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

 
Date: December 31st 2018

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


010/09:34:56 900 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

Coasting Arc #1 (Orbit 2926)
---------------------------------------

Vector Time (GMT): 2019/001/00:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4563402
23                 A    =         6780392
23  meter
 Y    =       -1047467
16  meter          E    =           
0009725
 Z    =       -4913167
50                 I    =           51
97909
 XDOT =       -903
024055                 Wp   =           79
32188
 YDOT =       7224
288876  meter/sec      RA   =          111
94116  deg
 ZDOT =      -2381
165399                 TA   =          167
44950
                                          MA   =          167
42527
                                          Ha   =            221
117  n
mi
                                          Hp   =            216
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14971792
11                 X    =         4598641
64
 Y    =       -3436572
06  feet           Y    =         -996238
61  meter
 Z    =      -16119315
96                 Z    =        -4890914
64
 XDOT =      -2962
677345                 XDOT =        -972
174558
 YDOT =      23701
735157  feet/sec       YDOT =        7213
804169  meter/sec
 ZDOT =      -7812
222438                 ZDOT =       -2385
719368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5873474
40                 X    =        -1790235
00
 Y    =      -14307266
62  feet           Y    =        -4360854
87  meter
 Z    =      -16018781
29                 Z    =        -4882524
54
 XDOT =      22813
599307                 XDOT =        6953
585069
 YDOT =       -603
127849  feet/sec       YDOT =        -183
833368  meter/sec
 ZDOT =      -7833
576735                 ZDOT =       -2387
674189


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   19001
02028722  
00016717  00000-0  10270-3 0  9001
2 25544  51
6397 112
8213 0002490 227
3026 132
7917 15
53733019 29275


Satellite: ISS
Catalog Number: 25544
Epoch time:      19001
02028722   =   yrday
fracday
Element set:     900
Inclination:       51
6397  deg
RA of node:       112
8213  deg
Eccentricity:     
0002490     
Arg of perigee:   227
3026  deg
Mean anomaly:     132
7917  deg
Mean motion:   15
53733019  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2927
Checksum:              280


Coasting Arc #2 (Orbit 2942)
---------------------------------------

Vector Time (GMT): 2019/002/00:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4183888
38                 A    =         6778575
09  meter
 Y    =        -508179
07  meter          E    =           
0002968
 Z    =        5308842
32                 I    =           51
98467
 XDOT =       1736
687875                 Wp   =          169
36252
 YDOT =      -7440
598164  meter/sec      RA   =          106
97197  deg
 ZDOT =        653
545626                 TA   =          274
41043
                                          MA   =          274
44434
                                          Ha   =            221
077  n
mi
                                          Hp   =            216
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13726667
92                 X    =        -4203682
28
 Y    =       -1667254
17  feet           Y    =         -555077
39  meter
 Z    =       17417461
68                 Z    =         5288470
39
 XDOT =       5697
794864                 XDOT =        1816
587090
 YDOT =     -24411
411300  feet/sec       YDOT =       -7420
730628  meter/sec
 ZDOT =       2144
178563                 ZDOT =         662
175192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         875313
91                 X    =          266795
68
 Y    =       13914997
78  feet           Y    =         4241291
32  meter
 Z    =       17325581
73                 Z    =         5280837
31
 XDOT =     -24022
731274                 XDOT =       -7322
128492
 YDOT =      -1220
027935  feet/sec       YDOT =        -371
864515  meter/sec
 ZDOT =       2183
970191                 ZDOT =         665
674114


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   19002
04938800  
00016717  00000-0  10270-3 0  9012
2 25544  51
6396 107
6955 0002674 233
4454 126
6453 15
53757634 29430


Satellite: ISS
Catalog Number: 25544
Epoch time:      19002
04938800   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:       107
6955  deg
Eccentricity:     
0002674     
Arg of perigee:   233
4454  deg
Mean anomaly:     126
6453  deg
Mean motion:   15
53757634  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2943
Checksum:              316


