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

 
Date: January 6th 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 8

Coasting Arc #1 (Orbit 2981)
---------------------------------------

Vector Time (GMT): 2019/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2907981
77                 A    =         6786229
75  meter
 Y    =        5239982
44  meter          E    =           
0010534
 Z    =        3175906
37                 I    =           52
02920
 XDOT =      -3415
355615                 Wp   =           93
54033
 YDOT =      -4849
746281  meter/sec      RA   =           94
59674  deg
 ZDOT =       4859
973238                 TA   =          302
90072
                                          MA   =          303
00202
                                          Ha   =            220
927  n
mi
                                          Hp   =            216
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9540622
59                 X    =        -2981787
30
 Y    =       17191543
43  feet           Y    =         5207050
30  meter
 Z    =       10419640
32                 Z    =         3161601
94
 XDOT =     -11205
234958                 XDOT =       -3384
477475
 YDOT =     -15911
241081  feet/sec       YDOT =       -4887
767103  meter/sec
 ZDOT =      15944
794087                 ZDOT =        4843
457216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18906334
95                 X    =        -5762650
89
 Y    =       -5520646
80  feet           Y    =        -1682693
14  meter
 Z    =       10354443
82                 Z    =         3156034
48
 XDOT =      12574
039053                 XDOT =        3832
567103
 YDOT =     -13205
083076  feet/sec       YDOT =       -4024
909322  meter/sec
 ZDOT =      15870
822459                 ZDOT =        4837
426685


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   19004
55781685  
00016717  00000-0  10270-3 0  9006
2 25544  51
6423  95
1958 0002853 235
5131 124
5752 15
53743234 29822


Satellite: ISS
Catalog Number: 25544
Epoch time:      19004
55781685   =   yrday
fracday
Element set:     900
Inclination:       51
6423  deg
RA of node:        95
1958  deg
Eccentricity:     
0002853     
Arg of perigee:   235
5131  deg
Mean anomaly:     124
5752  deg
Mean motion:   15
53743234  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2982
Checksum:              312


Coasting Arc #2 (Orbit 2996)
---------------------------------------

Vector Time (GMT): 2019/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3338920
48                 A    =         6782743
55  meter
 Y    =       -4042291
02  meter          E    =           
0005524
 Z    =       -4308643
53                 I    =           52
01787
 XDOT =       2833
460849                 Wp   =           75
14875
 YDOT =       6153
368139  meter/sec      RA   =           89
64192  deg
 ZDOT =      -3579
672330                 TA   =          158
51135
                                          MA   =          158
48815
                                          Ha   =            220
886  n
mi
                                          Hp   =            216
316

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10954463
51                 X    =         3404803
16
 Y    =      -13262109
63  feet           Y    =        -4004583
99  meter
 Z    =      -14135969
57                 Z    =        -4292264
92
 XDOT =       9296
131394                 XDOT =        2781
829468
 YDOT =      20188
215678  feet/sec       YDOT =        6184
765614  meter/sec
 ZDOT =     -11744
331791                 ZDOT =       -3566
033221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15530473
95                 X    =         4733688
46
 Y    =        7535710
39  feet           Y    =         2296884
53  meter
 Z    =      -14061539
97                 Z    =        -4285957
38
 XDOT =     -16791
868480                 XDOT =       -5118
161513
 YDOT =      12820
404082  feet/sec       YDOT =        3907
659164  meter/sec
 ZDOT =     -11683
510019                 ZDOT =       -3561
133854


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   19005
52259619  
00016717  00000-0  10270-3 0  9012
2 25544  51
6412  90
3905 0002908 239
4399 120
6467 15
53718336 29970


Satellite: ISS
Catalog Number: 25544
Epoch time:      19005
52259619   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:        90
3905  deg
Eccentricity:     
0002908     
Arg of perigee:   239
4399  deg
Mean anomaly:     120
6467  deg
Mean motion:   15
53718336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2997
Checksum:              326


