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

 
Date: October 18th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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


291/16:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 216 4

295/18:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 216 2

300/09:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 215 6

303/21:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 215 1

Coasting Arc #1 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2018/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4982485
14                 A    =         6781463
73  meter
 Y    =        -538548
77  meter          E    =           
0007878
 Z    =       -4576446
97                 I    =           51
92433
 XDOT =      -2138
308719                 Wp   =           46
58204
 YDOT =       6666
291645  meter/sec      RA   =          128
15455  deg
 ZDOT =      -3110
588212                 TA   =          192
35698
                                          MA   =          192
37631
                                          Ha   =            220
467  n
mi
                                          Hp   =            216
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16346736
02                 X    =         5010367
25
 Y    =       -1766892
28  feet           Y    =         -482675
45  meter
 Z    =      -15014589
81                 Z    =        -4552175
78
 XDOT =      -7015
448552                 XDOT =       -2197
584357
 YDOT =      21871
035580  feet/sec       YDOT =        6642
048031  meter/sec
 ZDOT =     -10205
341902                 ZDOT =       -3121
119743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14148833
71                 X    =        -4312564
52
 Y    =        8568295
56  feet           Y    =         2611616
49  meter
 Z    =      -14905381
91                 Z    =        -4543160
41
 XDOT =      -2346
375326                 XDOT =        -715
175199
 YDOT =     -21722
329892  feet/sec       YDOT =       -6620
966151  meter/sec
 ZDOT =     -10253
373080                 ZDOT =       -3125
228115


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   18290
52169558  
00016717  00000-0  10270-3 0  9008
2 25544  51
6367 129
0935 0004059 300
2730  59
8020 15
53829294 17530


Satellite: ISS
Catalog Number: 25544
Epoch time:      18290
52169558   =   yrday
fracday
Element set:     900
Inclination:       51
6367  deg
RA of node:       129
0935  deg
Eccentricity:     
0004059     
Arg of perigee:   300
2730  deg
Mean anomaly:      59
8020  deg
Mean motion:   15
53829294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1753
Checksum:              312


Coasting Arc #2 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2018/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4271469
33                 A    =         6779000
05  meter
 Y    =        -890849
21  meter          E    =           
0000502
 Z    =        5187814
32                 I    =           51
93590
 XDOT =       3150
244328                 Wp   =          135
65991
 YDOT =      -6846
037584  meter/sec      RA   =          123
18167  deg
 ZDOT =       1417
772495                 TA   =          300
75591
                                          MA   =          300
76085
                                          Ha   =            220
758  n
mi
                                          Hp   =            216
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14014007
00                 X    =        -4286390
08
 Y    =       -2922733
62  feet           Y    =         -938698
90  meter
 Z    =       17020388
20                 Z    =         5167028
60
 XDOT =      10335
447271                 XDOT =        3219
677630
 YDOT =     -22460
753229  feet/sec       YDOT =       -6810
421064  meter/sec
 ZDOT =       4651
484565                 ZDOT =        1433
244457

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13974894
92                 X    =         4259547
97
 Y    =       -3578779
36  feet           Y    =        -1090811
95  meter
 Z    =       16926991
13                 Z    =         5159346
90
 XDOT =        344
420176                 XDOT =         104
979270
 YDOT =      23684
813314  feet/sec       YDOT =        7219
131098  meter/sec
 ZDOT =       4721
768091                 ZDOT =        1439
194914


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   18291
55072673  
00016717  00000-0  10270-3 0  9014
2 25544  51
6372 123
9657 0004068 303
9418  56
1347 15
53796853 17696


Satellite: ISS
Catalog Number: 25544
Epoch time:      18291
55072673   =   yrday
fracday
Element set:     901
Inclination:       51
6372  deg
RA of node:       123
9657  deg
Eccentricity:     
0004068     
Arg of perigee:   303
9418  deg
Mean anomaly:      56
1347  deg
Mean motion:   15
53796853  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1769
Checksum:              334


