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

 
Date: January 13th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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


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

018/18:05:10 953 3 0 3 2 3 2
N/A 0 8 0 0 220 9
000/00:08:17 907 -0 6 -0 0 217 9

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 9

025/12:55:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 217 5

026/08:59:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 217 4

Coasting Arc #1 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2019/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4566338
91                 A    =         6788521
90  meter
 Y    =        4544137
99  meter          E    =           
0005200
 Z    =       -2132661
17                 I    =           51
98695
 XDOT =      -2209
931963                 Wp   =           19
33295
 YDOT =       4816
285216  meter/sec      RA   =           59
85727  deg
 ZDOT =       5539
066230                 TA   =          317
15800
                                          MA   =          317
19850
                                          Ha   =            220
695  n
mi
                                          Hp   =            216
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14981426
86                 X    =         4525544
83
 Y    =       14908589
20  feet           Y    =         4594973
96  meter
 Z    =       -6996919
86                 Z    =        -2110578
85
 XDOT =      -7250
432950                 XDOT =       -2290
530071
 YDOT =      15801
460683  feet/sec       YDOT =        4791
121354  meter/sec
 ZDOT =      18172
789470                 ZDOT =        5528
135801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8927760
66                 X    =        -2721181
45
 Y    =       19193263
71  feet           Y    =         5850106
78  meter
 Z    =       -6897810
36                 Z    =        -2102452
60
 XDOT =     -15966
687775                 XDOT =       -4866
646434
 YDOT =       -924
122925  feet/sec       YDOT =        -281
672668  meter/sec
 ZDOT =      18122
813187                 ZDOT =        5523
833459


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
50416252  
00016717  00000-0  10270-3 0  9004
2 25544  51
6404  60
5908 0002501 271
5814  88
5052 15
53760647 30900


Satellite: ISS
Catalog Number: 25544
Epoch time:      19011
50416252   =   yrday
fracday
Element set:     900
Inclination:       51
6404  deg
RA of node:        60
5908  deg
Eccentricity:     
0002501     
Arg of perigee:   271
5814  deg
Mean anomaly:      88
5052  deg
Mean motion:   15
53760647  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3090
Checksum:              278


Coasting Arc #2 (Orbit 3105)
---------------------------------------

Vector Time (GMT): 2019/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4246007
44                 A    =         6790238
86  meter
 Y    =       -5259917
30  meter          E    =           
0011012
 Z    =         576248
24                 I    =           51
97546
 XDOT =       3364
093521                 Wp   =          135
76068
 YDOT =      -3380
216821  meter/sec      RA   =           54
91038  deg
 ZDOT =      -6005
078287                 TA   =           38
04944
                                          MA   =           37
97171
                                          Ha   =            220
667  n
mi
                                          Hp   =            216
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13930470
61                 X    =        -4189673
06
 Y    =      -17256946
51  feet           Y    =        -5307084
14  meter
 Z    =        1890578
22                 Z    =          555759
66
 XDOT =      11037
052233                 XDOT =        3430
811001
 YDOT =     -11089
950199  feet/sec       YDOT =       -3342
223967  meter/sec
 ZDOT =     -19701
700416                 ZDOT =       -5988
575042

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11177279
84                 X    =         3406834
89
 Y    =      -19164220
61  feet           Y    =        -5841254
44  meter
 Z    =        1798767
35                 Z    =          548264
29
 XDOT =      12938
237228                 XDOT =        3943
574707
 YDOT =       5684
061308  feet/sec       YDOT =        1732
501887  meter/sec
 ZDOT =     -19626
747923                 ZDOT =       -5982
232767


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
53324361  
00016717  00000-0  10270-3 0  9018
2 25544  51
6406  55
4636 0002475 276
7729  83
3141 15
53772113 31066


Satellite: ISS
Catalog Number: 25544
Epoch time:      19012
53324361   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:        55
4636  deg
Eccentricity:     
0002475     
Arg of perigee:   276
7729  deg
Mean anomaly:      83
3141  deg
Mean motion:   15
53772113  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3106
Checksum:              288


