp   =           79
16747
 YDOT =      -6470
835885  meter/sec      RA   =           60
34905  deg
 ZDOT =      -4116
306404                 TA   =           53
82269
                                          MA   =           53
74236
                                          Ha   =            220
737  n
mi
                                          Hp   =            216
214

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16215503
44                 X    =        -4933066
75
 Y    =       -8223652
92  feet           Y    =        -2561787
22  meter
 Z    =       12818274
51                 Z    =         3883024
48
 XDOT =         66
846372                 XDOT =         112
726387
 YDOT =     -21229
776524  feet/sec       YDOT =       -6470
091508  meter/sec
 ZDOT =     -13504
942271                 ZDOT =       -4115
983386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12519322
11                 X    =         3815889
38
 Y    =      -13288862
46  feet           Y    =        -4050445
28  meter
 Z    =       12710306
42                 Z    =         3874101
40
 XDOT =      19340
254041                 XDOT =        5894
909432
 YDOT =       5275
983932  feet/sec       YDOT =        1608
119902  meter/sec
 ZDOT =     -13502
643506                 ZDOT =       -4115
605741


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   19011
43984628  
00016717  00000-0  10270-3 0  9047
2 25544  51
6417  60
9103 0002597 268
2116  91
8739 15
53763414 30890


Satellite: ISS
Catalog Number: 25544
Epoch time:      19011
43984628   =   yrday
fracday
Element set:     904
Inclination:       51
6417  deg
RA of node:        60
9103  deg
Eccentricity:     
0002597     
Arg of perigee:   268
2116  deg
Mean anomaly:      91
8739  deg
Mean motion:   15
53763414  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3089
Checksum:              321


Coasting Arc #6 (Orbit 3103)
---------------------------------------

Vector Time (GMT): 2019/012/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5057122
55                 A    =         6787525
82  meter
 Y    =        3655718
67  meter          E    =           
0003332
 Z    =       -2667039
86                 I    =           51
96807
 XDOT =      -1197
842187                 Wp   =           22
70410
 YDOT =       5470
938901  meter/sec      RA   =           55
39308  deg
 ZDOT =       5232
899327                 TA   =          307
36489
                                          MA   =          307
39524
                                          Ha   =            220
649  n
mi
                                          Hp   =            216
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16591609
43                 X    =         5028822
26
 Y    =       11993827
66  feet           Y    =         3712112
78  meter
 Z    =       -8750130
78                 Z    =        -2642543
19
 XDOT =      -3929
928436                 XDOT =       -1284
348932
 YDOT =      17949
274610  feet/sec       YDOT =        5457
059949  meter/sec
 ZDOT =      17168
304879                 ZDOT =        5226
870791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16015025
22                 X    =        -4881379
69
 Y    =       12828380
28  feet           Y    =         3910090
31  meter
 Z    =       -8640012
76                 Z    =        -2633475
89
 XDOT =     -15275
550381                 XDOT =       -4655
987756
 YDOT =      -7537
472005  feet/sec       YDOT =       -2297
421467  meter/sec
 ZDOT =      17140
369567                 ZDOT =        5224
384644


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   19012
40461053  
00016717  00000-0  10270-3 0  9058
2 25544  51
6409  56
1042 0002736 271
8670  88
2169 15
53736965 31046


Satellite: ISS
Catalog Number: 25544
Epoch time:      19012
40461053   =   yrday
fracday
Element set:     905
Inclination:       51
6409  deg
RA of node:        56
1042  deg
Eccentricity:     
0002736     
Arg of perigee:   271
8670  deg
Mean anomaly:      88
2169  deg
Mean motion:   15
53736965  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3104
Checksum:              298


