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

 
Date: June 19th 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) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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


172/07:16:36 447 1 2 1 2 1 3
N/A 0 1 -0 1 220 4
000/00:03:12 895 0 4 -0 0 216 0

179/14:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 216 0

180/09:42:42 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 9

183/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 216 0

Coasting Arc #1 (Orbit 3871)
---------------------------------------

Vector Time (GMT): 2018/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         531203
90                 A    =         6777705
68  meter
 Y    =        4306061
54  meter          E    =           
0005094
 Z    =        5206143
49                 I    =           51
70140
 XDOT =      -7549
904587                 Wp   =          157
11346
 YDOT =       -559
408954  meter/sec      RA   =           11
59749  deg
 ZDOT =       1228
050753                 TA   =          281
08525
                                          MA   =          281
14252
                                          Ha   =            220
682  n
mi
                                          Hp   =            215
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1742794
94                 X    =          457724
42
 Y    =       14127498
50  feet           Y    =         4311590
36  meter
 Z    =       17080523
27                 Z    =         5208545
92
 XDOT =     -24770
028172                 XDOT =       -7549
053162
 YDOT =      -1835
331215  feet/sec       YDOT =        -643
832577  meter/sec
 ZDOT =       4029
037904                 ZDOT =        1191
378305

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14210240
50                 X    =         4331281
30
 Y    =        -591343
55  feet           Y    =         -180241
52  meter
 Z    =       17090558
83                 Z    =         5209202
33
 XDOT =      -3687
708881                 XDOT =       -1124
013667
 YDOT =      23559
190586  feet/sec       YDOT =        7180
841291  meter/sec
 ZDOT =       3865
008934                 ZDOT =        1178
054723


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   18169
55025789  
00016717  00000-0  10270-3 0  9003
2 25544  51
6400  11
9206 0002836 208
9467 151
1529 15
54163973 38720


Satellite: ISS
Catalog Number: 25544
Epoch time:      18169
55025789   =   yrday
fracday
Element set:     900
Inclination:       51
6400  deg
RA of node:        11
9206  deg
Eccentricity:     
0002836     
Arg of perigee:   208
9467  deg
Mean anomaly:     151
1529  deg
Mean motion:   15
54163973  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3872
Checksum:              317


Coasting Arc #2 (Orbit 3886)
---------------------------------------

Vector Time (GMT): 2018/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1309894
07                 A    =         6777352
03  meter
 Y    =       -4053548
01  meter          E    =           
0013575
 Z    =       -5282847
06                 I    =           51
66606
 XDOT =       7483
279416                 Wp   =          106
64358
 YDOT =       1453
283492  meter/sec      RA   =            6
59902  deg
 ZDOT =        738
162532                 TA   =          170
42724
                                          MA   =          170
40134
                                          Ha   =            220
602  n
mi
                                          Hp   =            215
089

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4297552
73                 X    =         1380785
68
 Y    =      -13299042
02  feet           Y    =        -4038502
96  meter
 Z    =      -17332175
39                 Z    =        -5276312
32
 XDOT =      24551
441655                 XDOT =        7462
886656
 YDOT =       4767
990460  feet/sec       YDOT =        1536
852584  meter/sec
 ZDOT =       2421
793085                 ZDOT =         774
464039

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13032417
88                 X    =        -3972280
97
 Y    =       -5150309
45  feet           Y    =        -1569814
32  meter
 Z    =      -17302259
36                 Z    =        -5273728
65
 XDOT =       5759
343759                 XDOT =        1755
447978
 YDOT =     -23278
938921  feet/sec       YDOT =       -7095
420583  meter/sec
 ZDOT =       2584
003419                 ZDOT =         787
604242


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   18170
51474717  
00016717  00000-0  10270-3 0  9011
2 25544  51
6381   7
1111 0002873 211
4456 148
6526 15
54201159 38871


Satellite: ISS
Catalog Number: 25544
Epoch time:      18170
51474717   =   yrday
fracday
Element set:     901
Inclination:       51
6381  deg
RA of node:         7
1111  deg
Eccentricity:     
0002873     
Arg of perigee:   211
4456  deg
Mean anomaly:     148
6526  deg
Mean motion:   15
54201159  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3887
Checksum:              296