Coasting Arc #3 (Orbit 2957)
---------------------------------------

Vector Time (GMT): 2019/003/00:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3747661
34                 A    =         6778940
20  meter
 Y    =        2107281
44  meter          E    =           
0012412
 Z    =       -5251855
91                 I    =           51
99532
 XDOT =      -2434
376365                 Wp   =          106
70667
 YDOT =       7171
537237  meter/sec      RA   =          101
99983  deg
 ZDOT =       1139
155370                 TA   =          174
18141
                                          MA   =          174
16697
                                          Ha   =            220
938  n
mi
                                          Hp   =            216
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12295476
85                 X    =         3749329
18
 Y    =        6913653
01  feet           Y    =         2149200
29  meter
 Z    =      -17230498
38                 Z    =        -5233646
90
 XDOT =      -7986
799099                 XDOT =       -2519
922961
 YDOT =      23528
665475  feet/sec       YDOT =        7143
835903  meter/sec
 ZDOT =       3737
386385                 ZDOT =        1127
123083

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4311791
69                 X    =         1314234
11
 Y    =      -13535241
94  feet           Y    =        -4125541
74  meter
 Z    =      -17148559
74                 Z    =        -5226881
01
 XDOT =      23663
933112                 XDOT =        7212
766812
 YDOT =       2867
937657  feet/sec       YDOT =         874
147398  meter/sec
 ZDOT =       3682
246536                 ZDOT =        1122
348744


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   19003
01417073  
00016717  00000-0  10270-3 0  9025
2 25544  51
6407 102
8886 0002584 236
8328 123
2577 15
53727965 29580


Satellite: ISS
Catalog Number: 25544
Epoch time:      19003
01417073   =   yrday
fracday
Element set:     902
Inclination:       51
6407  deg
RA of node:       102
8886  deg
Eccentricity:     
0002584     
Arg of perigee:   236
8328  deg
Mean anomaly:     123
2577  deg
Mean motion:   15
53727965  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2958
Checksum:              319


Coasting Arc #4 (Orbit 2973)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3266259
99                 A    =         6781115
65  meter
 Y    =       -3610977
91  meter          E    =           
0005455
 Z    =        4716582
97                 I    =           52
00898
 XDOT =       3027
938768                 Wp   =           64
37511
 YDOT =      -6450
184147  meter/sec      RA   =           97
03287  deg
 ZDOT =      -2836
503635                 TA   =           53
63811
                                          MA   =           53
58778
                                          Ha   =            220
999  n
mi
                                          Hp   =            216
094

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10716076
10                 X    =        -3248548
73
 Y    =      -11847040
40  feet           Y    =        -3647405
04  meter
 Z    =       15474353
57                 Z    =         4700759
35
 XDOT =       9934
182310                 XDOT =        3113
619604
 YDOT =     -21162
021481  feet/sec       YDOT =       -6415
844222  meter/sec
 ZDOT =      -9306
114287                 ZDOT =       -2821
587757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9238705
28                 X    =        -2815957
37
 Y    =       13115835
92  feet           Y    =         3997706
79  meter
 Z    =       15403358
22                 Z    =         4694943
59
 XDOT =     -21862
141932                 XDOT =       -6663
580861
 YDOT =      -4531
586612  feet/sec       YDOT =       -1381
227599  meter/sec
 ZDOT =      -9238
022693                 ZDOT =       -2815
749317


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
04326726  
00016717  00000-0  10270-3 0  9034
2 25544  51
6411  97
7626 0002512 241
7969 118
2930 15
53736868 29743


Satellite: ISS
Catalog Number: 25544
Epoch time:      19004
04326726   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:        97
7626  deg
Eccentricity:     
0002512     
Arg of perigee:   241
7969  deg
Mean anomaly:     118
2930  deg
Mean motion:   15
53736868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2974
Checksum:              321


Coasting Arc #5 (Orbit 2988)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2774113
57                 A    =         6784442
05  meter
 Y    =        4908323
93  meter          E    =           
0004213
 Z    =       -3778796
33                 I    =           52
02398
 XDOT =      -3531
277717                 Wp   =          123
44749
 YDOT =       5286
827665  meter/sec      RA   =           92
07213  deg
 ZDOT =       4275
888429                 TA   =          191
61826
                                          MA   =          191
62799
                                          Ha   =            220
832  n
mi
                                          Hp   =            216
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9101422
48                 X    =         2737376
29
 Y    =       16103424
97  feet           Y    =         4939141
05  meter
 Z    =      -12397625
76                 Z    =        -3765409
45
 XDOT =     -11585
556814                 XDOT =       -3610
903793
 YDOT =      17345
235122  feet/sec       YDOT =        5246
892721  meter/sec
 ZDOT =      14028
505345                 ZDOT =        4258
542181