Coasting Arc #3 (Orbit 1770)
---------------------------------------

Vector Time (GMT): 2018/291/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         490924
31                 A    =         6782855
63  meter
 Y    =        5330356
40  meter          E    =           
0004039
 Z    =       -4169691
30                 I    =           51
95376
 XDOT =      -5691
791485                 Wp   =          100
98117
 YDOT =       3475
294518  meter/sec      RA   =          122
29858  deg
 ZDOT =       3774
882582                 TA   =          207
72807
                                          MA   =          207
74961
                                          Ha   =            220
500  n
mi
                                          Hp   =            216
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1610644
06                 X    =          451536
67
 Y    =       17488045
94  feet           Y    =         5335625
80  meter
 Z    =      -13680089
56                 Z    =        -4167402
50
 XDOT =     -18673
856578                 XDOT =       -5748
566753
 YDOT =      11401
884902  feet/sec       YDOT =        3411
327712  meter/sec
 ZDOT =      12384
785375                 ZDOT =        3747
095453

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17545189
49                 X    =        -5347773
76
 Y    =         926801
67  feet           Y    =          282489
15  meter
 Z    =      -13670337
96                 Z    =        -4166719
01
 XDOT =     -10494
788531                 XDOT =       -3198
811544
 YDOT =     -17962
230707  feet/sec       YDOT =       -5474
887920  meter/sec
 ZDOT =      12259
451869                 ZDOT =        3736
680930


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   18291
67935537  
00016717  00000-0  10270-3 0  9025
2 25544  51
6386 123
3223 0003798 298
9346  61
1425 15
53825271 17719


Satellite: ISS
Catalog Number: 25544
Epoch time:      18291
67935537   =   yrday
fracday
Element set:     902
Inclination:       51
6386  deg
RA of node:       123
3223  deg
Eccentricity:     
0003798     
Arg of perigee:   298
9346  deg
Mean anomaly:      61
1425  deg
Mean motion:   15
53825271  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1771
Checksum:              328


Coasting Arc #4 (Orbit 1786)
---------------------------------------

Vector Time (GMT): 2018/292/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         534380
87                 A    =         6786480
49  meter
 Y    =       -6077870
60  meter          E    =           
0009983
 Z    =        2963313
27                 I    =           51
98315
 XDOT =       5444
341906                 Wp   =           88
49615
 YDOT =      -1978
160100  meter/sec      RA   =          117
33902  deg
 ZDOT =      -5024
251212                 TA   =           57
82490
                                          MA   =           57
72812
                                          Ha   =            220
590  n
mi
                                          Hp   =            216
273

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1753218
07                 X    =          587911
22
 Y    =      -19940520
33  feet           Y    =        -6071595
27  meter
 Z    =        9722156
40                 Z    =         2966039
58
 XDOT =      17862
014127                 XDOT =        5490
463046
 YDOT =      -6490
026576  feet/sec       YDOT =       -1917
020158  meter/sec
 ZDOT =     -16483
763819                 ZDOT =       -4997
692034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19886908
88                 X    =         6061529
83
 Y    =        2226692
55  feet           Y    =          678695
89  meter
 Z    =        9735047
26                 Z    =         2967242
40
 XDOT =       6165
594838                 XDOT =        1879
273307
 YDOT =      16689
950922  feet/sec       YDOT =        5087
097041  meter/sec
 ZDOT =     -16364
094085                 ZDOT =       -4987
775877


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   18292
70838163  
00016717  00000-0  10270-3 0  9038
2 25544  51
6391 118
1943 0003697 303
1658  56
9140 15
53825292 17875


Satellite: ISS
Catalog Number: 25544
Epoch time:      18292
70838163   =   yrday
fracday
Element set:     903
Inclination:       51
6391  deg
RA of node:       118
1943  deg
Eccentricity:     
0003697     
Arg of perigee:   303
1658  deg
Mean anomaly:      56
9140  deg
Mean motion:   15
53825292  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1787
Checksum:              327