Coasting Arc #3 (Orbit 3012)
---------------------------------------

Vector Time (GMT): 2019/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3713029
15                 A    =         6779730
93  meter
 Y    =        2598520
43  meter          E    =           
0005026
 Z    =        5041847
20                 I    =           52
00758
 XDOT =      -2224
031891                 Wp   =          153
70368
 YDOT =      -7061
711262  meter/sec      RA   =           84
67785  deg
 ZDOT =       1996
524940                 TA   =          276
97615
                                          MA   =          277
03331
                                          Ha   =            220
818  n
mi
                                          Hp   =            216
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12181854
16                 X    =        -3766300
75
 Y    =        8525329
51  feet           Y    =         2556700
33  meter
 Z    =       16541493
44                 Z    =         5023681
84
 XDOT =      -7296
692557                 XDOT =       -2154
598443
 YDOT =     -23168
344035  feet/sec       YDOT =       -7086
193934  meter/sec
 ZDOT =       6550
278675                 ZDOT =        1985
889401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11400069
95                 X    =        -3474741
32
 Y    =       -9686803
24  feet           Y    =        -2952537
63  meter
 Z    =       16459163
63                 Z    =         5016753
07
 XDOT =      19795
698831                 XDOT =        6033
729004
 YDOT =     -12218
380445  feet/sec       YDOT =       -3724
162360  meter/sec
 ZDOT =       6503
135626                 ZDOT =        1982
155739


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   19006
55169009  
00016717  00000-0  10270-3 0  9020
2 25544  51
6419  85
2638 0002930 244
9652 115
1197 15
53758066 30134


Satellite: ISS
Catalog Number: 25544
Epoch time:      19006
55169009   =   yrday
fracday
Element set:     902
Inclination:       51
6419  deg
RA of node:        85
2638  deg
Eccentricity:     
0002930     
Arg of perigee:   244
9652  deg
Mean anomaly:     115
1197  deg
Mean motion:   15
53758066  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3013
Checksum:              308


Coasting Arc #4 (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    =        4063070
37                 A    =         6778560
11  meter
 Y    =        -995696
55  meter          E    =           
0012186
 Z    =       -5344217
94                 I    =           51
99847
 XDOT =       1541
314687                 Wp   =           92
12747
 YDOT =       7498
905494  meter/sec      RA   =           79
70812  deg
 ZDOT =       -226
204563                 TA   =          175
72976
                                          MA   =          175
71935
                                          Ha   =            220
715  n
mi
                                          Hp   =            216
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13330283
38                 X    =         4099861
39
 Y    =       -3266720
95  feet           Y    =         -950054
22  meter
 Z    =      -17533523
42                 Z    =        -5324392
12
 XDOT =       5056
806715                 XDOT =        1458
444026
 YDOT =      24602
708314  feet/sec       YDOT =        7515
678212  meter/sec
 ZDOT =       -742
140955                 ZDOT =        -218
918070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6823324
57                 X    =         2079749
33
 Y    =       12039324
67  feet           Y    =         3669586
16  meter
 Z    =      -17443889
12                 Z    =        -5316897
40
 XDOT =     -21400
254326                 XDOT =       -6522
797519
 YDOT =      11103
894361  feet/sec       YDOT =        3384
467001  meter/sec
 ZDOT =       -710
181152                 ZDOT =        -216
463215


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
51646522  
00016717  00000-0  10270-3 0  9038
2 25544  51
6413  80
4577 0002816 251
3099 108
7748 15
53720101 30282


Satellite: ISS
Catalog Number: 25544
Epoch time:      19007
51646522   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:        80
4577  deg
Eccentricity:     
0002816     
Arg of perigee:   251
3099  deg
Mean anomaly:     108
7748  deg
Mean motion:   15
53720101  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3028
Checksum:              294


Coasting Arc #5 (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    =       -4351312
85                 A    =         6779205
79  meter
 Y    =        -630455
26  meter          E    =           
0002437
 Z    =        5159469
48                 I    =           51
99408
 XDOT =       -772
650547                 Wp   =           30
80277
 YDOT =      -7467
876298  meter/sec      RA   =           74
73744  deg
 ZDOT =      -1561
791605                 TA   =           74
19023
                                          MA   =           74
16335
                                          Ha   =            220
753  n
mi
                                          Hp   =            216
228