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13531599
43                 X    =         4124431
51
 Y    =      -12670126
24  feet           Y    =        -3861854
48  meter
 Z    =      -12337788
67                 Z    =        -3760557
99
 XDOT =      18659
097746                 XDOT =        5687
292993
 YDOT =       6347
859237  feet/sec       YDOT =        1934
827496  meter/sec
 ZDOT =      13949
563988                 ZDOT =        4251
827104


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
00804239  
00016717  00000-0  10270-3 0  9042
2 25544  51
6418  92
9558 0002477 245
2306 114
8588 15
53749508 29897


Satellite: ISS
Catalog Number: 25544
Epoch time:      19005
00804239   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:        92
9558  deg
Eccentricity:     
0002477     
Arg of perigee:   245
2306  deg
Mean anomaly:     114
8588  deg
Mean motion:   15
53749508  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2989
Checksum:              333


Coasting Arc #6 (Orbit 3004)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2238998
38                 A    =         6787925
86  meter
 Y    =       -5898967
37  meter          E    =           
0011809
 Z    =        2486212
00                 I    =           52
03509
 XDOT =       3991
006472                 Wp   =          112
60123
 YDOT =      -3776
842791  meter/sec      RA   =           87
12201  deg
 ZDOT =      -5351
282651                 TA   =           39
68831
                                          MA   =           39
60195
                                          Ha   =            220
878  n
mi
                                          Hp   =            216
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7345795
21                 X    =        -2184944
57
 Y    =      -19353567
49  feet           Y    =        -5923703
47  meter
 Z    =        8156863
51                 Z    =         2475466
49
 XDOT =      13093
853256                 XDOT =        4058
936836
 YDOT =     -12391
216507  feet/sec       YDOT =       -3731
832125  meter/sec
 ZDOT =     -17556
701610                 ZDOT =       -5331
731510

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16903700
35                 X    =        -5152247
87
 Y    =       11981798
20  feet           Y    =         3652052
09  meter
 Z    =        8109077
03                 Z    =         2471646
68
 XDOT =     -14415
591321                 XDOT =       -4393
872235
 YDOT =      -8480
013622  feet/sec       YDOT =       -2584
708152  meter/sec
 ZDOT =     -17467
975931                 ZDOT =       -5324
239064


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
03713489  
00016717  00000-0  10270-3 0  9053
2 25544  51
6414  87
8301 0002544 247
5307 112
5576 15
53721184 30055


Satellite: ISS
Catalog Number: 25544
Epoch time:      19006
03713489   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:        87
8301  deg
Eccentricity:     
0002544     
Arg of perigee:   247
5307  deg
Mean anomaly:     112
5576  deg
Mean motion:   15
53721184  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3005
Checksum:              292


Coasting Arc #7 (Orbit 3019)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1675001
29                 A    =         6789992
59  meter
 Y    =        6500418
07  meter          E    =           
0007830
 Z    =        -992933
63                 I    =           52
04074
 XDOT =      -4397
934078                 Wp   =           27
15353
 YDOT =       2036
767162  meter/sec      RA   =           82
17708  deg
 ZDOT =       5940
249000                 TA   =          322
15114
                                          MA   =          322
20618
                                          Ha   =            220
685  n
mi
                                          Hp   =            216
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5495411
07                 X    =         1607010
36
 Y    =       21326830
93  feet           Y    =         6518769
04  meter
 Z    =       -3257656
26                 Z    =         -984961
65
 XDOT =     -14428
917580                 XDOT =       -4449
236929
 YDOT =       6682
306962  feet/sec       YDOT =        1987
298911  meter/sec
 ZDOT =      19489
005905                 ZDOT =        5918
761408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19097691
79                 X    =         5820976
46
 Y    =      -10979044
65  feet           Y    =        -3346412
81  meter
 Z    =       -3222472
91                 Z    =         -982209
74
 XDOT =       9507
189027                 XDOT =        2897
791215
 YDOT =      10870
243216  feet/sec       YDOT =        3313
250132  meter/sec
 ZDOT =      19391
742510                 ZDOT =        5910
603117


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
00190403  
00016717  00000-0  10270-3 0  9067
2 25544  51
6425  83
0232 0002632 255
1346 104
9515 15
53758597 30207


Satellite: ISS
Catalog Number: 25544
Epoch time:      19007
00190403   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:        83
0232  deg
Eccentricity:     
0002632     
Arg of perigee:   255
1346  deg
Mean anomaly:     104
9515  deg
Mean motion:   15
53758597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3020
Checksum:              278