Coasting Arc #5 (Orbit 1801)
---------------------------------------

Vector Time (GMT): 2018/293/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1395246
32                 A    =         6789216
67  meter
 Y    =        6466673
34  meter          E    =           
0009166
 Z    =       -1501873
73                 I    =           52
00674
 XDOT =      -5008
646732                 Wp   =           13
55597
 YDOT =        262
879967  meter/sec      RA   =          112
38961  deg
 ZDOT =       5800
743370                 TA   =          330
12873
                                          MA   =          330
18102
                                          Ha   =            220
733  n
mi
                                          Hp   =            216
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4577579
78                 X    =        -1460159
35
 Y    =       21216119
87  feet           Y    =         6450707
65  meter
 Z    =       -4927407
25                 Z    =        -1508809
64
 XDOT =     -16432
568019                 XDOT =       -5039
391401
 YDOT =        862
467084  feet/sec       YDOT =         206
698377  meter/sec
 ZDOT =      19031
310268                 ZDOT =        5776
338087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21170096
48                 X    =        -6452645
41
 Y    =       -4752875
40  feet           Y    =        -1448676
42  meter
 Z    =       -4959285
42                 Z    =        -1511590
20
 XDOT =      -1047
722671                 XDOT =        -319
345870
 YDOT =     -15022
759908  feet/sec       YDOT =       -4578
937220  meter/sec
 ZDOT =      18921
499407                 ZDOT =        5767
273019


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   18293
67309069  
00016717  00000-0  10270-3 0  9044
2 25544  51
6392 113
3876 0003770 309
2686  50
8132 15
53833310 18020


Satellite: ISS
Catalog Number: 25544
Epoch time:      18293
67309069   =   yrday
fracday
Element set:     904
Inclination:       51
6392  deg
RA of node:       113
3876  deg
Eccentricity:     
0003770     
Arg of perigee:   309
2686  deg
Mean anomaly:      50
8132  deg
Mean motion:   15
53833310  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1802
Checksum:              308


Coasting Arc #6 (Orbit 1817)
---------------------------------------

Vector Time (GMT): 2018/294/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2126308
91                 A    =         6790126
60  meter
 Y    =       -6443223
63  meter          E    =           
0008137
 Z    =        -123967
20                 I    =           52
02107
 XDOT =       4447
482784                 Wp   =          137
48615
 YDOT =       1579
386601  meter/sec      RA   =          107
44597  deg
 ZDOT =      -6041
307198                 TA   =           43
84182
                                          MA   =           43
77726
                                          Ha   =            220
746  n
mi
                                          Hp   =            216
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6976079
10                 X    =         2198802
98
 Y    =      -21139185
14  feet           Y    =        -6419040
44  meter
 Z    =        -406716
54                 Z    =         -113461
50
 XDOT =      14591
478949                 XDOT =        4458
837062
 YDOT =       5181
714570  feet/sec       YDOT =        1629
184378  meter/sec
 ZDOT =     -19820
561674                 ZDOT =       -6019
675085

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21190131
78                 X    =         6458752
17
 Y    =        6822451
63  feet           Y    =         2079483
26  meter
 Z    =        -358769
09                 Z    =         -109352
82
 XDOT =      -4574
006022                 XDOT =       -1394
157036
 YDOT =      13215
641644  feet/sec       YDOT =        4028
127573  meter/sec
 ZDOT =     -19723
417529                 ZDOT =       -6011
697663


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   18294
70211184  
00016717  00000-0  10270-3 0  9050
2 25544  51
6387 108
2601 0003768 311
3126  48
7702 15
53851787 18187


Satellite: ISS
Catalog Number: 25544
Epoch time:      18294
70211184   =   yrday
fracday
Element set:     905
Inclination:       51
6387  deg
RA of node:       108
2601  deg
Eccentricity:     
0003768     
Arg of perigee:   311
3126  deg
Mean anomaly:      48
7702  deg
Mean motion:   15
53851787  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1818
Checksum:              311