Coasting Arc #7 (Orbit 3119)
---------------------------------------

Vector Time (GMT): 2019/013/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4919827
30                 A    =         6789853
48  meter
 Y    =       -4522724
69  meter          E    =           
0011382
 Z    =        1166650
56                 I    =           51
95657
 XDOT =       2485
265098                 Wp   =          128
15233
 YDOT =      -4231
797933  meter/sec      RA   =           50
44339  deg
 ZDOT =      -5892
736247                 TA   =           39
23448
                                          MA   =           39
15204
                                          Ha   =            220
645  n
mi
                                          Hp   =            216
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16141165
68                 X    =        -4874554
16
 Y    =      -14838335
61  feet           Y    =        -4577488
52  meter
 Z    =        3827593
72                 Z    =         1142861
96
 XDOT =       8153
756882                 XDOT =        2561
024903
 YDOT =     -13883
851485  feet/sec       YDOT =       -4203
582207  meter/sec
 ZDOT =     -19333
124171                 ZDOT =       -5880
479989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18424144
95                 X    =         5615679
38
 Y    =      -11919331
32  feet           Y    =        -3633012
19  meter
 Z    =        3720797
06                 Z    =         1134098
94
 XDOT =      10489
407808                 XDOT =        3197
171500
 YDOT =      10162
394236  feet/sec       YDOT =        3097
497763  meter/sec
 ZDOT =     -19277
230702                 ZDOT =       -5875
699918


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   19013
43369127  
00016717  00000-0  10270-3 0  9062
2 25544  51
6411  50
9773 0002610 276
4387  83
6468 15
53761259 31202


Satellite: ISS
Catalog Number: 25544
Epoch time:      19013
43369127   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:        50
9773  deg
Eccentricity:     
0002610     
Arg of perigee:   276
4387  deg
Mean anomaly:      83
6468  deg
Mean motion:   15
53761259  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3120
Checksum:              308


Coasting Arc #8 (Orbit 3135)
---------------------------------------

Vector Time (GMT): 2019/014/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4509238
10                 A    =         6790421
98  meter
 Y    =        5051344
66  meter          E    =           
0011609
 Z    =         414851
99                 I    =           51
93644
 XDOT =      -3782
800362                 Wp   =           38
77662
 YDOT =       2875
738620  meter/sec      RA   =           45
49541  deg
 ZDOT =       6019
442985                 TA   =          325
67808
                                          MA   =          325
75303
                                          Ha   =            220
759  n
mi
                                          Hp   =            216
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14794088
26                 X    =         4450402
30
 Y    =       16572653
09  feet           Y    =         5101441
12  meter
 Z    =        1361062
97                 Z    =          436613
29
 XDOT =     -12410
762341                 XDOT =       -3843
915441
 YDOT =       9434
837993  feet/sec       YDOT =        2833
094801  meter/sec
 ZDOT =      19748
828690                 ZDOT =        6000
919343

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19578556
08                 X    =        -5967543
89
 Y    =       10484413
48  feet           Y    =         3195649
23  meter
 Z    =        1458624
68                 Z    =          444588
80
 XDOT =      -5466
184572                 XDOT =       -1666
093057
 YDOT =     -12978
294828  feet/sec       YDOT =       -3955
784264  meter/sec
 ZDOT =      19664
819561                 ZDOT =        5993
837002


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   19014
46277080  
00016717  00000-0  10270-3 0  9073
2 25544  51
6414  45
8500 0002607 285
9319  74
1546 15
53724749 31364


Satellite: ISS
Catalog Number: 25544
Epoch time:      19014
46277080   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:        45
8500  deg
Eccentricity:     
0002607     
Arg of perigee:   285
9319  deg
Mean anomaly:      74
1546  deg
Mean motion:   15
53724749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3136
Checksum:              311


Coasting Arc #9 (Orbit 3150)
---------------------------------------

Vector Time (GMT): 2019/015/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3777907
98                 A    =         6788679
91  meter
 Y    =       -5277424
20  meter          E    =           
0004799
 Z    =       -1982862
86                 I    =           51
90623
 XDOT =       5015
380254                 Wp   =          155
62207
 YDOT =      -1488
872079  meter/sec      RA   =           40
54560  deg
 ZDOT =      -5602
120700                 TA   =           46
17116
                                          MA   =           46
13150
                                          Ha   =            220
715  n
mi
                                          Hp   =            216
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12394711
23                 X    =        -3708981
96
 Y    =      -17314383
84  feet           Y    =        -5319285
92  meter
 Z    =       -6505455
58                 Z    =        -2001047
26
 XDOT =      16454
659626                 XDOT =        5058
868340
 YDOT =      -4884
750915  feet/sec       YDOT =       -1432
543195  meter/sec
 ZDOT =     -18379
661090                 ZDOT =       -5577
652429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19589474
41                 X    =         5970871
80
 Y    =       -8282747
65  feet           Y    =        -2524581
48  meter
 Z    =       -6586827
03                 Z    =        -2007664
88
 XDOT =        553
824581                 XDOT =         168
805732
 YDOT =      15814
816611  feet/sec       YDOT =        4820
356103  meter/sec
 ZDOT =     -18269
004007                 ZDOT =       -5568
392421