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14275960
80                 X    =        -4369000
93
 Y    =       -2068422
77  feet           Y    =         -679214
01  meter
 Z    =       16927393
31                 Z    =         5138289
79
 XDOT =      -2534
942738                 XDOT =        -681
499049
 YDOT =     -24500
906489  feet/sec       YDOT =       -7476
006822  meter/sec
 ZDOT =      -5123
988206                 ZDOT =       -1565
324035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2197003
97                 X    =         -669646
81
 Y    =      -14369417
57  feet           Y    =        -4379798
48  meter
 Z    =       16831847
37                 Z    =         5130347
08
 XDOT =      21673
608802                 XDOT =        6606
115963
 YDOT =      -9342
547848  feet/sec       YDOT =       -2847
608584  meter/sec
 ZDOT =      -5138
993499                 ZDOT =       -1566
365219


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
54555491  
00016717  00000-0  10270-3 0  9047
2 25544  51
6412  75
3311 0002810 255
6948 104
3892 15
53769543 30447


Satellite: ISS
Catalog Number: 25544
Epoch time:      19008
54555491   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:        75
3311  deg
Eccentricity:     
0002810     
Arg of perigee:   255
6948  deg
Mean anomaly:     104
3892  deg
Mean motion:   15
53769543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3044
Checksum:              308


Coasting Arc #6 (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    =        4569004
07                 A    =         6781840
67  meter
 Y    =        2159268
14  meter          E    =           
0007480
 Z    =       -4530335
32                 I    =           51
99188
 XDOT =       -107
688257                 Wp   =          120
72104
 YDOT =       6956
264989  meter/sec      RA   =           69
77033  deg
 ZDOT =       3207
123718                 TA   =          181
37304
                                          MA   =          181
37509
                                          Ha   =            220
675  n
mi
                                          Hp   =            216
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14990170
85                 X    =         4566524
41
 Y    =        7084213
06  feet           Y    =         2210348
37  meter
 Z    =      -14863304
87                 Z    =        -4508147
09
 XDOT =       -353
307930                 XDOT =        -201
045309
 YDOT =      22822
391697  feet/sec       YDOT =        6954
538534  meter/sec
 ZDOT =      10522
059441                 ZDOT =        3206
374348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2115784
74                 X    =         -644891
19
 Y    =       16534044
08  feet           Y    =         5039576
64  meter
 Z    =      -14763399
66                 Z    =        -4499884
22
 XDOT =     -20648
189030                 XDOT =       -6293
568016
 YDOT =       6748
570045  feet/sec       YDOT =        2056
964150  meter/sec
 ZDOT =      10517
788569                 ZDOT =        3205
821956


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
51032767  
00016717  00000-0  10270-3 0  9052
2 25544  51
6402  70
5248 0002586 258
8473 101
2389 15
53756415 30597


Satellite: ISS
Catalog Number: 25544
Epoch time:      19009
51032767   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:        70
5248  deg
Eccentricity:     
0002586     
Arg of perigee:   258
8473  deg
Mean anomaly:     101
2389  deg
Mean motion:   15
53756415  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3059
Checksum:              313


Coasting Arc #7 (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    =        4651025
91                 A    =         6780658
97  meter
 Y    =        1095645
90  meter          E    =           
0009049
 Z    =       -4819553
60                 I    =           51
97859
 XDOT =       1028
133093                 Wp   =          116
30297
 YDOT =       7127
225288  meter/sec      RA   =           65
31343  deg
 ZDOT =       2612
327804                 TA   =          179
34903
                                          MA   =          179
34785
                                          Ha   =            220
608  n
mi
                                          Hp   =            216
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15259271
37                 X    =         4661838
73
 Y    =        3594638
78  feet           Y    =         1147717
63  meter
 Z    =      -15812183
71                 Z    =        -4796934
72
 XDOT =       3373
140068                 XDOT =         935
669026
 YDOT =      23383
285067  feet/sec       YDOT =        7138
205450  meter/sec
 ZDOT =       8570
629277                 ZDOT =        2617
097809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8049630
61                 X    =        -2453527
41
 Y    =       13571477
87  feet           Y    =         4136586
45  meter
 Z    =      -15710199
87                 Z    =        -4788468
92
 XDOT =     -22308
433610                 XDOT =       -6799
610564
 YDOT =      -3286
204449  feet/sec       YDOT =       -1001
635116  meter/sec
 ZDOT =       8591
249108                 ZDOT =        2618
612728


