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

 
Date: August 8th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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


222/19:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 213 6

227/00:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 213 3

Coasting Arc #1 (Orbit 664)
---------------------------------------

Vector Time (GMT): 2018/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3418764
54                 A    =         6778243
07  meter
 Y    =       -2446796
31  meter          E    =           
0008081
 Z    =        5312403
76                 I    =           51
95847
 XDOT =       3854
689853                 Wp   =           45
76559
 YDOT =      -6610
420322  meter/sec      RA   =          116
97680  deg
 ZDOT =       -557
961762                 TA   =           49
56776
                                          MA   =           49
49730
                                          Ha   =            223
168  n
mi
                                          Hp   =            213
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11216419
09                 X    =        -3416954
18
 Y    =       -8027546
94  feet           Y    =        -2485017
59  meter
 Z    =       17429146
19                 Z    =         5295801
03
 XDOT =      12646
620251                 XDOT =        3931
033155
 YDOT =     -21687
730714  feet/sec       YDOT =       -6566
887610  meter/sec
 ZDOT =      -1830
583209                 ZDOT =        -539
052384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2592618
23                 X    =          790230
04
 Y    =       13642218
09  feet           Y    =         4158148
07  meter
 Z    =       17354910
55                 Z    =         5289776
74
 XDOT =     -23168
298744                 XDOT =       -7061
697457
 YDOT =       6647
998103  feet/sec       YDOT =        2026
309822  meter/sec
 ZDOT =      -1744
918530                 ZDOT =        -531
851168


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   18220
54736158  
00016717  00000-0  10270-3 0  9009
2 25544  51
6412 117
7634 0005589  34
8042 325
3475 15
53852044  6651


Satellite: ISS
Catalog Number: 25544
Epoch time:      18220
54736158   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:       117
7634  deg
Eccentricity:     
0005589     
Arg of perigee:    34
8042  deg
Mean anomaly:     325
3475  deg
Mean motion:   15
53852044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             665
Checksum:              304


Coasting Arc #2 (Orbit 679)
---------------------------------------

Vector Time (GMT): 2018/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2603331
18                 A    =         6779976
28  meter
 Y    =        3863560
12  meter          E    =           
0015075
 Z    =       -4938455
97                 I    =           51
97867
 XDOT =      -4330
009808                 Wp   =           86
65747
 YDOT =       5873
818005  meter/sec      RA   =          112
00494  deg
 ZDOT =       2319
693441                 TA   =          205
92085
                                          MA   =          205
99644
                                          Ha   =            223
158  n
mi
                                          Hp   =            213
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8541112
80                 X    =         2583922
25
 Y    =       12675722
17  feet           Y    =         3892564
19  meter
 Z    =      -16202283
36                 Z    =        -4925857
00
 XDOT =     -14206
068925                 XDOT =       -4406
638276
 YDOT =      19271
056446  feet/sec       YDOT =        5824
968223  meter/sec
 ZDOT =       7610
542785                 ZDOT =        2298
474462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2304197
39                 X    =          702319
36
 Y    =      -15170031
83  feet           Y    =        -4623825
70  meter
 Z    =      -16146186
40                 Z    =        -4921357
61
 XDOT =      22459
153841                 XDOT =        6845
550091
 YDOT =      -4562
430989  feet/sec       YDOT =       -1390
628965  meter/sec
 ZDOT =       7514
579249                 ZDOT =        2290
443755


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   18221
51208968  
00016717  00000-0  10270-3 0  9011
2 25544  51
6419 112
9572 0005568  37
7056 322
4486 15
53823268  6803


Satellite: ISS
Catalog Number: 25544
Epoch time:      18221
51208968   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:       112
9572  deg
Eccentricity:     
0005568     
Arg of perigee:    37
7056  deg
Mean anomaly:     322
4486  deg
Mean motion:   15
53823268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             680
Checksum:              318