Coasting Arc #3 (Orbit 3902)
---------------------------------------

Vector Time (GMT): 2018/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3063417
83                 A    =         6779521
75  meter
 Y    =        3699473
45  meter          E    =           
0004997
 Z    =        4780824
33                 I    =           51
64078
 XDOT =      -6841
315158                 Wp   =           75
51740
 YDOT =      -2269
161388  meter/sec      RA   =            1
60254  deg
 ZDOT =      -2624
293256                 TA   =           40
36926
                                          MA   =           40
33218
                                          Ha   =            220
563  n
mi
                                          Hp   =            215
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10050583
44                 X    =        -3127781
29
 Y    =       12137380
08  feet           Y    =         3664855
88  meter
 Z    =       15685119
20                 Z    =         4765787
39
 XDOT =     -22445
259704                 XDOT =       -6802
684941
 YDOT =      -7444
755209  feet/sec       YDOT =       -2345
449456  meter/sec
 ZDOT =      -8609
886011                 ZDOT =       -2657
432225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11735212
50                 X    =         3576892
77
 Y    =       10617928
99  feet           Y    =         3236344
75  meter
 Z    =       15617219
93                 Z    =         4760128
64
 XDOT =      -7534
827313                 XDOT =       -2296
615365
 YDOT =      21226
013115  feet/sec       YDOT =        6469
688797  meter/sec
 ZDOT =      -8757
797949                 ZDOT =       -2669
376815


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   18171
54353484  
00016717  00000-0  10270-3 0  9023
2 25544  51
6387   1
9825 0003002 218
0774 142
0167 15
54192336 39036


Satellite: ISS
Catalog Number: 25544
Epoch time:      18171
54353484   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:         1
9825  deg
Eccentricity:     
0003002     
Arg of perigee:   218
0774  deg
Mean anomaly:     142
0167  deg
Mean motion:   15
54192336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3903
Checksum:              293


Coasting Arc #4 (Orbit 3914)
---------------------------------------

Vector Time (GMT): 2018/172/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3141304
33                 A    =         6780707
33  meter
 Y    =       -3817595
95  meter          E    =           
0008689
 Z    =       -4649240
50                 I    =           51
61977
 XDOT =       6786
172821                 Wp   =          126
42842
 YDOT =       2028
310894  meter/sec      RA   =          357
59353  deg
 ZDOT =       2918
408439                 TA   =          172
65505
                                          MA   =          172
64231
                                          Ha   =            220
400  n
mi
                                          Hp   =            215
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10306116
57                 X    =         3206343
79
 Y    =      -12524921
09  feet           Y    =        -3782103
64  meter
 Z    =      -15253413
72                 Z    =        -4633823
54
 XDOT =      22264
346524                 XDOT =        6748
811267
 YDOT =       6654
563299  feet/sec       YDOT =        2103
989390  meter/sec
 ZDOT =       9574
830837                 ZDOT =        2951
282702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5994768
89                 X    =         1827205
56
 Y    =      -15141707
62  feet           Y    =        -4615192
48  meter
 Z    =      -15183799
05                 Z    =        -4628021
95
 XDOT =      22065
146264                 XDOT =        6725
456581
 YDOT =      -1016
887989  feet/sec       YDOT =        -309
947459  meter/sec
 ZDOT =       9721
589307                 ZDOT =        2963
140421


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   18172
31512506  
00016717  00000-0  10270-3 0  9032
2 25544  51
6424 358
1382 0003248 238
2382 121
8454 15
53975871 39153


Satellite: ISS
Catalog Number: 25544
Epoch time:      18172
31512506   =   yrday
fracday
Element set:     903
Inclination:       51
6424  deg
RA of node:       358
1382  deg
Eccentricity:     
0003248     
Arg of perigee:   238
2382  deg
Mean anomaly:     121
8454  deg
Mean motion:   15
53975871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3915
Checksum:              309