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
41077858  
00016717  00000-0  10270-3 0  9064
2 25544  51
6418  66
0374 0002674 260
1158  99
9693 15
53773369 30732


Satellite: ISS
Catalog Number: 25544
Epoch time:      19010
41077858   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:        66
0374  deg
Eccentricity:     
0002674     
Arg of perigee:   260
1158  deg
Mean anomaly:      99
9693  deg
Mean motion:   15
53773369  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3073
Checksum:              330


Coasting Arc #8 (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    =       -4942501
20                 A    =         6784017
40  meter
 Y    =       -2496675
14  meter          E    =           
0008638
 Z    =        3913306
01                 I    =           51
97482
 XDOT =         10
750119                 Wp   =           79
29831
 YDOT =      -6475
714359  meter/sec      RA   =           60
34925  deg
 ZDOT =      -4108
671649                 TA   =           53
59264
                                          MA   =           53
51300
                                          Ha   =            220
736  n
mi
                                          Hp   =            216
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16215555
11                 X    =        -4933223
71
 Y    =       -8191191
40  feet           Y    =        -2551893
91  meter
 Z    =       12838930
47                 Z    =         3889319
99
 XDOT =         35
269418                 XDOT =         103
119914
 YDOT =     -21245
782019  feet/sec       YDOT =       -6475
077511  meter/sec
 ZDOT =     -13479
893861                 ZDOT =       -4108
395339

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12488253
70                 X    =         3806419
73
 Y    =      -13298277
23  feet           Y    =        -4053314
90  meter
 Z    =       12730959
19                 Z    =         3880396
36
 XDOT =      19363
938608                 XDOT =        5902
128488
 YDOT =       5252
368634  feet/sec       YDOT =        1600
921960  meter/sec
 ZDOT =     -13477
805349                 ZDOT =       -4108
035070


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
43986395  
00016717  00000-0  10270-3 0  9073
2 25544  51
6418  60
9103 0002622 267
1431  92
9421 15
53759400 30898


Satellite: ISS
Catalog Number: 25544
Epoch time:      19011
43986395   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:        60
9103  deg
Eccentricity:     
0002622     
Arg of perigee:   267
1431  deg
Mean anomaly:      92
9421  deg
Mean motion:   15
53759400  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3089
Checksum:              305


Coasting Arc #9 (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    =        5059202
44                 A    =         6787515
81  meter
 Y    =        3646256
33  meter          E    =           
0003246
 Z    =       -2676121
10                 I    =           51
96806
 XDOT =      -1186
630268                 Wp   =           22
89530
 YDOT =       5479
007067  meter/sec      RA   =           55
39326  deg
 ZDOT =       5226
943500                 TA   =          307
06147
                                          MA   =          307
09115
                                          Ha   =            220
644  n
mi
                                          Hp   =            216
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16598433
22                 X    =         5031051
92
 Y    =       11962783
22  feet           Y    =         3702674
53  meter
 Z    =       -8779924
87                 Z    =        -2651613
97
 XDOT =      -3893
143923                 XDOT =       -1273
199136
 YDOT =      17975
744971  feet/sec       YDOT =        5465
253148  meter/sec
 ZDOT =      17148
764763                 ZDOT =        5220
969275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15986994
56                 X    =        -4872835
94
 Y    =       12843463
07  feet           Y    =         3914687
54  meter
 Z    =       -8669758
36                 Z    =        -2642542
35
 XDOT =     -15309
840754                 XDOT =       -4666
439462
 YDOT =      -7511
041588  feet/sec       YDOT =       -2289
365476  meter/sec
 ZDOT =      17121
073600                 ZDOT =        5218
503233


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
40463066  
00016717  00000-0  10270-3 0  9087
2 25544  51
6410  56
1043 0002760 270
8212  89
2625 15
53733454 31045


Satellite: ISS
Catalog Number: 25544
Epoch time:      19012
40463066   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:        56
1043  deg
Eccentricity:     
0002760     
Arg of perigee:   270
8212  deg
Mean anomaly:      89
2625  deg
Mean motion:   15
53733454  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3104
Checksum:              276