Coasting Arc #3 (Orbit 695)
---------------------------------------

Vector Time (GMT): 2018/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1763480
22                 A    =         6783126
54  meter
 Y    =       -5119325
16  meter          E    =           
0015602
 Z    =        4078367
33                 I    =           52
00134
 XDOT =       4629
338316                 Wp   =           65
02165
 YDOT =      -4713
906685  meter/sec      RA   =          107
03985  deg
 ZDOT =      -3897
313111                 TA   =           65
20580
                                          MA   =           65
04358
                                          Ha   =            223
225  n
mi
                                          Hp   =            213
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5785696
25                 X    =        -1725913
53
 Y    =      -16795686
22  feet           Y    =        -5138835
77  meter
 Z    =       13380470
25                 Z    =         4069892
15
 XDOT =      15188
117835                 XDOT =        4700
637103
 YDOT =     -15465
573114  feet/sec       YDOT =       -4661
739378  meter/sec
 ZDOT =     -12786
460338                 ZDOT =       -3874
652987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6860534
71                 X    =        -2091090
98
 Y    =       16416538
43  feet           Y    =         5003760
91  meter
 Z    =       13343038
28                 Z    =         4066958
07
 XDOT =     -20500
920902                 XDOT =       -6248
680691
 YDOT =       1790
271416  feet/sec       YDOT =         545
674728  meter/sec
 ZDOT =     -12684
151137                 ZDOT =       -3866
129266


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   18222
54112833  
00016717  00000-0  10270-3 0  9021
2 25544  51
6423 107
8300 0005703  40
9269 319
2311 15
53849022  6967


Satellite: ISS
Catalog Number: 25544
Epoch time:      18222
54112833   =   yrday
fracday
Element set:     902
Inclination:       51
6423  deg
RA of node:       107
8300  deg
Eccentricity:     
0005703     
Arg of perigee:    40
9269  deg
Mean anomaly:     319
2311  deg
Mean motion:   15
53849022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             696
Checksum:              282


Coasting Arc #4 (Orbit 700)
---------------------------------------

Vector Time (GMT): 2018/222/19:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4286137
32                 A    =         6778577
77  meter
 Y    =         115861
40  meter          E    =           
0007181
 Z    =        5243927
26                 I    =           51
98734
 XDOT =       1171
402102                 Wp   =           77
79425
 YDOT =      -7500
225509  meter/sec      RA   =          105
51904  deg
 ZDOT =       1123
347515                 TA   =            1
49906
                                          MA   =            1
49690
                                          Ha   =            223
264  n
mi
                                          Hp   =            213
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14062130
33                 X    =        -4312585
97
 Y    =         380122
69  feet           Y    =           67782
75  meter
 Z    =       17204485
77                 Z    =         5223042
97
 XDOT =       3843
182748                 XDOT =        1249
728139
 YDOT =     -24607
039073  feet/sec       YDOT =       -7486
688178  meter/sec
 ZDOT =       3685
523343                 ZDOT =        1129
227575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4290260
59                 X    =         1307671
43
 Y    =      -13516649
59  feet           Y    =        -4119874
79  meter
 Z    =       17110703
70                 Z    =         5215342
49
 XDOT =      21006
572966                 XDOT =        6402
803440
 YDOT =      11366
897404  feet/sec       YDOT =        3464
630329  meter/sec
 ZDOT =       3712
833882                 ZDOT =        1131
671767


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   18222
86270233  
00016717  00000-0  10270-3 0  9036
2 25544  51
6405 106
2218 0005277  46
0078 314
1509 15
53849442  7015


Satellite: ISS
Catalog Number: 25544
Epoch time:      18222
86270233   =   yrday
fracday
Element set:     903
Inclination:       51
6405  deg
RA of node:       106
2218  deg
Eccentricity:     
0005277     
Arg of perigee:    46
0078  deg
Mean anomaly:     314
1509  deg
Mean motion:   15
53849442  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             701
Checksum:              285