Coasting Arc #7 (Orbit 1833)
---------------------------------------

Vector Time (GMT): 2018/295/16:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2698261
63                 A    =         6788899
15  meter
 Y    =        5979583
23  meter          E    =           
0013325
 Z    =        1716603
29                 I    =           52
02716
 XDOT =      -3828
772707                 Wp   =           48
69462
 YDOT =      -3377
232788  meter/sec      RA   =          102
50210  deg
 ZDOT =       5725
745284                 TA   =          330
03660
                                          MA   =          330
11280
                                          Ha   =            220
940  n
mi
                                          Hp   =            216
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8852564
41                 X    =        -2773264
98
 Y    =       19618055
22  feet           Y    =         5948990
18  meter
 Z    =        5631900
56                 Z    =         1703313
09
 XDOT =     -12561
590246                 XDOT =       -3818
536202
 YDOT =     -11080
160064  feet/sec       YDOT =       -3419
991028  meter/sec
 ZDOT =      18785
253556                 ZDOT =        5707
171229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19831032
99                 X    =        -6044498
86
 Y    =       -8404952
77  feet           Y    =        -2561829
60  meter
 Z    =        5571462
18                 Z    =         1698181
67
 XDOT =      10150
749302                 XDOT =        3093
948387
 YDOT =     -11508
664793  feet/sec       YDOT =       -3507
841029  meter/sec
 ZDOT =      18702
062722                 ZDOT =        5700
388718


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   18295
73112977  
00016717  00000-0  10270-3 0  9065
2 25544  51
6400 103
1322 0003780 317
4331  42
6528 15
53857339 18342


Satellite: ISS
Catalog Number: 25544
Epoch time:      18295
73112977   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       103
1322  deg
Eccentricity:     
0003780     
Arg of perigee:   317
4331  deg
Mean anomaly:      42
6528  deg
Mean motion:   15
53857339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1834
Checksum:              301


Coasting Arc #8 (Orbit 1834)
---------------------------------------

Vector Time (GMT): 2018/295/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4044184
81                 A    =         6783102
34  meter
 Y    =       -3580115
05  meter          E    =           
0006751
 Z    =       -4110814
73                 I    =           52
00729
 XDOT =       1725
963783                 Wp   =           39
08263
 YDOT =       6386
587247  meter/sec      RA   =          102
00770  deg
 ZDOT =      -3862
449969                 TA   =          191
13561
                                          MA   =          191
15056
                                          Ha   =            220
909  n
mi
                                          Hp   =            216
171

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13268322
87                 X    =         4103886
67
 Y    =      -11745784
29  feet           Y    =        -3534556
73  meter
 Z    =      -13486924
97                 Z    =        -4091023
75
 XDOT =       5662
610837                 XDOT =        1673
181042
 YDOT =      20953
370232  feet/sec       YDOT =        6405
592698  meter/sec
 ZDOT =     -12672
079951                 ZDOT =       -3854
194442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17495137
89                 X    =         5332518
03
 Y    =        3214977
36  feet           Y    =          979925
10  meter
 Z    =      -13397501
87                 Z    =        -4083558
57
 XDOT =     -12659
320238                 XDOT =       -3858
560809
 YDOT =      16210
861165  feet/sec       YDOT =        4941
070483  meter/sec
 ZDOT =     -12635
637340                 ZDOT =       -3851
342261


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   18295
79544302  
00016717  00000-0  10270-3 0  9073
2 25544  51
6389 102
8139 0003955 317
3679  42
7166 15
53842646 18353


Satellite: ISS
Catalog Number: 25544
Epoch time:      18295
79544302   =   yrday
fracday
Element set:     907
Inclination:       51
6389  deg
RA of node:       102
8139  deg
Eccentricity:     
0003955     
Arg of perigee:   317
3679  deg
Mean anomaly:      42
7166  deg
Mean motion:   15
53842646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1835
Checksum:              340