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   19015
42753056  
00016717  00000-0  10270-3 0  9083
2 25544  51
6406  41
0441 0002495 287
5756  72
5124 15
53763345 31511


Satellite: ISS
Catalog Number: 25544
Epoch time:      19015
42753056   =   yrday
fracday
Element set:     908
Inclination:       51
6406  deg
RA of node:        41
0441  deg
Eccentricity:     
0002495     
Arg of perigee:   287
5756  deg
Mean anomaly:      72
5124  deg
Mean motion:   15
53763345  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3151
Checksum:              298


Coasting Arc #10 (Orbit 3163)
---------------------------------------

Vector Time (GMT): 2019/016/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5935885
86                 A    =         6787014
32  meter
 Y    =       -1565394
65  meter          E    =           
0010896
 Z    =        2883134
39                 I    =           51
87923
 XDOT =       -977
222899                 Wp   =           98
29596
 YDOT =      -5666
918362  meter/sec      RA   =           36
39863  deg
 ZDOT =      -5073
960553                 TA   =           48
99603
                                          MA   =           48
90185
                                          Ha   =            220
807  n
mi
                                          Hp   =            216
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19474691
13                 X    =        -5931944
61
 Y    =       -5135809
23  feet           Y    =        -1631752
00  meter
 Z    =        9459102
34                 Z    =         2854309
69
 XDOT =      -3206
111872                 XDOT =        -889
134827
 YDOT =     -18592
251844  feet/sec       YDOT =       -5677
353515  meter/sec
 ZDOT =     -16646
852209                 ZDOT =       -5078
493905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20197890
67                 X    =         6156317
08
 Y    =        -354929
70  feet           Y    =         -108182
57  meter
 Z    =        9329200
69                 Z    =         2843540
37
 XDOT =       7994
746794                 XDOT =        2436
798823
 YDOT =      15584
833332  feet/sec       YDOT =        4750
257200  meter/sec
 ZDOT =     -16666
538570                 ZDOT =       -5079
960956


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   19016
26365639  
00016717  00000-0  10270-3 0  9093
2 25544  51
6409  36
8756 0002461 282
8169  77
2708 15
53746403 31644


Satellite: ISS
Catalog Number: 25544
Epoch time:      19016
26365639   =   yrday
fracday
Element set:     909
Inclination:       51
6409  deg
RA of node:        36
8756  deg
Eccentricity:     
0002461     
Arg of perigee:   282
8169  deg
Mean anomaly:      77
2708  deg
Mean motion:   15
53746403  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3164
Checksum:              331


Coasting Arc #11 (Orbit 3178)
---------------------------------------

Vector Time (GMT): 2019/017/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6163460
49                 A    =         6789600
38  meter
 Y    =        2446517
45  meter          E    =           
0008308
 Z    =       -1436278
19                 I    =           51
86186
 XDOT =       -621
587000                 Wp   =           20
23508
 YDOT =       4965
757434  meter/sec      RA   =           31
44152  deg
 ZDOT =       5808
748195                 TA   =          324
15194
                                          MA   =          324
20767
                                          Ha   =            220
844  n
mi
                                          Hp   =            216
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20221327
05                 X    =         6142621
36
 Y    =        8026632
05  feet           Y    =         2515325
15  meter
 Z    =       -4712198
79                 Z    =        -1406388
99
 XDOT =      -2039
327427                 XDOT =        -705
284813
 YDOT =      16291
855099  feet/sec       YDOT =        4958
337968  meter/sec
 ZDOT =      19057
572819                 ZDOT =        5805
525886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21705202
72                 X    =        -6615745
79
 Y    =       -1860986
59  feet           Y    =         -567228
71  meter
 Z    =       -4577620
65                 Z    =        -1395258
78
 XDOT =      -2747
829280                 XDOT =        -837
538364
 YDOT =     -14645
005144  feet/sec       YDOT =       -4463
797568  meter/sec
 ZDOT =      19042
338499                 ZDOT =        5804
104775