Coasting Arc #8 (Orbit 3035)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1021194
20                 A    =         6790365
07  meter
 Y    =       -6679298
74  meter          E    =           
0009822
 Z    =        -614752
50                 I    =           52
03574
 XDOT =       4764
087086                 Wp   =          152
80412
 YDOT =       -179
878447  meter/sec      RA   =           77
23648  deg
 ZDOT =      -6005
661720                 TA   =           33
79524
                                          MA   =           33
73267
                                          Ha   =            220
750  n
mi
                                          Hp   =            216
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3350374
68                 X    =         -943442
44
 Y    =      -21913709
79  feet           Y    =        -6690283
65  meter
 Z    =       -2016904
52                 Z    =         -619524
77
 XDOT =      15630
206974                 XDOT =        4794
916140
 YDOT =       -590
152385  feet/sec       YDOT =        -126
430175  meter/sec
 ZDOT =     -19703
614566                 ZDOT =       -5982
445096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20084130
75                 X    =        -6121643
05
 Y    =        9379734
69  feet           Y    =         2858943
13  meter
 Z    =       -2037611
38                 Z    =         -621063
95
 XDOT =      -4327
300085                 XDOT =       -1318
961066
 YDOT =     -13490
685643  feet/sec       YDOT =       -4111
960984  meter/sec
 ZDOT =     -19598
771072                 ZDOT =       -5973
705423


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
03098972  
00016717  00000-0  10270-3 0  9070
2 25544  51
6423  77
8968 0002600 256
6348 103
4515 15
53715788 30361


Satellite: ISS
Catalog Number: 25544
Epoch time:      19008
03098972   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:        77
8968  deg
Eccentricity:     
0002600     
Arg of perigee:   256
6348  deg
Mean anomaly:     103
4515  deg
Mean motion:   15
53715788  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3036
Checksum:              325


Coasting Arc #9 (Orbit 3051)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         295942
12                 A    =         6788497
98  meter
 Y    =        6428437
59  meter          E    =           
0011435
 Z    =        2143403
01                 I    =           52
02062
 XDOT =      -5054
127690                 Wp   =           66
60907
 YDOT =      -1619
505482  meter/sec      RA   =           72
29223  deg
 ZDOT =       5536
105262                 TA   =          317
02559
                                          MA   =          317
11486
                                          Ha   =            220
672  n
mi
                                          Hp   =            216
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         970938
72                 X    =          213624
26
 Y    =       21090674
49  feet           Y    =         6431286
58  meter
 Z    =        7032162
09                 Z    =         2144641
12
 XDOT =     -16581
783760                 XDOT =       -5062
533138
 YDOT =      -5313
338196  feet/sec       YDOT =       -1676
071677  meter/sec
 ZDOT =      18163
075006                 ZDOT =        5511
534101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19854617
41                 X    =         6051687
39
 Y    =       -7175393
72  feet           Y    =        -2187060
01  meter
 Z    =        7036936
04                 Z    =         2144858
10
 XDOT =       -609
228886                 XDOT =        -185
692964
 YDOT =      16079
014560  feet/sec       YDOT =        4900
883638  meter/sec
 ZDOT =      18052
341404                 ZDOT =        5502
353660


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
06007209  
00016717  00000-0  10270-3 0  9088
2 25544  51
6415  72
7695 0002584 266
3153  93
7704 15
53744782 30521


Satellite: ISS
Catalog Number: 25544
Epoch time:      19009
06007209   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:        72
7695  deg
Eccentricity:     
0002584     
Arg of perigee:   266
3153  deg
Mean anomaly:      93
7704  deg
Mean motion:   15
53744782  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3052
Checksum:              313