Coasting Arc #9 (Orbit 1850)
---------------------------------------

Vector Time (GMT): 2018/296/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4147634
62                 A    =         6779822
62  meter
 Y    =        2072427
55  meter          E    =           
0003151
 Z    =        4943931
50                 I    =           52
00274
 XDOT =       -902
485127                 Wp   =           95
18606
 YDOT =      -7265
074269  meter/sec      RA   =           97
04272  deg
 ZDOT =       2286
767073                 TA   =          332
57419
                                          MA   =          332
59081
                                          Ha   =            221
159  n
mi
                                          Hp   =            215
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13607725
14                 X    =        -4194516
43
 Y    =        6799303
00  feet           Y    =         2025784
08  meter
 Z    =       16220247
69                 Z    =         4923669
19
 XDOT =      -2960
909208                 XDOT =        -832
286150
 YDOT =     -23835
545502  feet/sec       YDOT =       -7274
773795  meter/sec
 ZDOT =       7502
516644                 ZDOT =        2282
554090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13943410
75                 X    =        -4249951
60
 Y    =       -6319672
01  feet           Y    =        -1926236
03  meter
 Z    =       16128861
79                 Z    =         4916077
07
 XDOT =      16093
520823                 XDOT =        4905
305147
 YDOT =     -16393
725401  feet/sec       YDOT =       -4996
807502  meter/sec
 ZDOT =       7484
373429                 ZDOT =        2281
237021


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   18296
82445681  
00016717  00000-0  10270-3 0  9089
2 25544  51
6392  97
6859 0004041 322
3696  37
7173 15
53870058 18517


Satellite: ISS
Catalog Number: 25544
Epoch time:      18296
82445681   =   yrday
fracday
Element set:     908
Inclination:       51
6392  deg
RA of node:        97
6859  deg
Eccentricity:     
0004041     
Arg of perigee:   322
3696  deg
Mean anomaly:      37
7173  deg
Mean motion:   15
53870058  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1851
Checksum:              340


Coasting Arc #10 (Orbit 1865)
---------------------------------------

Vector Time (GMT): 2018/297/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4181820
47                 A    =         6778293
67  meter
 Y    =        -407266
69  meter          E    =           
0013210
 Z    =       -5330044
64                 I    =           51
99952
 XDOT =        110
000838                 Wp   =           70
81380
 YDOT =       7641
904675  meter/sec      RA   =           92
07230  deg
 ZDOT =       -494
388446                 TA   =          194
46838
                                          MA   =          194
50623
                                          Ha   =            221
190  n
mi
                                          Hp   =            216
026

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13719883
42                 X    =         4211955
10
 Y    =       -1336176
79  feet           Y    =         -360334
51  meter
 Z    =      -17487023
08                 Z    =        -5309657
01
 XDOT =        360
895138                 XDOT =          26
940301
 YDOT =      25071
865733  feet/sec       YDOT =        7642
670330  meter/sec
 ZDOT =      -1622
009336                 ZDOT =        -494
056308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9957156
03                 X    =         3034941
16
 Y    =        9699311
61  feet           Y    =         2956350
18  meter
 Z    =      -17395256
36                 Z    =        -5302074
14
 XDOT =     -18193
817920                 XDOT =       -5545
475702
 YDOT =      15750
533145  feet/sec       YDOT =        4800
762502  meter/sec
 ZDOT =      -1621
388202                 ZDOT =        -494
199124


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   18297
78915762  
00016717  00000-0  10270-3 0  9098
2 25544  51
6384  92
8792 0004035 326
3824  33
7072 15
53834855 18666


Satellite: ISS
Catalog Number: 25544
Epoch time:      18297
78915762   =   yrday
fracday
Element set:     909
Inclination:       51
6384  deg
RA of node:        92
8792  deg
Eccentricity:     
0004035     
Arg of perigee:   326
3824  deg
Mean anomaly:      33
7072  deg
Mean motion:   15
53834855  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1866
Checksum:              348


Coasting Arc #11 (Orbit 1881)
---------------------------------------

Vector Time (GMT): 2018/298/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4138550
57                 A    =         6778657
63  meter
 Y    =       -1311949
75  meter          E    =           
0006254
 Z    =        5205781
33                 I    =           52
00224
 XDOT =        675
972344                 Wp   =           14
14235
 YDOT =      -7518
083431  meter/sec      RA   =           87
09995  deg
 ZDOT =      -1351
055249                 TA   =           88
81262
                                          MA   =           88
74097
                                          Ha   =            221
323  n
mi
                                          Hp   =            215
715