Coasting Arc #5 (Orbit 3930)
---------------------------------------

Vector Time (GMT): 2018/173/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4561587
87                 A    =         6784323
55  meter
 Y    =        3479375
21  meter          E    =           
0009355
 Z    =        3612408
37                 I    =           51
59859
 XDOT =      -5624
733563                 Wp   =           94
57170
 YDOT =      -2791
029234  meter/sec      RA   =          352
60485  deg
 ZDOT =      -4405
309358                 TA   =           42
59162
                                          MA   =           42
51911
                                          Ha   =            220
456  n
mi
                                          Hp   =            215
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14965839
47                 X    =        -4617703
37
 Y    =       11415272
99  feet           Y    =         3428050
27  meter
 Z    =       11851733
49                 Z    =         3590113
77
 XDOT =     -18453
850272                 XDOT =       -5571
706769
 YDOT =      -9156
920058  feet/sec       YDOT =       -2853
631957  meter/sec
 ZDOT =     -14453
114692                 ZDOT =       -4432
503888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10478364
48                 X    =        -3193805
49
 Y    =       15711672
99  feet           Y    =         4788917
93  meter
 Z    =       11751408
65                 Z    =         3581829
36
 XDOT =     -19198
374469                 XDOT =       -5851
664538
 YDOT =      -1880
421642  feet/sec       YDOT =        -573
152516  meter/sec
 ZDOT =     -14574
324252                 ZDOT =       -4442
254032


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   18173
34406036  
00016717  00000-0  10270-3 0  9047
2 25544  51
6420 353
0107 0003073 241
5464 118
5380 15
53978367 39314


Satellite: ISS
Catalog Number: 25544
Epoch time:      18173
34406036   =   yrday
fracday
Element set:     904
Inclination:       51
6420  deg
RA of node:       353
0107  deg
Eccentricity:     
0003073     
Arg of perigee:   241
5464  deg
Mean anomaly:     118
5380  deg
Mean motion:   15
53978367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3931
Checksum:              295


Coasting Arc #6 (Orbit 3945)
---------------------------------------

Vector Time (GMT): 2018/174/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5632011
88                 A    =         6787668
78  meter
 Y    =       -3053302
15  meter          E    =           
0003453
 Z    =       -2237809
31                 I    =           51
57705
 XDOT =       4076
020048                 Wp   =           20
24365
 YDOT =       3529
831827  meter/sec      RA   =          347
62273  deg
 ZDOT =       5447
861926                 TA   =          314
86364
                                          MA   =          314
89168
                                          Ha   =            220
254  n
mi
                                          Hp   =            215
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18477729
27                 X    =         5676606
30
 Y    =      -10017395
49  feet           Y    =        -2990071
51  meter
 Z    =       -7341894
05                 Z    =        -2210342
88
 XDOT =      13372
769185                 XDOT =        4009
782636
 YDOT =      11580
813082  feet/sec       YDOT =        3575
041725  meter/sec
 ZDOT =      17873
562749                 ZDOT =        5467
501404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13956921
74                 X    =         4254069
75
 Y    =      -15772620
99  feet           Y    =        -4807494
88  meter
 Z    =       -7218508
32                 Z    =        -2200201
34
 XDOT =      15276
175468                 XDOT =        4656
178283
 YDOT =       5306
339265  feet/sec       YDOT =        1617
372208  meter/sec
 ZDOT =      17960
842019                 ZDOT =        5474
464648


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   18174
30868446  
00016717  00000-0  10270-3 0  9052
2 25544  51
6417 348
2029 0003209 246
4933 113
5882 15
53992620 39461


Satellite: ISS
Catalog Number: 25544
Epoch time:      18174
30868446   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:       348
2029  deg
Eccentricity:     
0003209     
Arg of perigee:   246
4933  deg
Mean anomaly:     113
5882  deg
Mean motion:   15
53992620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3946
Checksum:              327