Coasting Arc #10 (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    =       -4924638
76                 A    =         6789852
23  meter
 Y    =       -4514460
68  meter          E    =           
0011394
 Z    =        1178141
01                 I    =           51
95659
 XDOT =       2473
025266                 Wp   =          128
25861
 YDOT =      -4243
050008  meter/sec      RA   =           50
44355  deg
 ZDOT =      -5889
833343                 TA   =           39
00184
                                          MA   =           38
91973
                                          Ha   =            220
640  n
mi
                                          Hp   =            216
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16156951
30                 X    =        -4879513
48
 Y    =      -14811222
70  feet           Y    =        -4569279
14  meter
 Z    =        3865292
02                 Z    =         1154328
67
 XDOT =       8113
599954                 XDOT =        2548
897705
 YDOT =     -13920
767742  feet/sec       YDOT =       -4214
970527  meter/sec
 ZDOT =     -19323
600206                 ZDOT =       -5877
636267

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18401928
89                 X    =         5608907
92
 Y    =      -11941667
19  feet           Y    =        -3639820
16  meter
 Z    =        3758387
13                 Z    =         1145556
40
 XDOT =      10533
616276                 XDOT =        3210
646241
 YDOT =      10134
360791  feet/sec       YDOT =        3088
953169  meter/sec
 ZDOT =     -19267
972432                 ZDOT =       -5872
877997


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
43371379  
00016717  00000-0  10270-3 0  9097
2 25544  51
6412  50
9774 0002633 275
3666  84
7186 15
53757893 31205


Satellite: ISS
Catalog Number: 25544
Epoch time:      19013
43371379   =   yrday
fracday
Element set:     909
Inclination:       51
6412  deg
RA of node:        50
9774  deg
Eccentricity:     
0002633     
Arg of perigee:   275
3666  deg
Mean anomaly:      84
7186  deg
Mean motion:   15
53757893  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3120
Checksum:              326


Coasting Arc #11 (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    =        4517269
12                 A    =         6790436
16  meter
 Y    =        5045268
41  meter          E    =           
0011542
 Z    =         402074
37                 I    =           51
93651
 XDOT =      -3770
519576                 Wp   =           38
63642
 YDOT =       2889
425816  meter/sec      RA   =           45
49558  deg
 ZDOT =       6020
528975                 TA   =          325
68077
                                          MA   =          325
75529
                                          Ha   =            220
750  n
mi
                                          Hp   =            216
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14820436
75                 X    =         4458562
74
 Y    =       16552717
89  feet           Y    =         5095455
40  meter
 Z    =        1319141
63                 Z    =          423875
00
 XDOT =     -12370
471049                 XDOT =       -3831
793898
 YDOT =       9479
743492  feet/sec       YDOT =        2846
918439  meter/sec
 ZDOT =      19752
391651                 ZDOT =        6002
064602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19565420
67                 X    =        -5963540
22
 Y    =       10514975
51  feet           Y    =         3204964
54  meter
 Z    =        1416881
69                 Z    =          431865
54
 XDOT =      -5517
054570                 XDOT =       -1681
598233
 YDOT =     -12950
643853  feet/sec       YDOT =       -3947
356246  meter/sec
 ZDOT =      19668
648248                 ZDOT =        5995
003986


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
46279550  
00016717  00000-0  10270-3 0  9101
2 25544  51
6415  45
8501 0002626 284
8161  75
2700 15
53721480 31363


Satellite: ISS
Catalog Number: 25544
Epoch time:      19014
46279550   =   yrday
fracday
Element set:     910
Inclination:       51
6415  deg
RA of node:        45
8501  deg
Eccentricity:     
0002626     
Arg of perigee:   284
8161  deg
Mean anomaly:      75
2700  deg
Mean motion:   15
53721480  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3136
Checksum:              288


Coasting Arc #12 (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    =       -3789375
53                 A    =         6788709
63  meter
 Y    =       -5273978
63  meter          E    =           
0004866
 Z    =       -1969992
07                 I    =           51
90636
 XDOT =       5004
326451                 Wp   =          156
23080
 YDOT =      -1504
304164  meter/sec      RA   =           40
54582  deg
 ZDOT =      -5607
954797                 TA   =           45
41387
                                          MA   =           45
37416
                                          Ha   =            220
704  n
mi
                                          Hp   =            216
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12432334
42                 X    =        -3720549
71
 Y    =      -17303079
48  feet           Y    =        -5315969
14  meter
 Z    =       -6463228
57                 Z    =        -1988232
41
 XDOT =      16418
393868                 XDOT =        5048
016263
 YDOT =      -4935
381117  feet/sec       YDOT =       -1448
097763  meter/sec
 ZDOT =     -18398
801828                 ZDOT =       -5583
539731