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   19017
22841387  
00016717  00000-0  10270-3 0  9101
2 25544  51
6422  32
0692 0002514 292
5250  67
5636 15
53750443 31791


Satellite: ISS
Catalog Number: 25544
Epoch time:      19017
22841387   =   yrday
fracday
Element set:     910
Inclination:       51
6422  deg
RA of node:        32
0692  deg
Eccentricity:     
0002514     
Arg of perigee:   292
5250  deg
Mean anomaly:      67
5636  deg
Mean motion:   15
53750443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3179
Checksum:              296


Coasting Arc #12 (Orbit 3194)
---------------------------------------

Vector Time (GMT): 2019/018/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6012500
70                 A    =         6790372
73  meter
 Y    =       -3140924
78  meter          E    =           
0009463
 Z    =        -164950
09                 I    =           51
83478
 XDOT =       2320
053665                 Wp   =          141
28530
 YDOT =      -4134
888587  meter/sec      RA   =           26
48746  deg
 ZDOT =      -6025
404106                 TA   =           40
48649
                                          MA   =           40
41613
                                          Ha   =            220
796  n
mi
                                          Hp   =            216
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19726052
16                 X    =        -5976129
91
 Y    =      -10304871
33  feet           Y    =        -3207957
37  meter
 Z    =        -541174
85                 Z    =         -194068
29
 XDOT =       7611
724622                 XDOT =        2395
386534
 YDOT =     -13565
907437  feet/sec       YDOT =       -4108
522333  meter/sec
 ZDOT =     -19768
386175                 ZDOT =       -6013
951685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21921706
45                 X    =         6681736
13
 Y    =        3819339
07  feet           Y    =         1164134
55  meter
 Z    =        -672169
90                 Z    =         -204877
39
 XDOT =      -2972
463113                 XDOT =        -906
006757
 YDOT =      13681
082635  feet/sec       YDOT =        4169
993987  meter/sec
 ZDOT =     -19716
112675                 ZDOT =       -6009
471143


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   19018
25748783  
00016717  00000-0  10270-3 0  9112
2 25544  51
6412  26
9424 0002449 294
4719  65
6178 15
53763080 31952


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
25748783   =   yrday
fracday
Element set:     911
Inclination:       51
6412  deg
RA of node:        26
9424  deg
Eccentricity:     
0002449     
Arg of perigee:   294
4719  deg
Mean anomaly:      65
6178  deg
Mean motion:   15
53763080  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3195
Checksum:              328


Coasting Arc #13 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2019/018/18:08:37
370
Vector Time (MET): N/A
Weight (LBS)     : 929347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1683386
47                 A    =         6779967
15  meter
 Y    =       -3846985
31  meter          E    =           
0010587
 Z    =       -5332141
26                 I    =           51
77901
 XDOT =       7009
536306                 Wp   =           83
95277
 YDOT =       3087
631521  meter/sec      RA   =           23
85327  deg
 ZDOT =        -13
623148                 TA   =          185
91126
                                          MA   =          185
92377
                                          Ha   =            220
933  n
mi
                                          Hp   =            217
737

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5522921
49                 X    =         1752179
72
 Y    =      -12621342
88  feet           Y    =        -3827775
31  meter
 Z    =      -17493901
76                 Z    =        -5323797
40
 XDOT =      22997
166358                 XDOT =        6974
554755
 YDOT =      10130
024675  feet/sec       YDOT =        3165
821443  meter/sec
 ZDOT =        -44
695369                 ZDOT =          20
341535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1218892
23                 X    =         -371518
35
 Y    =      -13771363
24  feet           Y    =        -4197511
51  meter
 Z    =      -17455698
59                 Z    =        -5320496
93
 XDOT =      24015
135401                 XDOT =        7319
813270
 YDOT =      -2258
248618  feet/sec       YDOT =        -688
314179  meter/sec
 ZDOT =        108
180945                 ZDOT =          32
973552