Coasting Arc #3 (Orbit 3121)
---------------------------------------

Vector Time (GMT): 2019/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3681934
85                 A    =         6790056
71  meter
 Y    =        5607478
93  meter          E    =           
0012162
 Z    =        1007051
17                 I    =           51
95455
 XDOT =      -4486
938093                 Wp   =           47
27782
 YDOT =       1874
392737  meter/sec      RA   =           49
96397  deg
 ZDOT =       5930
658019                 TA   =          323
58818
                                          MA   =          323
67085
                                          Ha   =            220
822  n
mi
                                          Hp   =            216
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12079838
76                 X    =         3614065
15
 Y    =       18397240
59  feet           Y    =         5648273
38  meter
 Z    =        3303973
67                 Z    =         1024771
78
 XDOT =     -14720
925501                 XDOT =       -4536
372173
 YDOT =       6149
582471  feet/sec       YDOT =        1823
940105  meter/sec
 ZDOT =      19457
539434                 ZDOT =        5908
742347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12605125
54                 X    =        -3842042
26
 Y    =       18026695
99  feet           Y    =         5494536
94  meter
 Z    =        3383230
62                 Z    =         1031208
69
 XDOT =      -9910
897846                 XDOT =       -3020
841663
 YDOT =     -10585
729906  feet/sec       YDOT =       -3226
530475  meter/sec
 ZDOT =      19358
350195                 ZDOT =        5900
425139


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
56232475  
00016717  00000-0  10270-3 0  9027
2 25544  51
6407  50
3365 0002390 285
9572  74
1317 15
53724412 31224


Satellite: ISS
Catalog Number: 25544
Epoch time:      19013
56232475   =   yrday
fracday
Element set:     902
Inclination:       51
6407  deg
RA of node:        50
3365  deg
Eccentricity:     
0002390     
Arg of perigee:   285
9572  deg
Mean anomaly:      74
1317  deg
Mean motion:   15
53724412  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3122
Checksum:              285


Coasting Arc #4 (Orbit 3136)
---------------------------------------

Vector Time (GMT): 2019/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2828939
94                 A    =         6787621
40  meter
 Y    =       -5628401
50  meter          E    =           
0003097
 Z    =       -2525173
29                 I    =           51
92607
 XDOT =       5505
966651                 Wp   =          146
42525
 YDOT =       -384
116188  meter/sec      RA   =           45
01326  deg
 ZDOT =      -5317
766372                 TA   =           61
78147
                                          MA   =           61
75020
                                          Ha   =            220
720  n
mi
                                          Hp   =            216
068

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9281299
01                 X    =        -2753525
51
 Y    =      -18465884
17  feet           Y    =        -5659614
92  meter
 Z    =       -8284689
27                 Z    =        -2538732
15
 XDOT =      18064
195049                 XDOT =        5535
683314
 YDOT =      -1260
223715  feet/sec       YDOT =        -322
378301  meter/sec
 ZDOT =     -17446
740066                 ZDOT =       -5290
948466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13453328
81                 X    =         4100574
62
 Y    =      -15656755
54  feet           Y    =        -4772179
09  meter
 Z    =       -8345143
24                 Z    =        -2543599
66
 XDOT =       7061
290277                 XDOT =        2152
281276
 YDOT =      15292
433163  feet/sec       YDOT =        4661
133628  meter/sec
 ZDOT =     -17325
622021                 ZDOT =       -5280
849592


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
52708283  
00016717  00000-0  10270-3 0  9030
2 25544  51
6420  45
5302 0002441 287
2214  72
8672 15
53772130 31376


Satellite: ISS
Catalog Number: 25544
Epoch time:      19014
52708283   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:        45
5302  deg
Eccentricity:     
0002441     
Arg of perigee:   287
2214  deg
Mean anomaly:      72
8672  deg
Mean motion:   15
53772130  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3137
Checksum:              280


Coasting Arc #5 (Orbit 3152)
---------------------------------------

Vector Time (GMT): 2019/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929656
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1734068
20                 A    =         6784301
71  meter
 Y    =        5345267
89  meter          E    =           
0009280
 Z    =        3793429
34                 I    =           51
88851
 XDOT =      -6317
879818                 Wp   =           92
80169
 YDOT =       -966
142991  meter/sec      RA   =           40
05312  deg
 ZDOT =       4240
064041                 TA   =          312
52256
                                          MA   =          312
60090
                                          Ha   =            220
860  n
mi
                                          Hp   =            216
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5689200
13                 X    =         1655740
75
 Y    =       17536968
14  feet           Y    =         5364221
32  meter
 Z    =       12445634
33                 Z    =         3801662
76
 XDOT =     -20727
952160                 XDOT =       -6327
202353
 YDOT =      -3169
760468  feet/sec       YDOT =       -1036
846246  meter/sec
 ZDOT =      13910
971263                 ZDOT =        4209
351612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13791059
10                 X    =        -4203514
81
 Y    =       12198793
47  feet           Y    =         3718192
25  meter
 Z    =       12482074
77                 Z    =         3804536
39
 XDOT =      -4601
697899                 XDOT =       -1402
597520
 YDOT =     -19325
990766  feet/sec       YDOT =       -5890
561985  meter/sec
 ZDOT =      13772
460937                 ZDOT =        4197
846094