Coasting Arc #10 (Orbit 3066)
---------------------------------------

Vector Time (GMT): 2019/010/00:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         551541
80                 A    =         6785251
53  meter
 Y    =       -5785531
02  meter          E    =           
0002290
 Z    =       -3504084
58                 I    =           51
99901
 XDOT =       5223
511986                 Wp   =           83
47899
 YDOT =       3259
764111  meter/sec      RA   =           67
34138  deg
 ZDOT =      -4562
257401                 TA   =          137
45985
                                          MA   =          137
44211
                                          Ha   =            220
586  n
mi
                                          Hp   =            216
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1809520
35                 X    =          633216
84
 Y    =      -18981400
98  feet           Y    =        -5778906
41  meter
 Z    =      -11496340
50                 Z    =        -3501207
42
 XDOT =      17137
506516                 XDOT =        5208
832690
 YDOT =      10694
764144  feet/sec       YDOT =        3318
095254  meter/sec
 ZDOT =     -14968
036093                 ZDOT =       -4536
919441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18611073
91                 X    =        -5672655
33
 Y    =        4184664
91  feet           Y    =         1275485
86  meter
 Z    =      -11482608
56                 Z    =        -3499899
09
 XDOT =       5029
542251                 XDOT =        1533
004478
 YDOT =     -18369
781779  feet/sec       YDOT =       -5599
109486  meter/sec
 ZDOT =     -14854
051892                 ZDOT =       -4527
515017


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
02483408  
00016717  00000-0  10270-3 0  9096
2 25544  51
6418  67
9632 0002785 268
5052  91
5781 15
53746031 30672


Satellite: ISS
Catalog Number: 25544
Epoch time:      19010
02483408   =   yrday
fracday
Element set:     909
Inclination:       51
6418  deg
RA of node:        67
9632  deg
Eccentricity:     
0002785     
Arg of perigee:   268
5052  deg
Mean anomaly:      91
5781  deg
Mean motion:   15
53746031  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3067
Checksum:              312


Coasting Arc #11 (Orbit 3072)
---------------------------------------

Vector Time (GMT): 2019/010/09:34:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4651433
25                 A    =         6780624
93  meter
 Y    =        1098472
55  meter          E    =           
0009048
 Z    =       -4818468
66                 I    =           51
97841
 XDOT =       1025
760755                 Wp   =          116
03690
 YDOT =       7126
674796  meter/sec      RA   =           65
31315  deg
 ZDOT =       2614
818164                 TA   =          179
64106
                                          MA   =          179
64041
                                          Ha   =            220
594  n
mi
                                          Hp   =            216
297

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15260607
78                 X    =         4662209
16
 Y    =        3603912
57  feet           Y    =         1150548
63  meter
 Z    =      -15808624
20                 Z    =        -4795847
89
 XDOT =       3365
356809                 XDOT =         933
290924
 YDOT =      23381
478989  feet/sec       YDOT =        7137
628396  meter/sec
 ZDOT =       8578
799752                 ZDOT =        2619
576632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8061937
24                 X    =        -2457278
47
 Y    =       13568117
32  feet           Y    =         4135562
16  meter
 Z    =      -15706632
20                 Z    =        -4787381
49
 XDOT =     -22303
721046                 XDOT =       -6798
174175
 YDOT =      -3297
503976  feet/sec       YDOT =       -1005
079212  meter/sec
 ZDOT =       8599
367560                 ZDOT =        2621
087232


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
41073794  
00016717  00000-0  10270-3 0  9104
2 25544  51
6416  66
0370 0002643 260
8366  99
2487 15
53786527 30734


Satellite: ISS
Catalog Number: 25544
Epoch time:      19010
41073794   =   yrday
fracday
Element set:     910
Inclination:       51
6416  deg
RA of node:        66
0370  deg
Eccentricity:     
0002643     
Arg of perigee:   260
8366  deg
Mean anomaly:      99
2487  deg
Mean motion:   15
53786527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3073
Checksum:              312


Coasting Arc #12 (Orbit 3088)
---------------------------------------

Vector Time (GMT): 2019/011/09:34:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4942481
48                 A    =         6783992
53  meter
 Y    =       -2504255
84  meter          E    =           
0008687
 Z    =        3908428
30                 I    =           51
97468
 XDOT =         18
140376                 Wp   =           79
22607
 YDOT =      -6471
987128  meter/sec      RA   =           60
34885  deg
 ZDOT =      -4114
555994                 TA   =           53
74129
                                          MA   =           53
66105
                                          Ha   =            220
724  n
mi
                                          Hp   =            216
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16215490
41                 X    =        -4933095
53
 Y    =       -8216062
47  feet           Y    =        -2559473
78  meter
 Z    =       12822927
48                 Z    =         3884442
64
 XDOT =         59
515669                 XDOT =         110
496526
 YDOT =     -21233
553569  feet/sec       YDOT =       -6471
267712  meter/sec
 ZDOT =     -13499
199454                 ZDOT =       -4114
243818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12515054
14                 X    =         3814588
50
 Y    =      -13288209
93  feet           Y    =        -4050246
39  meter
 Z    =       12714958
81                 Z    =         3875519
45
 XDOT =      19344
619908                 XDOT =        5896
240148
 YDOT =       5274
896897  feet/sec       YDOT =        1607
788574  meter/sec
 ZDOT =     -13496
949494                 ZDOT =       -4113
870206