Coasting Arc #5 (Orbit 715)
---------------------------------------

Vector Time (GMT): 2018/223/19:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3938816
88                 A    =         6778358
37  meter
 Y    =        1534730
78  meter          E    =           
0018854
 Z    =       -5314656
32                 I    =           51
99372
 XDOT =      -1931
083122                 Wp   =           83
89397
 YDOT =       7373
395213  meter/sec      RA   =          100
54784  deg
 ZDOT =        702
151051                 TA   =          192
76764
                                          MA   =          192
81545
                                          Ha   =            223
223  n
mi
                                          Hp   =            213
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12922627
55                 X    =         3947177
49
 Y    =        5035205
97  feet           Y    =         1578824
15  meter
 Z    =      -17436536
49                 Z    =        -5295503
09
 XDOT =      -6335
574546                 XDOT =       -2016
801535
 YDOT =      24190
929176  feet/sec       YDOT =        7351
321217  meter/sec
 ZDOT =       2303
645179                 ZDOT =         692
562643

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8847779
93                 X    =        -2696803
32
 Y    =       10818947
87  feet           Y    =         3297615
31  meter
 Z    =      -17350722
29                 Z    =        -5288500
16
 XDOT =     -20216
594903                 XDOT =       -6162
018126
 YDOT =     -12930
856812  feet/sec       YDOT =       -3941
325156  meter/sec
 ZDOT =       2259
690905                 ZDOT =         688
753788


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   18223
82742496  
00016717  00000-0  10270-3 0  9049
2 25544  51
6400 101
4164 0005383  50
9911 309
1720 15
53839355  7162


Satellite: ISS
Catalog Number: 25544
Epoch time:      18223
82742496   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       101
4164  deg
Eccentricity:     
0005383     
Arg of perigee:    50
9911  deg
Mean anomaly:     309
1720  deg
Mean motion:   15
53839355  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             716
Checksum:              295


Coasting Arc #6 (Orbit 731)
---------------------------------------

Vector Time (GMT): 2018/224/19:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3514341
36                 A    =         6780307
16  meter
 Y    =       -3139801
76  meter          E    =           
0012447
 Z    =        4868297
93                 I    =           52
00511
 XDOT =       2606
769029                 Wp   =           57
78399
 YDOT =      -6777
342595  meter/sec      RA   =           95
57677  deg
 ZDOT =      -2478
182978                 TA   =           56
47098
                                          MA   =           56
35215
                                          Ha   =            223
426  n
mi
                                          Hp   =            213
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11529991
33                 X    =        -3502617
10
 Y    =      -10301186
87  feet           Y    =        -3179035
91  meter
 Z    =       15972106
08                 Z    =         4851255
42
 XDOT =       8552
391827                 XDOT =        2694
398829
 YDOT =     -22235
375967  feet/sec       YDOT =       -6747
701975  meter/sec
 ZDOT =      -8130
521580                 ZDOT =       -2465
307546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13277302
52                 X    =         4046921
81
 Y    =       -8074332
66  feet           Y    =        -2461056
60  meter
 Z    =       15895965
33                 Z    =         4845090
23
 XDOT =      18113
073019                 XDOT =        5520
864656
 YDOT =      13821
866246  feet/sec       YDOT =        4212
904832  meter/sec
 ZDOT =      -8071
872025                 ZDOT =       -2460
306593


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   18224
85646077  
00016717  00000-0  10270-3 0  9052
2 25544  51
6401  96
2882 0005396  55
0978 305
0681 15
53802398  7320


Satellite: ISS
Catalog Number: 25544
Epoch time:      18224
85646077   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:        96
2882  deg
Eccentricity:     
0005396     
Arg of perigee:    55
0978  deg
Mean anomaly:     305
0681  deg
Mean motion:   15
53802398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             732
Checksum:              326


Coasting Arc #7 (Orbit 746)
---------------------------------------

Vector Time (GMT): 2018/225/19:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3080953
79                 A    =         6783473
84  meter
 Y    =        4530902
77  meter          E    =           
0011063
 Z    =       -4008093
28                 I    =           52
01893
 XDOT =      -3187
032795                 Wp   =           85
45981
 YDOT =       5699
564435  meter/sec      RA   =           90
61404  deg
 ZDOT =       4003
525963                 TA   =          226
03241
                                          MA   =          226
12370
                                          Ha   =            223
311  n
mi
                                          Hp   =            213
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10108116
10                 X    =         3049527
82
 Y    =       14865166
58  feet           Y    =         4565180
27  meter
 Z    =      -13149912
33                 Z    =        -3993203
86
 XDOT =     -10456
144339                 XDOT =       -3269
976670
 YDOT =      18699
358383  feet/sec       YDOT =        5663
461205  meter/sec
 ZDOT =      13134
927700                 ZDOT =        3987
843110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17117778
44                 X    =        -5217498
87
 Y    =        5645179
52  feet           Y    =         1720650
72  meter
 Z    =      -13083615
41                 Z    =        -3987885
98
 XDOT =     -14606
293808                 XDOT =       -4451
998353
 YDOT =     -14091
953566  feet/sec       YDOT =       -4295
227447  meter/sec
 ZDOT =      13063
796171                 ZDOT =        3981
845073