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13577921
82                 X    =        -4148860
10
 Y    =       -4304297
10  feet           Y    =        -1358287
33  meter
 Z    =       17079335
06                 Z    =         5185652
10
 XDOT =       2217
757034                 XDOT =         766
554319
 YDOT =     -24665
628055  feet/sec       YDOT =       -7510
017820  meter/sec
 ZDOT =      -4432
595960                 ZDOT =       -1347
551185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5784234
88                 X    =        -1763034
79
 Y    =      -13134288
31  feet           Y    =        -4003331
08  meter
 Z    =       16988929
29                 Z    =         5178225
65
 XDOT =      19077
437044                 XDOT =        5814
802811
 YDOT =     -14140
127364  feet/sec       YDOT =       -4309
910821  meter/sec
 ZDOT =      -4415
950145                 ZDOT =       -1345
981604


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   18298
81816603  
00016717  00000-0  10270-3 0  9109
2 25544  51
6393  87
7515 0004124 330
4100  29
6818 15
53886002 18825


Satellite: ISS
Catalog Number: 25544
Epoch time:      18298
81816603   =   yrday
fracday
Element set:     910
Inclination:       51
6393  deg
RA of node:        87
7515  deg
Eccentricity:     
0004124     
Arg of perigee:   330
4100  deg
Mean anomaly:      29
6818  deg
Mean motion:   15
53886002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1882
Checksum:              308


Coasting Arc #12 (Orbit 1896)
---------------------------------------

Vector Time (GMT): 2018/299/18:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4038400
41                 A    =         6781179
25  meter
 Y    =        2910011
85  meter          E    =           
0007912
 Z    =       -4611740
09                 I    =           52
00836
 XDOT =      -1462
722228                 Wp   =           86
80909
 YDOT =       6870
502828  meter/sec      RA   =           82
13157  deg
 ZDOT =       3059
358956                 TA   =          213
60755
                                          MA   =          213
65776
                                          Ha   =            221
511  n
mi
                                          Hp   =            215
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13249345
17                 X    =         4027961
78
 Y    =        9547282
99  feet           Y    =         2955113
60  meter
 Z    =      -15130380
88                 Z    =        -4592147
76
 XDOT =      -4798
957442                 XDOT =       -1554
302592
 YDOT =      22541
019776  feet/sec       YDOT =        6853
633653  meter/sec
 ZDOT =      10037
266916                 ZDOT =        3052
030775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1895845
41                 X    =          577853
68
 Y    =       16301859
08  feet           Y    =         4968806
65  meter
 Z    =      -15042584
42                 Z    =        -4584979
73
 XDOT =     -18778
332403                 XDOT =       -5723
635716
 YDOT =      11399
537236  feet/sec       YDOT =        3474
578950  meter/sec
 ZDOT =      10003
470836                 ZDOT =        3049
057911


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   18299
78286063  
00016717  00000-0  10270-3 0  9118
2 25544  51
6399  82
9443 0004192 338
2908  21
8066 15
53869605 18970


Satellite: ISS
Catalog Number: 25544
Epoch time:      18299
78286063   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:        82
9443  deg
Eccentricity:     
0004192     
Arg of perigee:   338
2908  deg
Mean anomaly:      21
8066  deg
Mean motion:   15
53869605  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1897
Checksum:              352


Coasting Arc #13 (Orbit 1906)
---------------------------------------

Vector Time (GMT): 2018/300/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3390664
81                 A    =         6779545
35  meter
 Y    =       -3078964
66  meter          E    =           
0012967
 Z    =       -5010160
27                 I    =           51
99679
 XDOT =       2985
479150                 Wp   =           56
27904
 YDOT =       6728
650381  meter/sec      RA   =           79
02519  deg
 ZDOT =      -2111
525439                 TA   =          193
22183
                                          MA   =          193
25585
                                          Ha   =            221
480  n
mi
                                          Hp   =            215
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11124228
36                 X    =         3449180
07
 Y    =      -10101590
09  feet           Y    =        -3040720
74  meter
 Z    =      -16437533
68                 Z    =        -4993546
97
 XDOT =       9794
879102                 XDOT =        2920
272593
 YDOT =      22075
624611  feet/sec       YDOT =        6761
671478  meter/sec
 ZDOT =      -6927
576898                 ZDOT =       -2097
181010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11041590
51                 X    =        -3365476
79
 Y    =       10312023
71  feet           Y    =         3143104
83  meter
 Z    =      -16362412
36                 Z    =        -4987263
29
 XDOT =      -9501
743208                 XDOT =       -2896
131330
 YDOT =     -21081
201522  feet/sec       YDOT =       -6425
550224  meter/sec
 ZDOT =      -6863
861480                 ZDOT =       -2092
104979