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
55616035  
00016717  00000-0  10270-3 0  9048
2 25544  51
6401  40
4030 0002301 294
1862  65
9049 15
53746543 31536


Satellite: ISS
Catalog Number: 25544
Epoch time:      19015
55616035   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:        40
4030  deg
Eccentricity:     
0002301     
Arg of perigee:   294
1862  deg
Mean anomaly:      65
9049  deg
Mean motion:   15
53746543  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3153
Checksum:              278


Coasting Arc #6 (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    =       -5936432
44                 A    =         6787014
29  meter
 Y    =       -1568452
16  meter          E    =           
0010891
 Z    =        2880370
15                 I    =           51
87930
 XDOT =       -973
125420                 Wp   =           98
24627
 YDOT =      -5665
809074  meter/sec      RA   =           36
39825  deg
 ZDOT =      -5075
968900                 TA   =           49
08108
                                          MA   =           48
98683
                                          Ha   =            220
803  n
mi
                                          Hp   =            216
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19476484
38                 X    =        -5932443
53
 Y    =       -5145840
41  feet           Y    =        -1634815
35  meter
 Z    =        9450033
31                 Z    =         2851542
91
 XDOT =      -3192
668700                 XDOT =        -885
040301
 YDOT =     -18588
612446  feet/sec       YDOT =       -5676
198422  meter/sec
 ZDOT =     -16653
441273                 ZDOT =       -5080
482355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20202278
59                 X    =         6157654
51
 Y    =        -345743
50  feet           Y    =         -105382
62  meter
 Z    =        9320120
62                 Z    =         2840772
76
 XDOT =       7981
448348                 XDOT =        2432
745456
 YDOT =      15584
667802  feet/sec       YDOT =        4750
206746  meter/sec
 ZDOT =     -16673
037970                 ZDOT =       -5081
941973


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
26365000  
00016717  00000-0  10270-3 0  9051
2 25544  51
6409  36
8754 0002471 283
2585  76
8292 15
53748716 31642


Satellite: ISS
Catalog Number: 25544
Epoch time:      19016
26365000   =   yrday
fracday
Element set:     905
Inclination:       51
6409  deg
RA of node:        36
8754  deg
Eccentricity:     
0002471     
Arg of perigee:   283
2585  deg
Mean anomaly:      76
8292  deg
Mean motion:   15
53748716  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3164
Checksum:              317


Coasting Arc #7 (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    =        6163032
09                 A    =         6789597
41  meter
 Y    =        2449842
90  meter          E    =           
0008337
 Z    =       -1432329
04                 I    =           51
86192
 XDOT =       -626
903651                 Wp   =           20
19301
 YDOT =       4963
645519  meter/sec      RA   =           31
44114  deg
 ZDOT =       5810
015391                 TA   =          324
23799
                                          MA   =          324
29379
                                          Ha   =            220
841  n
mi
                                          Hp   =            216
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20219921
57                 X    =         6142136
64
 Y    =        8037542
32  feet           Y    =         2518645
50  meter
 Z    =       -4699242
24                 Z    =        -1402442
05
 XDOT =      -2056
770509                 XDOT =        -710
583608
 YDOT =      16284
926243  feet/sec       YDOT =        4956
166698  meter/sec
 ZDOT =      19061
730287                 ZDOT =        5806
767299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21706912
66                 X    =        -6616266
98
 Y    =       -1871865
79  feet           Y    =         -570544
69  meter
 Z    =       -4564674
58                 Z    =        -1391312
81
 XDOT =      -2729
897484                 XDOT =        -832
072753
 YDOT =     -14643
270531  feet/sec       YDOT =       -4463
268858  meter/sec
 ZDOT =      19046
379877                 ZDOT =        5805
336587