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19586695
14                 X    =         5970024
68
 Y    =       -8322204
90  feet           Y    =        -2536608
05  meter
 Z    =       -6544853
05                 Z    =        -1994871
21
 XDOT =        608
234791                 XDOT =         185
389964
 YDOT =      15790
778887  feet/sec       YDOT =        4813
029405  meter/sec
 ZDOT =     -18288
382830                 ZDOT =       -5574
299087


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
42755708  
00016717  00000-0  10270-3 0  9113
2 25544  51
6407  41
0442 0002515 286
4189  73
6686 15
53760593 31511


Satellite: ISS
Catalog Number: 25544
Epoch time:      19015
42755708   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:        41
0442  deg
Eccentricity:     
0002515     
Arg of perigee:   286
4189  deg
Mean anomaly:      73
6686  deg
Mean motion:   15
53760593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3151
Checksum:              308


Coasting Arc #13 (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    =       -5933484
33                 A    =         6786992
06  meter
 Y    =       -1551674
54  meter          E    =           
0010853
 Z    =        2895423
82                 I    =           51
87919
 XDOT =       -995
556540                 Wp   =           98
30255
 YDOT =      -5671
742482  meter/sec      RA   =           36
39891  deg
 ZDOT =      -5065
011632                 TA   =           48
83234
                                          MA   =           48
73877
                                          Ha   =            220
797  n
mi
                                          Hp   =            216
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19466812
10                 X    =        -5929756
38
 Y    =       -5090795
73  feet           Y    =        -1618006
22  meter
 Z    =        9499421
98                 Z    =         2866610
27
 XDOT =      -3266
261613                 XDOT =        -907
456629
 YDOT =     -18608
079009  feet/sec       YDOT =       -5682
382588  meter/sec
 ZDOT =     -16617
492231                 ZDOT =       -5069
634013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20178359
74                 X    =         6150364
05
 Y    =        -396196
25  feet           Y    =         -120760
62  meter
 Z    =        9369568
77                 Z    =         2855844
56
 XDOT =       8054
112353                 XDOT =        2454
893445
 YDOT =      15585
127012  feet/sec       YDOT =        4750
346713  meter/sec
 ZDOT =     -16637
579813                 ZDOT =       -5071
134327


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
26368433  
00016717  00000-0  10270-3 0  9122
2 25544  51
6410  36
8758 0002487 281
7041  78
3832 15
53743824 31647


Satellite: ISS
Catalog Number: 25544
Epoch time:      19016
26368433   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:        36
8758  deg
Eccentricity:     
0002487     
Arg of perigee:   281
7041  deg
Mean anomaly:      78
3832  deg
Mean motion:   15
53743824  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3164
Checksum:              313


Coasting Arc #14 (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    =        6165026
29                 A    =         6789589
89  meter
 Y    =        2433934
62  meter          E    =           
0008216
 Z    =       -1451025
71                 I    =           51
86186
 XDOT =       -601
575415                 Wp   =           19
98271
 YDOT =       4973
661075  meter/sec      RA   =           31
44175  deg
 ZDOT =       5804
031271                 TA   =          324
23993
                                          MA   =          324
29492
                                          Ha   =            220
830  n
mi
                                          Hp   =            216
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20226464
21                 X    =         6144399
39
 Y    =        7985349
79  feet           Y    =         2502761
02  meter
 Z    =       -4760583
05                 Z    =        -1421128
39
 XDOT =      -1973
672623                 XDOT =        -685
340184
 YDOT =      16317
785679  feet/sec       YDOT =        4966
465019  meter/sec
 ZDOT =      19042
097346                 ZDOT =        5800
906008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21698555
35                 X    =        -6613719
67
 Y    =       -1819875
26  feet           Y    =         -554697
98  meter
 Z    =       -4625966
52                 Z    =        -1409994
59
 XDOT =      -2815
267678                 XDOT =        -858
093588
 YDOT =     -14651
406940  feet/sec       YDOT =       -4465
748835  meter/sec
 ZDOT =      19027
299989                 ZDOT =        5799
521037