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
43981423  
00016717  00000-0  10270-3 0  9115
2 25544  51
6416  60
9099 0002591 267
9038  92
1818 15
53773436 30893


Satellite: ISS
Catalog Number: 25544
Epoch time:      19011
43981423   =   yrday
fracday
Element set:     911
Inclination:       51
6416  deg
RA of node:        60
9099  deg
Eccentricity:     
0002591     
Arg of perigee:   267
9038  deg
Mean anomaly:      92
1818  deg
Mean motion:   15
53773436  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3089
Checksum:              322


Coasting Arc #13 (Orbit 3103)
---------------------------------------

Vector Time (GMT): 2019/012/09:34:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5056833
59                 A    =         6787495
71  meter
 Y    =        3657024
72  meter          E    =           
0003326
 Z    =       -2665738
08                 I    =           51
96795
 XDOT =      -1199
413253                 Wp   =           22
86403
 YDOT =       5469
808436  meter/sec      RA   =           55
39279  deg
 ZDOT =       5233
734531                 TA   =          307
22090
                                          MA   =          307
25124
                                          Ha   =            220
633  n
mi
                                          Hp   =            216
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16590661
37                 X    =         5028512
39
 Y    =       11998112
60  feet           Y    =         3713415
48  meter
 Z    =       -8745859
84                 Z    =        -2641242
87
 XDOT =      -3935
082852                 XDOT =       -1285
911297
 YDOT =      17945
565736  feet/sec       YDOT =        5455
911965  meter/sec
 ZDOT =      17171
045049                 ZDOT =        5227
698384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16021791
30                 X    =        -4883441
99
 Y    =       12822669
99  feet           Y    =         3908349
81  meter
 Z    =       -8635748
56                 Z    =        -2632176
16
 XDOT =     -15269
038801                 XDOT =       -4654
003026
 YDOT =      -7544
631922  feet/sec       YDOT =       -2299
603810  meter/sec
 ZDOT =      17143
075525                 ZDOT =        5225
209420


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
40457180  
00016717  00000-0  10270-3 0  9122
2 25544  51
6408  56
1038 0002729 271
5796  88
5044 15
53748294 31041


Satellite: ISS
Catalog Number: 25544
Epoch time:      19012
40457180   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:        56
1038  deg
Eccentricity:     
0002729     
Arg of perigee:   271
5796  deg
Mean anomaly:      88
5044  deg
Mean motion:   15
53748294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3104
Checksum:              307


Coasting Arc #14 (Orbit 3119)
---------------------------------------

Vector Time (GMT): 2019/013/09:38:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4147071
26                 A    =         6790335
14  meter
 Y    =       -5362890
95  meter          E    =           
0009679
 Z    =        -278620
60                 I    =           51
95796
 XDOT =       3890
008123                 Wp   =          147
00385
 YDOT =      -2700
301850  meter/sec      RA   =           50
44271  deg
 ZDOT =      -6030
707672                 TA   =           35
98497
                                          MA   =           35
91984
                                          Ha   =            220
608  n
mi
                                          Hp   =            216
199

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13605876
84                 X    =        -4085440
32
 Y    =      -17594786
58  feet           Y    =        -5408921
78  meter
 Z    =        -914109
59                 Z    =         -298615
78
 XDOT =      12762
493842                 XDOT =        3949
208088
 YDOT =      -8859
258037  feet/sec       YDOT =       -2656
469898  meter/sec
 ZDOT =     -19785
786324                 ZDOT =       -6011
667943

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20293444
50                 X    =         6185441
89
 Y    =       -9093995
52  feet           Y    =        -2771849
83  meter
 Z    =       -1003668
97                 Z    =         -305918
30
 XDOT =       4926
558163                 XDOT =        1501
614928
 YDOT =      13132
882053  feet/sec       YDOT =        4002
902450  meter/sec
 ZDOT =     -19699
471180                 ZDOT =       -6004
398816


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
43364459  
00016717  00000-0  10270-3 0  9133
2 25544  51
6408  50
9768 0002608 275
5669  84
5186 15
53768640 31200