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
22840598  
00016717  00000-0  10270-3 0  9069
2 25544  51
6422  32
0689 0002525 292
9268  67
1618 15
53753076 31793


Satellite: ISS
Catalog Number: 25544
Epoch time:      19017
22840598   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:        32
0689  deg
Eccentricity:     
0002525     
Arg of perigee:   292
9268  deg
Mean anomaly:      67
1618  deg
Mean motion:   15
53753076  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3179
Checksum:              326


Coasting Arc #8 (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    =       -6010596
70                 A    =         6790363
35  meter
 Y    =       -3144320
54  meter          E    =           
0009436
 Z    =        -169954
35                 I    =           51
83482
 XDOT =       2326
401623                 Wp   =          141
27220
 YDOT =      -4131
558123  meter/sec      RA   =           26
48709  deg
 ZDOT =      -6025
220903                 TA   =           40
55336
                                          MA   =           40
48310
                                          Ha   =            220
793  n
mi
                                          Hp   =            216
072

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19719805
45                 X    =        -5974163
77
 Y    =      -10316012
26  feet           Y    =        -3211331
49  meter
 Z    =        -557593
00                 Z    =         -199063
14
 XDOT =       7632
551257                 XDOT =        2401
695888
 YDOT =     -13554
980717  feet/sec       YDOT =       -4105
121097  meter/sec
 ZDOT =     -19767
785115                 ZDOT =       -6013
737740

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21919039
61                 X    =         6680923
27
 Y    =        3831886
45  feet           Y    =         1167958
99  meter
 Z    =        -688545
15                 Z    =         -209868
56
 XDOT =      -2994
707012                 XDOT =        -912
786697
 YDOT =      13677
199925  feet/sec       YDOT =        4168
810537  meter/sec
 ZDOT =     -19715
373316                 ZDOT =       -6009
245787


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
25747813  
00016717  00000-0  10270-3 0  9070
2 25544  51
6412  26
9421 0002459 294
8943  65
1953 15
53765995 31956


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
25747813   =   yrday
fracday
Element set:     907
Inclination:       51
6412  deg
RA of node:        26
9421  deg
Eccentricity:     
0002459     
Arg of perigee:   294
8943  deg
Mean anomaly:      65
1953  deg
Mean motion:   15
53765995  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3195
Checksum:              340


Coasting Arc #9 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2019/018/18:09:19
907
Vector Time (MET): N/A
Weight (LBS)     : 929313
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1985793
94                 A    =         6780174
49  meter
 Y    =       -3708264
46  meter          E    =           
0010210
 Z    =       -5326313
61                 I    =           51
77914
 XDOT =       6908
307867                 Wp   =           86
96914
 YDOT =       3296
327194  meter/sec      RA   =           23
84789  deg
 ZDOT =        281
640757                 TA   =          185
70760
                                          MA   =          185
71925
                                          Ha   =            220
946  n
mi
                                          Hp   =            217
944

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6515071
99                 X    =         2052985
19
 Y    =      -12166221
98  feet           Y    =        -3685681
69  meter
 Z    =      -17474782
17                 Z    =        -5316504
66
 XDOT =      22665
052056                 XDOT =        6869
565934
 YDOT =      10814
721766  feet/sec       YDOT =        3373
364054  meter/sec
 ZDOT =        924
018231                 ZDOT =         315
104605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -173796
58                 X    =          -52973
20
 Y    =      -13856281
53  feet           Y    =        -4223394
61  meter
 Z    =      -17429985
35                 Z    =        -5312659
53
 XDOT =      24041
529992                 XDOT =        7327
858342
 YDOT =      -1649
201451  feet/sec       YDOT =        -502
676602  meter/sec
 ZDOT =       1074
604527                 ZDOT =         327
539460


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
77201666  
00016717  00000-0  10270-3 0  9089
2 25544  51
6413  24
3823 0004734 283
7007  76
3618 15
53172378 32030


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
77201666   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:        24
3823  deg
Eccentricity:     
0004734     
Arg of perigee:   283
7007  deg
Mean anomaly:      76
3618  deg
Mean motion:   15
53172378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3203
Checksum:              303