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
22844329  
00016717  00000-0  10270-3 0  9133
2 25544  51
6422  32
0694 0002535 291
3858  68
7023 15
53748016 31793


Satellite: ISS
Catalog Number: 25544
Epoch time:      19017
22844329   =   yrday
fracday
Element set:     913
Inclination:       51
6422  deg
RA of node:        32
0694  deg
Eccentricity:     
0002535     
Arg of perigee:   291
3858  deg
Mean anomaly:      68
7023  deg
Mean motion:   15
53748016  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3179
Checksum:              310


Coasting Arc #15 (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    =       -6018636
31                 A    =         6790381
49  meter
 Y    =       -3129886
69  meter          E    =           
0009499
 Z    =        -148863
26                 I    =           51
83485
 XDOT =       2299
582849                 Wp   =          141
43087
 YDOT =      -4145
568749  meter/sec      RA   =           26
48770  deg
 ZDOT =      -6025
966528                 TA   =           40
16809
                                          MA   =           40
09792
                                          Ha   =            220
781  n
mi
                                          Hp   =            216
094

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19746182
13                 X    =        -5982466
64
 Y    =      -10268657
11  feet           Y    =        -3196989
02  meter
 Z    =        -488396
52                 Z    =         -178011
75
 XDOT =       7544
563152                 XDOT =        2375
039399
 YDOT =     -13600
947338  feet/sec       YDOT =       -4119
430722  meter/sec
 ZDOT =     -19770
231390                 ZDOT =       -6014
613246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21930204
41                 X    =         6684326
31
 Y    =        3778607
67  feet           Y    =         1151719
62  meter
 Z    =        -619529
85                 Z    =         -188832
70
 XDOT =      -2900
810018                 XDOT =        -884
166894
 YDOT =      13693
423649  feet/sec       YDOT =        4173
755528  meter/sec
 ZDOT =     -19718
403894                 ZDOT =       -6010
169507


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
25751862  
00016717  00000-0  10270-3 0  9147
2 25544  51
6413  26
9426 0002470 293
2973  66
7919 15
53761010 31954


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
25751862   =   yrday
fracday
Element set:     914
Inclination:       51
6413  deg
RA of node:        26
9426  deg
Eccentricity:     
0002470     
Arg of perigee:   293
2973  deg
Mean anomaly:      66
7919  deg
Mean motion:   15
53761010  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3195
Checksum:              315


Coasting Arc #16 (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    =        1664383
97                 A    =         6779971
69  meter
 Y    =       -3855313
68  meter          E    =           
0010548
 Z    =       -5332067
23                 I    =           51
77907
 XDOT =       7015
323942                 Wp   =           83
96205
 YDOT =       3074
381624  meter/sec      RA   =           23
85382  deg
 ZDOT =        -32
076778                 TA   =          185
72649
                                          MA   =          185
73856
                                          Ha   =            220
914  n
mi
                                          Hp   =            217
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5460577
34                 X    =         1733271
41
 Y    =      -12648666
94  feet           Y    =        -3836315
66  meter
 Z    =      -17493658
90                 Z    =        -5323815
45
 XDOT =      23016
154664                 XDOT =        6980
579761
 YDOT =      10086
553885  feet/sec       YDOT =        3152
637597  meter/sec
 ZDOT =       -105
238774                 ZDOT =           1
916595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1286652
01                 X    =         -392171
53
 Y    =      -13764879
40  feet           Y    =        -4195535
24  meter
 Z    =      -17455870
18                 Z    =        -5320549
23
 XDOT =      24011
382140                 XDOT =        7318
669276
 YDOT =      -2300
723681  feet/sec       YDOT =        -701
260578  meter/sec
 ZDOT =         47
768900                 ZDOT =          14
559961


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
77205864  
00016717  00000-0  10270-3 0  9151
2 25544  51
6414  24
3827 0004498 283
6396  76
4255 15
53229932 32039


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
77205864   =   yrday
fracday
Element set:     915
Inclination:       51
6414  deg
RA of node:        24
3827  deg
Eccentricity:     
0004498     
Arg of perigee:   283
6396  deg
Mean anomaly:      76
4255  deg
Mean motion:   15
53229932  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3203
Checksum:              324
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