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   18225
82117743  
00016717  00000-0  10270-3 0  9064
2 25544  51
6410  91
4816 0005349  56
8961 303
2704 15
53826439  7477


Satellite: ISS
Catalog Number: 25544
Epoch time:      18225
82117743   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:        91
4816  deg
Eccentricity:     
0005349     
Arg of perigee:    56
8961  deg
Mean anomaly:     303
2704  deg
Mean motion:   15
53826439  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             747
Checksum:              315


Coasting Arc #8 (Orbit 762)
---------------------------------------

Vector Time (GMT): 2018/226/19:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2569259
45                 A    =         6787106
47  meter
 Y    =       -5647844
94  meter          E    =           
0018047
 Z    =        2734901
82                 I    =           52
02958
 XDOT =       3741
808444                 Wp   =           90
25337
 YDOT =      -4230
008526  meter/sec      RA   =           85
65975  deg
 ZDOT =      -5190
822527                 TA   =           58
97424
                                          MA   =           58
79714
                                          Ha   =            223
411  n
mi
                                          Hp   =            213
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8429328
92                 X    =        -2519197
25
 Y    =      -18529675
01  feet           Y    =        -5676296
15  meter
 Z    =        8972775
01                 Z    =         2722543
27
 XDOT =      12276
274422                 XDOT =        3814
045370
 YDOT =     -13877
980729  feet/sec       YDOT =       -4187
761353  meter/sec
 ZDOT =     -17030
257635                 ZDOT =       -5172
470767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20106944
97                 X    =         6128596
83
 Y    =       -3330666
64  feet           Y    =        -1015187
19  meter
 Z    =        8917990
65                 Z    =         2718203
55
 XDOT =       9900
223697                 XDOT =        3017
588183
 YDOT =      14129
960834  feet/sec       YDOT =        4306
812062  meter/sec
 ZDOT =     -16947
317181                 ZDOT =       -5165
542277


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   18226
85020812  
00016717  00000-0  10270-3 0  9079
2 25544  51
6403  86
3538 0005455  62
0531 298
1174 15
53817024  7634


Satellite: ISS
Catalog Number: 25544
Epoch time:      18226
85020812   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:        86
3538  deg
Eccentricity:     
0005455     
Arg of perigee:    62
0531  deg
Mean anomaly:     298
1174  deg
Mean motion:   15
53817024  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             763
Checksum:              297


Coasting Arc #9 (Orbit 765)
---------------------------------------

Vector Time (GMT): 2018/227/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3409068
18                 A    =         6783980
22  meter
 Y    =       -4438119
02  meter          E    =           
0016798
 Z    =        3824285
55                 I    =           52
01833
 XDOT =       2771
582210                 Wp   =           74
76801
 YDOT =      -5779
061326  meter/sec      RA   =           84
71631  deg
 ZDOT =      -4216
325015                 TA   =           59
52259
                                          MA   =           59
35680
                                          Ha   =            223
429  n
mi
                                          Hp   =            213
274

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11184606
90                 X    =        -3377762
64
 Y    =      -14560757
93  feet           Y    =        -4476066
37  meter
 Z    =       12546868
59                 Z    =         3807801
94
 XDOT =       9093
117487                 XDOT =        2856
479675
 YDOT =     -18960
174953  feet/sec       YDOT =       -5747
593062  meter/sec
 ZDOT =     -13833
087318                 ZDOT =       -4202
655380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -390346
88                 X    =         -118977
73
 Y    =      -18406430
49  feet           Y    =        -5610280
01  meter
 Z    =       12473410
13                 Z    =         3801895
41
 XDOT =      17323
168596                 XDOT =        5280
101788
 YDOT =      -9743
480951  feet/sec       YDOT =       -2969
812994  meter/sec
 ZDOT =     -13770
974735                 ZDOT =       -4197
393099