Coasting Arc #7 (Orbit 3961)
---------------------------------------

Vector Time (GMT): 2018/175/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6281994
02                 A    =         6789712
73  meter
 Y    =        2481040
96  meter          E    =           
0011827
 Z    =         622732
71                 I    =           51
55171
 XDOT =      -2275
175711                 Wp   =          142
20174
 YDOT =      -4250
790703  meter/sec      RA   =          342
64670  deg
 ZDOT =      -5964
898753                 TA   =           31
06606
                                          MA   =           30
99618
                                          Ha   =            220
263  n
mi
                                          Hp   =            216
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20610216
59                 X    =        -6312295
73
 Y    =        8139898
17  feet           Y    =         2410621
87  meter
 Z    =        2043086
31                 Z    =          592143
56
 XDOT =      -7464
487240                 XDOT =       -2198
498671
 YDOT =     -13946
163723  feet/sec       YDOT =       -4275
803785  meter/sec
 ZDOT =     -19569
877800                 ZDOT =       -5975
765126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16315927
30                 X    =        -4973094
64
 Y    =       15012377
95  feet           Y    =         4575772
80  meter
 Z    =        1905832
19                 Z    =          580897
65
 XDOT =     -10765
353991                 XDOT =       -3281
279896
 YDOT =      -9186
894219  feet/sec       YDOT =       -2800
165358  meter/sec
 ZDOT =     -19617
786011                 ZDOT =       -5979
501176


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   18175
33761653  
00016717  00000-0  10270-3 0  9069
2 25544  51
6419 343
0753 0003253 248
0661 112
0146 15
53948045 39622


Satellite: ISS
Catalog Number: 25544
Epoch time:      18175
33761653   =   yrday
fracday
Element set:     906
Inclination:       51
6419  deg
RA of node:       343
0753  deg
Eccentricity:     
0003253     
Arg of perigee:   248
0661  deg
Mean anomaly:     112
0146  deg
Mean motion:   15
53948045  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3962
Checksum:              305


Coasting Arc #8 (Orbit 3977)
---------------------------------------

Vector Time (GMT): 2018/176/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6466965
54                 A    =         6789206
86  meter
 Y    =       -1769118
55  meter          E    =           
0010574
 Z    =        1032521
98                 I    =           51
51934
 XDOT =        394
393476                 Wp   =           50
17608
 YDOT =       4897
556431  meter/sec      RA   =          337
66890  deg
 ZDOT =       5887
783781                 TA   =          321
03570
                                          MA   =          321
11185
                                          Ha   =            220
055  n
mi
                                          Hp   =            216
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21217078
55                 X    =         6481252
21
 Y    =       -5804194
73  feet           Y    =        -1696720
76  meter
 Z    =        3387539
29                 Z    =         1063970
78
 XDOT =       1293
941849                 XDOT =         310
998524
 YDOT =      16068
098527  feet/sec       YDOT =        4901
499657  meter/sec
 ZDOT =      19316
875922                 ZDOT =        5889
497779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17461881
73                 X    =         5322381
55
 Y    =      -13340194
41  feet           Y    =        -4066091
26  meter
 Z    =        3528515
39                 Z    =         1075491
49
 XDOT =       6144
116652                 XDOT =        1872
726755
 YDOT =      13181
514190  feet/sec       YDOT =        4017
725525  meter/sec
 ZDOT =      19323
733987                 ZDOT =        5889
874119


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   18176
36654206  
00016717  00000-0  10270-3 0  9079
2 25544  51
6418 337
9461 0003297 256
7502 103
3283 15
54002674 39789


Satellite: ISS
Catalog Number: 25544
Epoch time:      18176
36654206   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:       337
9461  deg
Eccentricity:     
0003297     
Arg of perigee:   256
7502  deg
Mean anomaly:     103
3283  deg
Mean motion:   15
54002674  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3978
Checksum:              322


Coasting Arc #9 (Orbit 3992)
---------------------------------------

Vector Time (GMT): 2018/177/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6203653
34                 A    =         6786826
78  meter
 Y    =         868048
45  meter          E    =           
0003609
 Z    =       -2607172
71                 I    =           51
47981
 XDOT =       1435
191067                 Wp   =          167
77445
 YDOT =      -5422
336595  meter/sec      RA   =          332
68644  deg
 ZDOT =      -5225
103170                 TA   =           41
64051
                                          MA   =           41
61304
                                          Ha   =            220
018  n
mi
                                          Hp   =            216
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20353193
37                 X    =        -6200234
75
 Y    =        2847927
99  feet           Y    =          798694
46  meter
 Z    =       -8553716
25                 Z    =        -2637299
49
 XDOT =       4708
632111                 XDOT =        1521
099259
 YDOT =     -17789
818225  feet/sec       YDOT =       -5405
806121  meter/sec
 ZDOT =     -17142
726935                 ZDOT =       -5217
923716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17561036
14                 X    =        -5352603
81
 Y    =       10566316
05  feet           Y    =         3220613
13  meter
 Z    =       -8688625
37                 Z    =        -2648293
01
 XDOT =      -1757
999294                 XDOT =        -535
838185
 YDOT =     -16978
293720  feet/sec       YDOT =       -5174
983926  meter/sec
 ZDOT =     -17109
717906                 ZDOT =       -5215
042018