Coasting Arc #10 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2019/019/18:09:19
907
Vector Time (MET): N/A
Weight (LBS)     : 929313
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3254932
85                 A    =         6781240
41  meter
 Y    =        3112265
33  meter          E    =           
0004620
 Z    =        5071334
03                 I    =           51
75188
 XDOT =      -6438
812124                 Wp   =          358
55429
 YDOT =      -3731
669608  meter/sec      RA   =           18
86817  deg
 ZDOT =      -1838
032132                 TA   =          109
24783
                                          MA   =          109
19784
                                          Ha   =            221
057  n
mi
                                          Hp   =            217
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10678913
54                 X    =        -3314126
47
 Y    =       10210844
26  feet           Y    =         3075534
89  meter
 Z    =       16638235
01                 Z    =         5055379
62
 XDOT =     -21124
711692                 XDOT =       -6387
677016
 YDOT =     -12243
010526  feet/sec       YDOT =       -3803
386779  meter/sec
 ZDOT =      -6030
289147                 ZDOT =       -1869
185142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4164631
37                 X    =        -1269379
64
 Y    =       14260509
53  feet           Y    =         4346603
30  meter
 Z    =       16565781
38                 Z    =         5049250
17
 XDOT =     -23341
070035                 XDOT =       -7114
358147
 YDOT =        368
454611  feet/sec       YDOT =         112
304966  meter/sec
 ZDOT =      -6170
380538                 ZDOT =       -1880
731988


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
80148956  
00016717  00000-0  10270-3 0  9097
2 25544  51
6411  19
2583 0004940 287
3495  72
7117 15
53195864 32190


Satellite: ISS
Catalog Number: 25544
Epoch time:      19019
80148956   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:        19
2583  deg
Eccentricity:     
0004940     
Arg of perigee:   287
3495  deg
Mean anomaly:      72
7117  deg
Mean motion:   15
53195864  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3219
Checksum:              331


Coasting Arc #11 (Orbit 3222)
---------------------------------------

Vector Time (GMT): 2019/020/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929313
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1825433
90                 A    =         6780249
59  meter
 Y    =       -3814950
60  meter          E    =           
0010194
 Z    =       -5308400
83                 I    =           51
73711
 XDOT =       7153
419074                 Wp   =           89
90045
 YDOT =       2686
402156  meter/sec      RA   =           17
44627  deg
 ZDOT =        530
171995                 TA   =          185
15174
                                          MA   =          185
16223
                                          Ha   =            220
984  n
mi
                                          Hp   =            217
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5988956
37                 X    =         1893742
86
 Y    =      -12516242
13  feet           Y    =        -3794154
84  meter
 Z    =      -17416013
21                 Z    =        -5299368
21
 XDOT =      23469
222684                 XDOT =        7120
272085
 YDOT =       8813
655366  feet/sec       YDOT =        2766
211277  meter/sec
 ZDOT =       1739
409431                 ZDOT =         564
839749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13245638
47                 X    =        -4037270
61
 Y    =        4302808
09  feet           Y    =         1311495
91  meter
 Z    =      -17374703
90                 Z    =        -5295809
75
 XDOT =      -9639
228247                 XDOT =       -2938
036770
 YDOT =     -22030
969588  feet/sec       YDOT =       -6715
039531  meter/sec
 ZDOT =       1895
512589                 ZDOT =         577
752237


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
05885833  
00016717  00000-0  10270-3 0  9100
2 25544  51
6389  17
9725 0004586 283
6838  76
3803 15
53172584 32234


Satellite: ISS
Catalog Number: 25544
Epoch time:      19020
05885833   =   yrday
fracday
Element set:     910
Inclination:       51
6389  deg
RA of node:        17
9725  deg
Eccentricity:     
0004586     
Arg of perigee:   283
6838  deg
Mean anomaly:      76
3803  deg
Mean motion:   15
53172584  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3223
Checksum:              328


Coasting Arc #12 (Orbit 3238)
---------------------------------------

Vector Time (GMT): 2019/021/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929313
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3138291
90                 A    =         6781742
84  meter
 Y    =        3345670
84  meter          E    =           
0004821
 Z    =        4995703
82                 I    =           51
70917
 XDOT =      -6672
362362                 Wp   =           10
55805
 YDOT =      -3152
581058  meter/sec      RA   =           12
46219  deg
 ZDOT =      -2075
304990                 TA   =           99
64607
                                          MA   =           99
59160
                                          Ha   =            221
256  n
mi
                                          Hp   =            217
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10296233
27                 X    =        -3199736
65
 Y    =       10976610
37  feet           Y    =         3310232
28  meter
 Z    =       16390104
40                 Z    =         4980310
61
 XDOT =     -21890
952630                 XDOT =       -6626
532984
 YDOT =     -10343
113707  feet/sec       YDOT =       -3226
939631  meter/sec
 ZDOT =      -6808
743407                 ZDOT =       -2107
605001