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   19018
77202723  
00016717  00000-0  10270-3 0  9129
2 25544  51
6413  24
3826 0004471 284
2858  75
7797 15
53231605 32031


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
77202723   =   yrday
fracday
Element set:     912
Inclination:       51
6413  deg
RA of node:        24
3826  deg
Eccentricity:     
0004471     
Arg of perigee:   284
2858  deg
Mean anomaly:      75
7797  deg
Mean motion:   15
53231605  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3203
Checksum:              304


Coasting Arc #14 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2019/019/18:08:37
370
Vector Time (MET): N/A
Weight (LBS)     : 929347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2992413
52                 A    =         6780761
74  meter
 Y    =        3259003
90  meter          E    =           
0004294
 Z    =        5139763
83                 I    =           51
75086
 XDOT =      -6599
276752                 Wp   =          354
27146
 YDOT =      -3568
408796  meter/sec      RA   =           18
87252  deg
 ZDOT =      -1575
451830                 TA   =          110
92206
                                          MA   =          110
87609
                                          Ha   =            221
021  n
mi
                                          Hp   =            217
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9817629
65                 X    =        -3053599
91
 Y    =       10692270
02  feet           Y    =         3225197
99  meter
 Z    =       16862742
24                 Z    =         5125079
79
 XDOT =     -21651
170446                 XDOT =       -6551
230794
 YDOT =     -11707
377940  feet/sec       YDOT =       -3641
937695  meter/sec
 ZDOT =      -5168
805218                 ZDOT =       -1607
391790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3223574
46                 X    =         -982545
50
 Y    =       14232548
87  feet           Y    =         4338080
89  meter
 Z    =       16796002
10                 Z    =         5119421
44
 XDOT =     -23534
738636                 XDOT =       -7173
388336
 YDOT =        954
628802  feet/sec       YDOT =         290
970859  meter/sec
 ZDOT =      -5312
471758                 ZDOT =       -1619
241392


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   19019
80146179  
00016717  00000-0  10270-3 0  9137
2 25544  51
6411  19
2583 0004694 287
7083  72
3556 15
53255828 32193


Satellite: ISS
Catalog Number: 25544
Epoch time:      19019
80146179   =   yrday
fracday
Element set:     913
Inclination:       51
6411  deg
RA of node:        19
2583  deg
Eccentricity:     
0004694     
Arg of perigee:   287
7083  deg
Mean anomaly:      72
3556  deg
Mean motion:   15
53255828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3219
Checksum:              324


Coasting Arc #15 (Orbit 3222)
---------------------------------------

Vector Time (GMT): 2019/020/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1848405
23                 A    =         6780091
42  meter
 Y    =       -3806305
07  meter          E    =           
0010435
 Z    =       -5306667
12                 I    =           51
73709
 XDOT =       7145
822171                 Wp   =           90
34668
 YDOT =       2701
923569  meter/sec      RA   =           17
44596  deg
 ZDOT =        551
887056                 TA   =          184
91342
                                          MA   =          184
92367
                                          Ha   =            220
970  n
mi
                                          Hp   =            217
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6064321
62                 X    =         1916607
38
 Y    =      -12487877
53  feet           Y    =        -3785253
02  meter
 Z    =      -17410325
18                 Z    =        -5297523
17
 XDOT =      23444
298462                 XDOT =        7112
396704
 YDOT =       8864
578640  feet/sec       YDOT =        2781
646177  meter/sec
 ZDOT =       1810
653072                 ZDOT =         586
517234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13277554
92                 X    =        -4046998
74
 Y    =        4228917
23  feet           Y    =         1288973
97  meter
 Z    =      -17368514
60                 Z    =        -5293923
25
 XDOT =      -9590
336391                 XDOT =       -2923
134532
 YDOT =     -22045
745477  feet/sec       YDOT =       -6719
543221  meter/sec
 ZDOT =       1966
584426                 ZDOT =         599
414933


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   19020
05882118  
00016717  00000-0  10270-3 0  9147
2 25544  51
6389  17
9725 0004327 283
9553  76
1118 15
53229810 32236