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   18177
33116060  
00016717  00000-0  10270-3 0  9089
2 25544  51
6406 333
1386 0003355 259
6377 100
4397 15
53965950 39932


Satellite: ISS
Catalog Number: 25544
Epoch time:      18177
33116060   =   yrday
fracday
Element set:     908
Inclination:       51
6406  deg
RA of node:       333
1386  deg
Eccentricity:     
0003355     
Arg of perigee:   259
6377  deg
Mean anomaly:     100
4397  deg
Mean motion:   15
53965950  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3993
Checksum:              325


Coasting Arc #10 (Orbit 4008)
---------------------------------------

Vector Time (GMT): 2018/178/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5541089
32                 A    =         6783194
49  meter
 Y    =         177848
24  meter          E    =           
0007925
 Z    =        3903522
85                 I    =           51
43912
 XDOT =      -3047
531037                 Wp   =          105
17376
 YDOT =       5751
701708  meter/sec      RA   =          327
69303  deg
 ZDOT =       4055
022535                 TA   =          302
23978
                                          MA   =          302
31656
                                          Ha   =            219
935  n
mi
                                          Hp   =            216
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18179426
92                 X    =         5519727
55
 Y    =         583491
59  feet           Y    =          239692
42  meter
 Z    =       12806833
51                 Z    =         3930387
63
 XDOT =      -9998
461408                 XDOT =       -3131
318753
 YDOT =      18870
412429  feet/sec       YDOT =        5717
152952  meter/sec
 ZDOT =      13303
879709                 ZDOT =        4040
016178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16763422
31                 X    =         5109491
12
 Y    =       -6835785
11  feet           Y    =        -2083547
30  meter
 Z    =       12926976
62                 Z    =         3940142
47
 XDOT =      -2024
124444                 XDOT =        -616
953131
 YDOT =      20120
989467  feet/sec       YDOT =        6132
877590  meter/sec
 ZDOT =      13235
810585                 ZDOT =        4034
275066


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   18178
36008516  
00016717  00000-0  10270-3 0  9090
2 25544  51
6408 328
0102 0003274 266
2998  93
7780 15
53974111 40094


Satellite: ISS
Catalog Number: 25544
Epoch time:      18178
36008516   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       328
0102  deg
Eccentricity:     
0003274     
Arg of perigee:   266
2998  deg
Mean anomaly:      93
7780  deg
Mean motion:   15
53974111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4009
Checksum:              318


Coasting Arc #11 (Orbit 4023)
---------------------------------------

Vector Time (GMT): 2018/179/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4565900
92                 A    =         6779697
42  meter
 Y    =       -1367645
45  meter          E    =           
0008584
 Z    =       -4829631
05                 I    =           51
39996
 XDOT =       4352
686196                 Wp   =           65
33399
 YDOT =      -5799
331234  meter/sec      RA   =          322
68692  deg
 ZDOT =      -2472
713169                 TA   =          180
27279
                                          MA   =          180
27326
                                          Ha   =            219
940  n
mi
                                          Hp   =            215
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14979989
90                 X    =        -4526808
53
 Y    =       -4487025
75  feet           Y    =        -1418485
11  meter
 Z    =      -15845246
24                 Z    =        -4851715
77
 XDOT =      14280
466523                 XDOT =        4429
223474
 YDOT =     -19026
677276  feet/sec       YDOT =       -5750
228136  meter/sec
 ZDOT =      -8112
576014                 ZDOT =       -2451
384527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15377056
35                 X    =        -4686926
78
 Y    =        2224025
91  feet           Y    =          677883
10  meter
 Z    =      -15943812
99                 Z    =        -4859674
20
 XDOT =       5103
465543                 XDOT =        1555
536297
 YDOT =     -22182
847026  feet/sec       YDOT =       -6761
331774  meter/sec
 ZDOT =      -8016
226424                 ZDOT =       -2443
345814