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   18227
04314945  
00016717  00000-0  10270-3 0  9085
2 25544  51
6395  85
3952 0005672  58
6762 301
4945 15
53859610  7665


Satellite: ISS
Catalog Number: 25544
Epoch time:      18227
04314945   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:        85
3952  deg
Eccentricity:     
0005672     
Arg of perigee:    58
6762  deg
Mean anomaly:     301
4945  deg
Mean motion:   15
53859610  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             766
Checksum:              334


Coasting Arc #10 (Orbit 780)
---------------------------------------

Vector Time (GMT): 2018/228/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3022272
34                 A    =         6787357
96  meter
 Y    =        5513506
14  meter          E    =           
0010907
 Z    =       -2555020
66                 I    =           52
02629
 XDOT =      -3430
406008                 Wp   =           57
41644
 YDOT =       4331
362982  meter/sec      RA   =           79
76314  deg
 ZDOT =       5311
095266                 TA   =          274
05654
                                          MA   =          274
18120
                                          Ha   =            223
452  n
mi
                                          Hp   =            213
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9915591
66                 X    =         2972804
98
 Y    =       18088930
89  feet           Y    =         5547026
60  meter
 Z    =       -8382613
71                 Z    =        -2540460
01
 XDOT =     -11254
612886                 XDOT =       -3504
383783
 YDOT =      14210
508470  feet/sec       YDOT =        4292
588365  meter/sec
 ZDOT =      17424
853234                 ZDOT =        5294
251883

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2399020
57                 X    =         -731221
47
 Y    =       20514707
11  feet           Y    =         6252882
73  meter
 Z    =       -8317937
48                 Z    =        -2535307
34
 XDOT =     -16016
505729                 XDOT =       -4881
830946
 YDOT =       5131
543809  feet/sec       YDOT =        1564
094553  meter/sec
 ZDOT =      17348
663537                 ZDOT =        5287
872646


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   18228
00786517  
00016717  00000-0  10270-3 0  9091
2 25544  51
6402  80
5881 0005747  64
0072 296
1672 15
53867548  7813


Satellite: ISS
Catalog Number: 25544
Epoch time:      18228
00786517   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:        80
5881  deg
Eccentricity:     
0005747     
Arg of perigee:    64
0072  deg
Mean anomaly:     296
1672  deg
Mean motion:   15
53867548  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             781
Checksum:              328


Coasting Arc #11 (Orbit 796)
---------------------------------------

Vector Time (GMT): 2018/229/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2495883
14                 A    =         6789759
50  meter
 Y    =       -6229213
19  meter          E    =           
0017319
 Z    =         995952
48                 I    =           52
02736
 XDOT =       4095
571719                 Wp   =          107
77032
 YDOT =      -2603
004830  meter/sec      RA   =           74
81738  deg
 ZDOT =      -5937
524540                 TA   =           61
49681
                                          MA   =           61
32252
                                          Ha   =            223
505  n
mi
                                          Hp   =            213
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8188592
99                 X    =        -2430878
63
 Y    =      -20437051
16  feet           Y    =        -6256760
40  meter
 Z    =        3267560
63                 Z    =          983986
48
 XDOT =      13436
915089                 XDOT =        4153
215982
 YDOT =      -8540
042092  feet/sec       YDOT =       -2556
883151  meter/sec
 ZDOT =     -19480
067389                 ZDOT =       -5917
489761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4828032
85                 X    =         1471584
41
 Y    =      -21488584
11  feet           Y    =        -6549720
44  meter
 Z    =        3214641
43                 Z    =          979822
71
 XDOT =      14450
502114                 XDOT =        4404
513044
 YDOT =        306
433171  feet/sec       YDOT =          93
400830  meter/sec
 ZDOT =     -19389
763388                 ZDOT =       -5909
999881