Satellite: ISS
Catalog Number: 25544
Epoch time:      19020
05882118   =   yrday
fracday
Element set:     914
Inclination:       51
6389  deg
RA of node:        17
9725  deg
Eccentricity:     
0004327     
Arg of perigee:   283
9553  deg
Mean anomaly:      76
1118  deg
Mean motion:   15
53229810  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3223
Checksum:              307


Coasting Arc #16 (Orbit 3238)
---------------------------------------

Vector Time (GMT): 2019/021/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3180748
28                 A    =         6781633
66  meter
 Y    =        3325252
64  meter          E    =           
0004873
 Z    =        4982035
08                 I    =           51
70931
 XDOT =      -6646
862409                 Wp   =           14
72305
 YDOT =      -3179
879471  meter/sec      RA   =           12
46135  deg
 ZDOT =      -2116
181038                 TA   =           95
89598
                                          MA   =           95
84043
                                          Ha   =            221
234  n
mi
                                          Hp   =            217
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10435525
86                 X    =        -3241895
16
 Y    =       10909621
52  feet           Y    =         3289340
97  meter
 Z    =       16345259
46                 Z    =         4966436
36
 XDOT =     -21807
291367                 XDOT =       -6600
531120
 YDOT =     -10432
675430  feet/sec       YDOT =       -3253
950076  meter/sec
 ZDOT =      -6942
851173                 ZDOT =       -2148
355965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15171268
47                 X    =         4624202
63
 Y    =        -254187
40  feet           Y    =          -77476
32  meter
 Z    =       16274383
25                 Z    =         4960432
02
 XDOT =       7983
774295                 XDOT =        2433
454405
 YDOT =      21660
563652  feet/sec       YDOT =        6602
139801  meter/sec
 ZDOT =      -7087
631559                 ZDOT =       -2160
310099


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   19021
08825525  
00016717  00000-0  10270-3 0  9151
2 25544  51
6384  12
8462 0004241 288
1040  71
9650 15
53189664 32399


Satellite: ISS
Catalog Number: 25544
Epoch time:      19021
08825525   =   yrday
fracday
Element set:     915
Inclination:       51
6384  deg
RA of node:        12
8462  deg
Eccentricity:     
0004241     
Arg of perigee:   288
1040  deg
Mean anomaly:      71
9650  deg
Mean motion:   15
53189664  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3239
Checksum:              304


Coasting Arc #17 (Orbit 3253)
---------------------------------------

Vector Time (GMT): 2019/022/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4385325
22                 A    =         6784191
39  meter
 Y    =       -2863737
04  meter          E    =           
0004046
 Z    =       -4316098
68                 I    =           51
68619
 XDOT =       5794
598897                 Wp   =          108
32378
 YDOT =       3567
632313  meter/sec      RA   =            7
48129  deg
 ZDOT =       3521
879633                 TA   =          197
52967
                                          MA   =          197
54364
                                          Ha   =            221
213  n
mi
                                          Hp   =            217
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14387549
95                 X    =         4437987
03
 Y    =       -9395462
72  feet           Y    =        -2814402
57  meter
 Z    =      -14160428
73                 Z    =        -4294669
28
 XDOT =      19011
151238                 XDOT =        5737
167116
 YDOT =      11704
830422  feet/sec       YDOT =        3632
110224  meter/sec
 ZDOT =      11554
723205                 ZDOT =        3549
887554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16942824
19                 X    =        -5164172
81
 Y    =       -3310321
08  feet           Y    =        -1008985
86  meter
 Z    =      -14063304
66                 Z    =        -4286495
26
 XDOT =      -5717
296546                 XDOT =       -1742
631987
 YDOT =     -20340
322346  feet/sec       YDOT =       -6199
730251  meter/sec
 ZDOT =      11680
639531                 ZDOT =        3560
258929


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   19022
05334690  
00016717  00000-0  10270-3 0  9168
2 25544  51
6392   8
0424 0004316 291
6801  68
3891 15
53220753 32549


Satellite: ISS
Catalog Number: 25544
Epoch time:      19022
05334690   =   yrday
fracday
Element set:     916
Inclination:       51
6392  deg
RA of node:         8
0424  deg
Eccentricity:     
0004316     
Arg of perigee:   291
6801  deg
Mean anomaly:      68
3891  deg
Mean motion:   15
53220753  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3254
Checksum:              291
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