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   18179
32469717  
00016717  00000-0  10270-3 0  9103
2 25544  51
6405 323
2016 0003402 269
8152  90
2611 15
54002630 40247


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
32469717   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:       323
2016  deg
Eccentricity:     
0003402     
Arg of perigee:   269
8152  deg
Mean anomaly:      90
2611  deg
Mean motion:   15
54002630  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4024
Checksum:              274


Coasting Arc #12 (Orbit 4028)
---------------------------------------

Vector Time (GMT): 2018/179/14:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          24070
95                 A    =         6780180
97  meter
 Y    =        4843169
83  meter          E    =           
0004826
 Z    =        4743034
38                 I    =           51
39481
 XDOT =      -6684
288743                 Wp   =           49
79981
 YDOT =       2649
590777  meter/sec      RA   =          321
15195  deg
 ZDOT =      -2666
750713                 TA   =           66
64773
                                          MA   =           66
59696
                                          Ha   =            220
071  n
mi
                                          Hp   =            216
017

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          78972
93                 X    =          -53127
49
 Y    =       15889664
79  feet           Y    =         4843006
57  meter
 Z    =       15561136
41                 Z    =         4742964
61
 XDOT =     -21930
081178                 XDOT =       -6700
466830
 YDOT =       8692
883127  feet/sec       YDOT =        2574
752440  meter/sec
 ZDOT =      -8749
182128                 ZDOT =       -2699
259303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11683390
36                 X    =         3561097
38
 Y    =      -10771267
99  feet           Y    =        -3283082
48  meter
 Z    =       15560039
39                 Z    =         4742700
00
 XDOT =      20445
818706                 XDOT =        6231
885542
 YDOT =       9304
530679  feet/sec       YDOT =        2836
020951  meter/sec
 ZDOT =      -8895
028135                 ZDOT =       -2711
204575


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   18179
64623627  
00016717  00000-0  10270-3 0  9111
2 25544  51
6418 321
5960 0003149 261
3017  98
7779 15
53992352 40296


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
64623627   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:       321
5960  deg
Eccentricity:     
0003149     
Arg of perigee:   261
3017  deg
Mean anomaly:      98
7779  deg
Mean motion:   15
53992352  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4029
Checksum:              331


Coasting Arc #13 (Orbit 4040)
---------------------------------------

Vector Time (GMT): 2018/180/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1455356
86                 A    =         6778600
18  meter
 Y    =       -4221002
76  meter          E    =           
0010593
 Z    =       -5109978
43                 I    =           51
36541
 XDOT =       6278
383348                 Wp   =          106
41386
 YDOT =      -4090
330990  meter/sec      RA   =          317
14880  deg
 ZDOT =       1590
427336                 TA   =          179
00129
                                          MA   =          178
99917
                                          Ha   =            220
082  n
mi
                                          Hp   =            215
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4774792
84                 X    =        -1383226
94
 Y    =      -13848434
27  feet           Y    =        -4236873
44  meter
 Z    =      -16765021
10                 Z    =        -5116873
48
 XDOT =      20598
370565                 XDOT =        6315
930549
 YDOT =     -13419
721097  feet/sec       YDOT =       -4019
912097  meter/sec
 ZDOT =       5217
937455                 ZDOT =        1621
015800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14427355
66                 X    =        -4397458
01
 Y    =       -2327415
66  feet           Y    =         -709396
29  meter
 Z    =      -16795185
49                 Z    =        -5119172
54
 XDOT =      -2460
937058                 XDOT =        -750
093615
 YDOT =     -23395
403236  feet/sec       YDOT =       -7130
918906  meter/sec
 ZDOT =       5355
421669                 ZDOT =        1632
332525


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   18180
41792450  
00016717  00000-0  10270-3 0  9120
2 25544  51
6378 317
7496 0003040 266
7031  93
3774 15
54004105 40418