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15120404
81                 X    =         4608699
39
 Y    =        -399854
90  feet           Y    =         -121875
77  meter
 Z    =       16320152
92                 Z    =         4974382
61
 XDOT =       8096
279405                 XDOT =        2467
745963
 YDOT =      21660
765015  feet/sec       YDOT =        6602
201177  meter/sec
 ZDOT =      -6954
092227                 ZDOT =       -2119
607311


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
08833036  
00016717  00000-0  10270-3 0  9113
2 25544  51
6385  12
8465 0004499 287
8130  72
2531 15
53132449 32395


Satellite: ISS
Catalog Number: 25544
Epoch time:      19021
08833036   =   yrday
fracday
Element set:     911
Inclination:       51
6385  deg
RA of node:        12
8465  deg
Eccentricity:     
0004499     
Arg of perigee:   287
8130  deg
Mean anomaly:      72
2531  deg
Mean motion:   15
53132449  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3239
Checksum:              302


Coasting Arc #13 (Orbit 3253)
---------------------------------------

Vector Time (GMT): 2019/022/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929313
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4329789
35                 A    =         6784233
62  meter
 Y    =       -2897581
73  meter          E    =           
0003969
 Z    =       -4349462
06                 I    =           51
68583
 XDOT =       5847
637931                 Wp   =          108
81747
 YDOT =       3532
684929  meter/sec      RA   =            7
48246  deg
 ZDOT =       3469
080229                 TA   =          196
41817
                                          MA   =          196
43103
                                          Ha   =            221
250  n
mi
                                          Hp   =            217
878

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14205345
62                 X    =         4382995
80
 Y    =       -9506501
74  feet           Y    =        -2848865
26  meter
 Z    =      -14269888
65                 Z    =        -4328301
11
 XDOT =      19185
163816                 XDOT =        5790
849463
 YDOT =      11590
173652  feet/sec       YDOT =        3597
759560  meter/sec
 ZDOT =      11381
496815                 ZDOT =        3497
347348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16889543
44                 X    =        -5147932
84
 Y    =       -3104351
25  feet           Y    =         -946206
26  meter
 Z    =      -14173971
48                 Z    =        -4320226
51
 XDOT =      -5907
914493                 XDOT =       -1800
732338
 YDOT =     -20383
519241  feet/sec       YDOT =       -6212
896665  meter/sec
 ZDOT =      11508
587942                 ZDOT =        3507
817605


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
05345737  
00016717  00000-0  10270-3 0  9128
2 25544  51
6392   8
0429 0004575 291
3786  68
6878 15
53164154 32540


Satellite: ISS
Catalog Number: 25544
Epoch time:      19022
05345737   =   yrday
fracday
Element set:     912
Inclination:       51
6392  deg
RA of node:         8
0429  deg
Eccentricity:     
0004575     
Arg of perigee:   291
3786  deg
Mean anomaly:      68
6878  deg
Mean motion:   15
53164154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3254
Checksum:              322


Coasting Arc #14 (Orbit 3269)
---------------------------------------

Vector Time (GMT): 2019/023/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929313
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5343588
91                 A    =         6787404
62  meter
 Y    =        2448469
75  meter          E    =           
0008489
 Z    =        3388709
45                 I    =           51
66335
 XDOT =      -4721
192029                 Wp   =           78
28142
 YDOT =      -3874
479897  meter/sec      RA   =            2
50591  deg
 ZDOT =      -4633
778837                 TA   =           62
16784
                                          MA   =           62
08184
                                          Ha   =            221
346  n
mi
                                          Hp   =            217
795

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17531459
68                 X    =        -5387031
24
 Y    =        8033037
24  feet           Y    =         2388471
02  meter
 Z    =       11117813
14                 Z    =         3362647
60
 XDOT =     -15489
475162                 XDOT =       -4655
007944
 YDOT =     -12711
548219  feet/sec       YDOT =       -3926
905372  meter/sec
 ZDOT =     -15202
686473                 ZDOT =       -4656
551321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18349760
74                 X    =         5593007
07
 Y    =        6146314
69  feet           Y    =         1873396
72  meter
 Z    =       10999846
87                 Z    =         3352753
33
 XDOT =       3015
686901                 XDOT =         919
181367
 YDOT =      18455
755043  feet/sec       YDOT =        5625
314137  meter/sec
 ZDOT =     -15304
928503                 ZDOT =       -4664
942208