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   18229
03689163  
00016717  00000-0  10270-3 0  9106
2 25544  51
6404  75
4603 0005802  66
5195 293
6567 15
53841331  7979


Satellite: ISS
Catalog Number: 25544
Epoch time:      18229
03689163   =   yrday
fracday
Element set:     910
Inclination:       51
6404  deg
RA of node:        75
4603  deg
Eccentricity:     
0005802     
Arg of perigee:    66
5195  deg
Mean anomaly:     293
6567  deg
Mean motion:   15
53841331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             797
Checksum:              319


Coasting Arc #12 (Orbit 812)
---------------------------------------

Vector Time (GMT): 2018/230/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1879474
16                 A    =         6790022
52  meter
 Y    =        6488596
52  meter          E    =           
0018799
 Z    =         599179
22                 I    =           52
01887
 XDOT =      -4703
544078                 Wp   =           56
63597
 YDOT =        796
112607  meter/sec      RA   =           69
87495  deg
 ZDOT =       6007
366206                 TA   =          309
79982
                                          MA   =          309
96517
                                          Ha   =            223
555  n
mi
                                          Hp   =            213
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6166253
81                 X    =         1803866
72
 Y    =       21288046
33  feet           Y    =         6509191
36  meter
 Z    =        1965811
08                 Z    =          608125
27
 XDOT =     -15431
575060                 XDOT =       -4741
277266
 YDOT =       2611
918001  feet/sec       YDOT =         743
303414  meter/sec
 ZDOT =      19709
206712                 ZDOT =        5984
426525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6642464
88                 X    =        -2024623
29
 Y    =       21140604
69  feet           Y    =         6443656
31  meter
 Z    =        2005120
80                 Z    =          611160
82
 XDOT =     -12870
679735                 XDOT =       -3922
983183
 YDOT =      -5941
808418  feet/sec       YDOT =       -1811
063206  meter/sec
 ZDOT =      19606
092869                 ZDOT =        5975
937107


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   18230
06591642  
00016717  00000-0  10270-3 0  9116
2 25544  51
6408  70
3334 0005866  68
7964 291
3815 15
53837418  8137


Satellite: ISS
Catalog Number: 25544
Epoch time:      18230
06591642   =   yrday
fracday
Element set:     911
Inclination:       51
6408  deg
RA of node:        70
3334  deg
Eccentricity:     
0005866     
Arg of perigee:    68
7964  deg
Mean anomaly:     291
3815  deg
Mean motion:   15
53837418  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             813
Checksum:              317


Coasting Arc #13 (Orbit 827)
---------------------------------------

Vector Time (GMT): 2018/231/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1069747
68                 A    =         6788149
37  meter
 Y    =       -6334661
30  meter          E    =           
0010083
 Z    =       -2195321
65                 I    =           51
99897
 XDOT =       5227
505569                 Wp   =          106
27825
 YDOT =       1017
941321  meter/sec      RA   =           64
92955  deg
 ZDOT =      -5508
248348                 TA   =           97
94894
                                          MA   =           97
83450
                                          Ha   =            223
537  n
mi
                                          Hp   =            213
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3509670
86                 X    =         -988168
61
 Y    =      -20783009
52  feet           Y    =        -6346167
82  meter
 Z    =       -7202498
86                 Z    =        -2200319
93
 XDOT =      17150
608822                 XDOT =        5242
490113
 YDOT =       3339
702497  feet/sec       YDOT =        1076
482687  meter/sec
 ZDOT =     -18071
680931                 ZDOT =       -5482
818737

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8273945
22                 X    =         2521898
50
 Y    =      -19377348
77  feet           Y    =        -5906215
90  meter
 Z    =       -7224088
13                 Z    =        -2201902
06
 XDOT =      11342
276853                 XDOT =        3457
125985
 YDOT =      11508
988055  feet/sec       YDOT =        3507
939559  meter/sec
 ZDOT =     -17957
629544                 ZDOT =       -5473
485485


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   18231
03062630  
00016717  00000-0  10270-3 0  9125
2 25544  51
6395  65
5264 0005746  73
4534 286
7249 15
53825776  8282