Satellite: ISS
Catalog Number: 25544
Epoch time:      18180
41792450   =   yrday
fracday
Element set:     912
Inclination:       51
6378  deg
RA of node:       317
7496  deg
Eccentricity:     
0003040     
Arg of perigee:   266
7031  deg
Mean anomaly:      93
3774  deg
Mean motion:   15
54004105  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4041
Checksum:              292


Coasting Arc #14 (Orbit 4056)
---------------------------------------

Vector Time (GMT): 2018/181/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          95819
92                 A    =         6781520
77  meter
 Y    =        5149318
77  meter          E    =           
0006462
 Z    =        4408814
29                 I    =           51
35085
 XDOT =      -6250
870519                 Wp   =           60
30452
 YDOT =       2959
322205  meter/sec      RA   =          312
13616  deg
 ZDOT =      -3313
707854                 TA   =           63
32043
                                          MA   =           63
25428
                                          Ha   =            220
059  n
mi
                                          Hp   =            216
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         314369
81                 X    =           16816
26
 Y    =       16894090
45  feet           Y    =         5149947
89  meter
 Z    =       14464613
82                 Z    =         4409088
64
 XDOT =     -20508
105376                 XDOT =       -6267
401845
 YDOT =       9709
062353  feet/sec       YDOT =        2889
328727  meter/sec
 ZDOT =     -10871
744929                 ZDOT =       -3344
111768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15180520
57                 X    =         4627022
67
 Y    =        7419504
48  feet           Y    =         2261464
96  meter
 Z    =       14465024
10                 Z    =         4408939
35
 XDOT =         -2
815226                 XDOT =           -
858081
 YDOT =      21510
855685  feet/sec       YDOT =        6556
508813  meter/sec
 ZDOT =     -11008
215132                 ZDOT =       -3355
303972


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   18181
44684091  
00016717  00000-0  10270-3 0  9136
2 25544  51
6373 312
6216 0003165 269
9697  90
1092 15
53977910 40575


Satellite: ISS
Catalog Number: 25544
Epoch time:      18181
44684091   =   yrday
fracday
Element set:     913
Inclination:       51
6373  deg
RA of node:       312
6216  deg
Eccentricity:     
0003165     
Arg of perigee:   269
9697  deg
Mean anomaly:      90
1092  deg
Mean motion:   15
53977910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4057
Checksum:              325


Coasting Arc #15 (Orbit 4071)
---------------------------------------

Vector Time (GMT): 2018/182/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1120966
93                 A    =         6785110
76  meter
 Y    =       -5831341
06  meter          E    =           
0001721
 Z    =       -3283283
66                 I    =           51
34382
 XDOT =       5862
336649                 Wp   =           63
84615
 YDOT =      -1516
914125  meter/sec      RA   =          307
13055  deg
 ZDOT =       4698
308705                 TA   =          257
86439
                                          MA   =          257
88367
                                          Ha   =            220
059  n
mi
                                          Hp   =            215
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3677713
01                 X    =         1202039
52
 Y    =      -19131696
40  feet           Y    =        -5818351
88  meter
 Z    =      -10771928
03                 Z    =        -3277642
35
 XDOT =      19233
387957                 XDOT =        5856
041901
 YDOT =      -4976
752378  feet/sec       YDOT =       -1451
393270  meter/sec
 ZDOT =      15414
398639                 ZDOT =        4726
770036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15593204
43                 X    =        -4752808
71
 Y    =      -11703074
56  feet           Y    =        -3567097
13  meter
 Z    =      -10745782
19                 Z    =        -3275314
41
 XDOT =       2994
198024                 XDOT =         912
631558
 YDOT =     -18252
068112  feet/sec       YDOT =       -5563
230361  meter/sec
 ZDOT =      15541
946155                 ZDOT =        4737
185188


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   18182
41144642  
00016717  00000-0  10270-3 0  9148
2 25544  51
6392 307
8137 0003070 274
2122  85
8680 15
54014967 40727


Satellite: ISS
Catalog Number: 25544
Epoch time:      18182
41144642   =   yrday
fracday
Element set:     914
Inclination:       51
6392  deg
RA of node:       307
8137  deg
Eccentricity:     
0003070     
Arg of perigee:   274
2122  deg
Mean anomaly:      85
8680  deg
Mean motion:   15
54014967  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4072
Checksum:              299