Satellite: ISS
Catalog Number: 25544
Epoch time:      19013
43364459   =   yrday
fracday
Element set:     913
Inclination:       51
6408  deg
RA of node:        50
9768  deg
Eccentricity:     
0002608     
Arg of perigee:   275
5669  deg
Mean anomaly:      84
5186  deg
Mean motion:   15
53768640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3120
Checksum:              327


Coasting Arc #15 (Orbit 3135)
---------------------------------------

Vector Time (GMT): 2019/014/09:38:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3439116
92                 A    =         6788940
84  meter
 Y    =        5550207
40  meter          E    =           
0012014
 Z    =        1835985
64                 I    =           51
93168
 XDOT =      -5018
521925                 Wp   =           58
72298
 YDOT =       1227
547998  meter/sec      RA   =           45
49354  deg
 ZDOT =       5668
438922                 TA   =          321
38764
                                          MA   =          321
47349
                                          Ha   =            220
684  n
mi
                                          Hp   =            216
139

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11283192
00                 X    =         3367879
21
 Y    =       18209341
87  feet           Y    =         5588267
63  meter
 Z    =        6023574
93                 Z    =         1852518
62
 XDOT =     -16464
966946                 XDOT =       -5059
409663
 YDOT =       4027
388444  feet/sec       YDOT =        1171
198589  meter/sec
 ZDOT =      18597
240558                 ZDOT =        5643
961724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20220983
51                 X    =        -6163355
77
 Y    =        7007619
47  feet           Y    =         2135922
42  meter
 Z    =        6097466
94                 Z    =         1858507
92
 XDOT =        191
269058                 XDOT =          58
298809
 YDOT =     -15593
462955  feet/sec       YDOT =       -4752
887509  meter/sec
 ZDOT =      18486
575783                 ZDOT =        5634
708299


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
46271425  
00016717  00000-0  10270-3 0  9148
2 25544  51
6413  45
8494 0002549 283
6705  76
4163 15
53759680 31366


Satellite: ISS
Catalog Number: 25544
Epoch time:      19014
46271425   =   yrday
fracday
Element set:     914
Inclination:       51
6413  deg
RA of node:        45
8494  deg
Eccentricity:     
0002549     
Arg of perigee:   283
6705  deg
Mean anomaly:      76
4163  deg
Mean motion:   15
53759680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3136
Checksum:              318


Coasting Arc #16 (Orbit 3150)
---------------------------------------

Vector Time (GMT): 2019/015/09:38:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2436075
76                 A    =         6785849
94  meter
 Y    =       -5437186
98  meter          E    =           
0002215
 Z    =       -3250192
14                 I    =           51
89662
 XDOT =       5982
552842                 Wp   =           86
20101
 YDOT =        178
555445  meter/sec      RA   =           40
53809  deg
 ZDOT =      -4785
393379                 TA   =          131
28638
                                          MA   =          131
26731
                                          Ha   =            220
705  n
mi
                                          Hp   =            216
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7992374
55                 X    =        -2359307
01
 Y    =      -17838539
97  feet           Y    =        -5463999
49  meter
 Z    =      -10663360
03                 Z    =        -3261839
41
 XDOT =      19627
798038                 XDOT =        6003
356215
 YDOT =        585
811826  feet/sec       YDOT =         245
573052  meter/sec
 ZDOT =     -15700
109510                 ZDOT =       -4756
281990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19067086
35                 X    =         5811647
92
 Y    =       -4174867
27  feet           Y    =        -1272499
54  meter
 Z    =      -10715199
84                 Z    =        -3265992
91
 XDOT =      -4842
100631                 XDOT =       -1475
872272
 YDOT =      17821
885049  feet/sec       YDOT =        5432
110563  meter/sec
 ZDOT =     -15568
718916                 ZDOT =       -4745
345526


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
42746582  
00016717  00000-0  10270-3 0  9157
2 25544  51
6404  41
0434 0002481 286
4021  73
6858 15
53770641 31512


Satellite: ISS
Catalog Number: 25544
Epoch time:      19015
42746582   =   yrday
fracday
Element set:     915
Inclination:       51
6404  deg
RA of node:        41
0434  deg
Eccentricity:     
0002481     
Arg of perigee:   286
4021  deg
Mean anomaly:      73
6858  deg
Mean motion:   15
53770641  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3151
Checksum:              293
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