Satellite: ISS
Catalog Number: 25544
Epoch time:      18231
03062630   =   yrday
fracday
Element set:     912
Inclination:       51
6395  deg
RA of node:        65
5264  deg
Eccentricity:     
0005746     
Arg of perigee:    73
4534  deg
Mean anomaly:     286
7249  deg
Mean motion:   15
53825776  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             828
Checksum:              321


Coasting Arc #14 (Orbit 843)
---------------------------------------

Vector Time (GMT): 2018/232/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         145805
38                 A    =         6784854
08  meter
 Y    =        5778822
23  meter          E    =           
0017740
 Z    =        3535928
09                 I    =           51
97295
 XDOT =      -5610
299408                 Wp   =           86
56181
 YDOT =      -2637
657267  meter/sec      RA   =           59
97608  deg
 ZDOT =       4523
656086                 TA   =          314
92320
                                          MA   =          315
06701
                                          Ha   =            223
553  n
mi
                                          Hp   =            213
055

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         478364
11                 X    =           63998
64
 Y    =       18959390
52  feet           Y    =         5779995
29  meter
 Z    =       11600813
95                 Z    =         3536437
71
 XDOT =     -18406
494122                 XDOT =       -5602
360759
 YDOT =      -8653
731192  feet/sec       YDOT =       -2700
351165  meter/sec
 ZDOT =      14841
391359                 ZDOT =        4496
422712

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9591087
63                 X    =        -2923363
51
 Y    =       16360428
59  feet           Y    =         4986658
63  meter
 Z    =       11602310
96                 Z    =         3536384
38
 XDOT =     -10036
149443                 XDOT =       -3059
018350
 YDOT =     -16365
075293  feet/sec       YDOT =       -4988
074949  meter/sec
 ZDOT =      14719
464261                 ZDOT =        4486
492707


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   18232
05964815  
00016717  00000-0  10270-3 0  9135
2 25544  51
6393  60
3990 0005777  75
4303 284
7490 15
53842691  8448


Satellite: ISS
Catalog Number: 25544
Epoch time:      18232
05964815   =   yrday
fracday
Element set:     913
Inclination:       51
6393  deg
RA of node:        60
3990  deg
Eccentricity:     
0005777     
Arg of perigee:    75
4303  deg
Mean anomaly:     284
7490  deg
Mean motion:   15
53842691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             844
Checksum:              327


Coasting Arc #15 (Orbit 858)
---------------------------------------

Vector Time (GMT): 2018/233/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         951796
10                 A    =         6781261
19  meter
 Y    =       -4911505
06  meter          E    =           
0015907
 Z    =       -4593360
24                 I    =           51
94338
 XDOT =       5750
329056                 Wp   =           72
86986
 YDOT =       3998
993644  meter/sec      RA   =           55
01231  deg
 ZDOT =      -3088
701434                 TA   =          166
32571
                                          MA   =          166
28257
                                          Ha   =            223
586  n
mi
                                          Hp   =            213
014

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3122690
62                 X    =         1028959
03
 Y    =      -16113861
74  feet           Y    =        -4900429
92  meter
 Z    =      -15070079
53                 Z    =        -4588549
44
 XDOT =      18865
908975                 XDOT =        5720
186935
 YDOT =      13120
057886  feet/sec       YDOT =        4063
129302  meter/sec
 ZDOT =     -10133
534888                 ZDOT =       -3060
841823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10978686
84                 X    =         3346303
75
 Y    =      -12228953
16  feet           Y    =        -3727384
92  meter
 Z    =      -15047796
31                 Z    =        -4586568
32
 XDOT =       8723
565574                 XDOT =        2658
942787
 YDOT =      20130
566289  feet/sec       YDOT =        6135
796605  meter/sec
 ZDOT =     -10008
989315                 ZDOT =       -3050
739943


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   18233
02435410  
00016717  00000-0  10270-3 0  9148
2 25544  51
6392  55
5920 0005903  78
8098 281
3717 15
53846213  8590


Satellite: ISS
Catalog Number: 25544
Epoch time:      18233
02435410   =   yrday
fracday
Element set:     914
Inclination:       51
6392  deg
RA of node:        55
5920  deg
Eccentricity:     
0005903     
Arg of perigee:    78
8098  deg
Mean anomaly:     281
3717  deg
Mean motion:   15
53846213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             859
Checksum:              312