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   19023
08292650  
00016717  00000-0  10270-3 0  9138
2 25544  51
6393   2
9178 0004607 294
2545  65
8126 15
53153792 32705


Satellite: ISS
Catalog Number: 25544
Epoch time:      19023
08292650   =   yrday
fracday
Element set:     913
Inclination:       51
6393  deg
RA of node:         2
9178  deg
Eccentricity:     
0004607     
Arg of perigee:   294
2545  deg
Mean anomaly:      65
8126  deg
Mean motion:   15
53153792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3270
Checksum:              307


Coasting Arc #15 (Orbit 3284)
---------------------------------------

Vector Time (GMT): 2019/024/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929313
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6092290
54                 A    =         6790114
58  meter
 Y    =       -2012551
48  meter          E    =           
0006914
 Z    =       -2209446
20                 I    =           51
64111
 XDOT =       3364
585628                 Wp   =             
74510
 YDOT =       4187
949456  meter/sec      RA   =          357
53445  deg
 ZDOT =       5469
659567                 TA   =          334
72132
                                          MA   =          334
75514
                                          Ha   =            221
509  n
mi
                                          Hp   =            217
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19987829
85                 X    =         6125074
65
 Y    =       -6602859
17  feet           Y    =        -1944239
93  meter
 Z    =       -7248839
25                 Z    =        -2179773
30
 XDOT =      11038
666758                 XDOT =        3290
936872
 YDOT =      13739
991655  feet/sec       YDOT =        4225
162802  meter/sec
 ZDOT =      17945
077319                 ZDOT =        5485
824157

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19298910
99                 X    =        -5882308
07
 Y    =       -8520011
27  feet           Y    =        -2596899
44  meter
 Z    =       -7114647
19                 Z    =        -2168544
46
 XDOT =        478
163055                 XDOT =         145
744099
 YDOT =     -16109
206673  feet/sec       YDOT =       -4910
086194  meter/sec
 ZDOT =      18017
451962                 ZDOT =        5491
719358


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   19024
04805097  
00016717  00000-0  10270-3 0  9141
2 25544  51
6411 358
1137 0004648 299
6688  60
4001 15
53172687 32852


Satellite: ISS
Catalog Number: 25544
Epoch time:      19024
04805097   =   yrday
fracday
Element set:     914
Inclination:       51
6411  deg
RA of node:       358
1137  deg
Eccentricity:     
0004648     
Arg of perigee:   299
6688  deg
Mean anomaly:      60
4001  deg
Mean motion:   15
53172687  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3285
Checksum:              317


Coasting Arc #16 (Orbit 3300)
---------------------------------------

Vector Time (GMT): 2019/025/01:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929313
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6554534
02                 A    =         6791804
66  meter
 Y    =        1540379
23  meter          E    =           
0008713
 Z    =         857620
03                 I    =           51
61305
 XDOT =      -1837
543333                 Wp   =          127
31967
 YDOT =      -4497
510383  meter/sec      RA   =          352
56637  deg
 ZDOT =      -5929
476941                 TA   =           43
40388
                                          MA   =           43
33531
                                          Ha   =            221
543  n
mi
                                          Hp   =            217
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21504376
71                 X    =        -6575437
58
 Y    =        5053737
64  feet           Y    =         1466965
00  meter
 Z    =        2813714
02                 Z    =          825730
49
 XDOT =      -6028
685477                 XDOT =       -1758
312879
 YDOT =     -14755
611494  feet/sec       YDOT =       -4517
616160  meter/sec
 ZDOT =     -19453
664505                 ZDOT =       -5938
210336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19545410
25                 X    =         5957441
04
 Y    =       10331779
15  feet           Y    =         3149126
29  meter
 Z    =        2669596
60                 Z    =          813693
04
 XDOT =      -4496
209292                 XDOT =       -1370
444592
 YDOT =      13574
849579  feet/sec       YDOT =        4137
614152  meter/sec
 ZDOT =     -19492
460777                 ZDOT =       -5941
302045