Coasting Arc #16 (Orbit 4087)
---------------------------------------

Vector Time (GMT): 2018/183/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2164146
89                 A    =         6788289
62  meter
 Y    =        6168157
82  meter          E    =           
0010968
 Z    =        1809832
57                 I    =           51
33397
 XDOT =      -5209
007361                 Wp   =          118
47671
 YDOT =       -170
720686  meter/sec      RA   =          302
13356  deg
 ZDOT =      -5626
056561                 TA   =           41
54043
                                          MA   =           41
45713
                                          Ha   =            220
061  n
mi
                                          Hp   =            215
978

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7100219
47                 X    =        -2241751
18
 Y    =       20236738
25  feet           Y    =         6143522
70  meter
 Z    =        5937770
91                 Z    =         1799132
30
 XDOT =     -17089
919163                 XDOT =       -5179
383129
 YDOT =       -560
107239  feet/sec       YDOT =        -228
805083  meter/sec
 ZDOT =     -18458
190816                 ZDOT =       -5651
287845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15371837
39                 X    =         4685336
04
 Y    =       14974064
00  feet           Y    =         4564094
71  meter
 Z    =        5888958
93                 Z    =         1794954
68
 XDOT =      -6539
251204                 XDOT =       -1993
163767
 YDOT =      14043
698279  feet/sec       YDOT =        4280
519235  meter/sec
 ZDOT =     -18571
025442                 ZDOT =       -5660
448555


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   18183
44035543  
00016717  00000-0  10270-3 0  9152
2 25544  51
6378 302
6855 0003123 279
2976  80
7823 15
54016861 40887


Satellite: ISS
Catalog Number: 25544
Epoch time:      18183
44035543   =   yrday
fracday
Element set:     915
Inclination:       51
6378  deg
RA of node:       302
6855  deg
Eccentricity:     
0003123     
Arg of perigee:   279
2976  deg
Mean anomaly:      80
7823  deg
Mean motion:   15
54016861  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4088
Checksum:              323


Coasting Arc #17 (Orbit 4088)
---------------------------------------

Vector Time (GMT): 2018/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 947612
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1590573
45                 A    =         6787391
87  meter
 Y    =       -6163095
27  meter          E    =           
0004675
 Z    =       -2349674
79                 I    =           51
33219
 XDOT =       5438
171144                 Wp   =           11
44913
 YDOT =       -639
641976  meter/sec      RA   =          301
65310  deg
 ZDOT =       5365
371405                 TA   =          322
22070
                                          MA   =          322
25352
                                          Ha   =            220
080  n
mi
                                          Hp   =            216
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5218416
83                 X    =         1670785
99
 Y    =      -20220128
84  feet           Y    =        -6144859
61  meter
 Z    =       -7708906
79                 Z    =        -2341754
35
 XDOT =      17841
768844                 XDOT =        5418
857830
 YDOT =      -2098
562913  feet/sec       YDOT =        -578
937220  meter/sec
 ZDOT =      17602
924557                 ZDOT =        5391
740820

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20816410
75                 X    =        -6344842
00
 Y    =       -1822644
38  feet           Y    =         -555542
01  meter
 Z    =       -7672531
49                 Z    =        -2338587
60
 XDOT =      -5157
254004                 XDOT =       -1571
931021
 YDOT =     -15608
591698  feet/sec       YDOT =       -4757
498750  meter/sec
 ZDOT =      17720
974501                 ZDOT =        5401
353028


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   18183
50466233  
00016717  00000-0  10270-3 0  9164
2 25544  51
6410 302
3659 0003180 279
8010  80
2783 15
53996316 40893


Satellite: ISS
Catalog Number: 25544
Epoch time:      18183
50466233   =   yrday
fracday
Element set:     916
Inclination:       51
6410  deg
RA of node:       302
3659  deg
Eccentricity:     
0003180     
Arg of perigee:   279
8010  deg
Mean anomaly:      80
2783  deg
Mean motion:   15
53996316  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4089
Checksum:              311
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