Coasting Arc #16 (Orbit 874)
---------------------------------------

Vector Time (GMT): 2018/234/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2109849
37                 A    =         6778800
80  meter
 Y    =        3810762
18  meter          E    =           
0009437
 Z    =        5186427
42                 I    =           51
91369
 XDOT =      -5633
751586                 Wp   =           99
75436
 YDOT =      -5021
932734  meter/sec      RA   =           50
03926  deg
 ZDOT =       1394
366169                 TA   =          336
87865
                                          MA   =          336
92108
                                          Ha   =            223
649  n
mi
                                          Hp   =            213
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6922077
97                 X    =        -2177498
12
 Y    =       12502500
61  feet           Y    =         3786790
09  meter
 Z    =       17015837
98                 Z    =         5176014
38
 XDOT =     -18483
436963                 XDOT =       -5583
949234
 YDOT =     -16476
157263  feet/sec       YDOT =       -5084
654793  meter/sec
 ZDOT =       4574
692157                 ZDOT =        1367
120666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12295790
86                 X    =        -3747757
05
 Y    =        7392454
78  feet           Y    =         2253220
22  meter
 Z    =       16968546
39                 Z    =         5172012
94
 XDOT =      -7411
266412                 XDOT =       -2258
954002
 YDOT =     -22576
585519  feet/sec       YDOT =       -6881
343266  meter/sec
 ZDOT =       4453
053910                 ZDOT =        1357
290832


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   18234
05337287  
00016717  00000-0  10270-3 0  9156
2 25544  51
6377  50
4644 0005765  81
7075 278
4731 15
53837496  8758


Satellite: ISS
Catalog Number: 25544
Epoch time:      18234
05337287   =   yrday
fracday
Element set:     915
Inclination:       51
6377  deg
RA of node:        50
4644  deg
Eccentricity:     
0005765     
Arg of perigee:    81
7075  deg
Mean anomaly:     278
4731  deg
Mean motion:   15
53837496  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             875
Checksum:              338


Coasting Arc #17 (Orbit 889)
---------------------------------------

Vector Time (GMT): 2018/235/00:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3309945
15                 A    =         6778310
94  meter
 Y    =       -2601742
28  meter          E    =           
0020487
 Z    =       -5329994
71                 I    =           51
89020
 XDOT =       5146
402848                 Wp   =           90
92603
 YDOT =       5646
728028  meter/sec      RA   =           45
06073  deg
 ZDOT =        440
724068                 TA   =          183
26465
                                          MA   =          183
27804
                                          Ha   =            223
582  n
mi
                                          Hp   =            213
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10859400
09                 X    =         3364682
42
 Y    =       -8535899
85  feet           Y    =        -2564422
12  meter
 Z    =      -17486859
28                 Z    =        -5313783
47
 XDOT =      16884
523779                 XDOT =        5080
736315
 YDOT =      18526
010590  feet/sec       YDOT =        5703
911502  meter/sec
 ZDOT =       1445
945105                 ZDOT =         465
563606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13724242
22                 X    =         4183149
03
 Y    =       -2233079
24  feet           Y    =         -680642
55  meter
 Z    =      -17413699
68                 Z    =        -5307695
66
 XDOT =       5769
085850                 XDOT =        1758
417367
 YDOT =      23346
285651  feet/sec       YDOT =        7115
947866  meter/sec
 ZDOT =       1556
684504                 ZDOT =         474
477437


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   18235
01807654  
00016717  00000-0  10270-3 0  9164
2 25544  51
6381  45
6576 0005781  85
1523 275
0289 15
53828463  8909


Satellite: ISS
Catalog Number: 25544
Epoch time:      18235
01807654   =   yrday
fracday
Element set:     916
Inclination:       51
6381  deg
RA of node:        45
6576  deg
Eccentricity:     
0005781     
Arg of perigee:    85
1523  deg
Mean anomaly:     275
0289  deg
Mean motion:   15
53828463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             890
Checksum:              327
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