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   19025
07751575  
00016717  00000-0  10270-3 0  9157
2 25544  51
6404 352
9896 0004645 303
4948  56
5760 15
53180707 33017


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
07751575   =   yrday
fracday
Element set:     915
Inclination:       51
6404  deg
RA of node:       352
9896  deg
Eccentricity:     
0004645     
Arg of perigee:   303
4948  deg
Mean anomaly:      56
5760  deg
Mean motion:   15
53180707  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3301
Checksum:              318


Coasting Arc #17 (Orbit 3308)
---------------------------------------

Vector Time (GMT): 2019/025/12:55:30
000
Vector Time (MET): N/A
Weight (LBS)     : 914879
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4051376
84                 A    =         6783088
98  meter
 Y    =        2966101
75  meter          E    =           
0003965
 Z    =        4557313
78                 I    =           51
56764
 XDOT =      -6063
440241                 Wp   =           94
40431
 YDOT =       3538
643412  meter/sec      RA   =          350
13635  deg
 ZDOT =       3084
578061                 TA   =          324
68470
                                          MA   =          324
71096
                                          Ha   =            221
592  n
mi
                                          Hp   =            217
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13291918
76                 X    =         3995771
50
 Y    =        9731304
96  feet           Y    =         3011096
25  meter
 Z    =       14951816
87                 Z    =         4576858
34
 XDOT =     -19893
176645                 XDOT =       -6117
542567
 YDOT =      11609
722481  feet/sec       YDOT =        3470
535347  meter/sec
 ZDOT =      10120
006761                 ZDOT =        3054
993276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3161203
90                 X    =          963534
95
 Y    =       16085621
79  feet           Y    =         4902897
52  meter
 Z    =       15039607
37                 Z    =         4584072
33
 XDOT =     -21390
396550                 XDOT =       -6519
792869
 YDOT =      -5140
909520  feet/sec       YDOT =       -1566
949222  meter/sec
 ZDOT =       9986
024074                 ZDOT =        3043
740138


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   19025
59224657  
00016717  00000-0  10270-3 0  9161
2 25544  51
6398 350
4317 0004970 309
1357  50
9353 15
53210893 33092


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
59224657   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:       350
4317  deg
Eccentricity:     
0004970     
Arg of perigee:   309
1357  deg
Mean anomaly:      50
9353  deg
Mean motion:   15
53210893  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3309
Checksum:              317


Coasting Arc #18 (Orbit 3321)
---------------------------------------

Vector Time (GMT): 2019/026/08:59:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914879
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4583677
07                 A    =         6783928
52  meter
 Y    =        2429604
64  meter          E    =           
0005338
 Z    =        4366589
90                 I    =           51
54178
 XDOT =      -5462
135101                 Wp   =           87
67057
 YDOT =       4160
569885  meter/sec      RA   =          345
97299  deg
 ZDOT =       3415
314543                 TA   =          327
65098
                                          MA   =          327
68370
                                          Ha   =            221
787  n
mi
                                          Hp   =            217
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15038310
60                 X    =         4534957
78
 Y    =        7971143
84  feet           Y    =         2480590
18  meter
 Z    =       14326082
36                 Z    =         4388736
94
 XDOT =     -17920
390751                 XDOT =       -5524
843230
 YDOT =      13650
163664  feet/sec       YDOT =        4099
137915  meter/sec
 ZDOT =      11205
100207                 ZDOT =        3388
629620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10622663
52                 X    =        -3237787
84
 Y    =       13190345
49  feet           Y    =         4020417
30  meter
 Z    =       14425684
08                 Z    =         4396948
51
 XDOT =      -9087
974993                 XDOT =       -2770
014778
 YDOT =     -19453
201365  feet/sec       YDOT =       -5929
335776  meter/sec
 ZDOT =      11084
129505                 ZDOT =        3378
442673


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   19026
42868633  
00016717  00000-0  10270-3 0  9173
2 25544  51
6388 346
2678 0004848 313
5188  46
5561 15
53167193 33220


Satellite: ISS
Catalog Number: 25544
Epoch time:      19026
42868633   =   yrday
fracday
Element set:     917
Inclination:       51
6388  deg
RA of node:       346
2678  deg
Eccentricity:     
0004848     
Arg of perigee:   313
5188  deg
Mean anomaly:      46
5561  deg
Mean motion:   15
53167193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3322
Checksum:              337
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