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   18300
42598897  
00016717  00000-0  10270-3 0  9124
2 25544  51
6369  79
7375 0004058 340
8002  19
2997 15
53876259 19079


Satellite: ISS
Catalog Number: 25544
Epoch time:      18300
42598897   =   yrday
fracday
Element set:     912
Inclination:       51
6369  deg
RA of node:        79
7375  deg
Eccentricity:     
0004058     
Arg of perigee:   340
8002  deg
Mean anomaly:      19
2997  deg
Mean motion:   15
53876259  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1907
Checksum:              347


Coasting Arc #14 (Orbit 1922)
---------------------------------------

Vector Time (GMT): 2018/301/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3916617
32                 A    =         6778238
47  meter
 Y    =        1466650
53  meter          E    =           
0003613
 Z    =        5332908
96                 I    =           51
98448
 XDOT =      -2330
044079                 Wp   =           21
42020
 YDOT =      -7300
984039  meter/sec      RA   =           74
05283  deg
 ZDOT =        299
878265                 TA   =           65
75402
                                          MA   =           65
71627
                                          Ha   =            221
776  n
mi
                                          Hp   =            215
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12849794
35                 X    =        -3958631
85
 Y    =        4811845
58  feet           Y    =         1422617
21  meter
 Z    =       17496420
49                 Z    =         5313780
87
 XDOT =      -7644
501571                 XDOT =       -2249
685954
 YDOT =     -23953
359707  feet/sec       YDOT =       -7326
590903  meter/sec
 ZDOT =        983
852575                 ZDOT =         288
754513

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12784360
65                 X    =         3896673
13
 Y    =       -5276527
94  feet           Y    =        -1608285
72  meter
 Z    =       17410174
56                 Z    =         5306621
21
 XDOT =       8123
012224                 XDOT =        2475
894126
 YDOT =      22730
246419  feet/sec       YDOT =        6928
179109  meter/sec
 ZDOT =        934
715833                 ZDOT =         284
901386


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   18301
45499307  
00016717  00000-0  10270-3 0  9135
2 25544  51
6368  74
6093 0004091 344
0939  16
0084 15
53831488 19236


Satellite: ISS
Catalog Number: 25544
Epoch time:      18301
45499307   =   yrday
fracday
Element set:     913
Inclination:       51
6368  deg
RA of node:        74
6093  deg
Eccentricity:     
0004091     
Arg of perigee:   344
0939  deg
Mean anomaly:      16
0084  deg
Mean motion:   15
53831488  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1923
Checksum:              315


Coasting Arc #15 (Orbit 1937)
---------------------------------------

Vector Time (GMT): 2018/302/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4392053
38                 A    =         6778848
96  meter
 Y    =         165391
22  meter          E    =           
0012575
 Z    =       -5171435
64                 I    =           51
97873
 XDOT =       1524
528688                 Wp   =           84
40843
 YDOT =       7347
404245  meter/sec      RA   =           69
07956  deg
 ZDOT =       1534
140340                 TA   =          200
29636
                                          MA   =          200
34638
                                          Ha   =            221
675  n
mi
                                          Hp   =            215
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14409623
94                 X    =         4414998
14
 Y    =         542622
12  feet           Y    =          214634
62  meter
 Z    =      -16966652
36                 Z    =        -5150044
38
 XDOT =       5001
734541                 XDOT =        1434
802457
 YDOT =      24105
656971  feet/sec       YDOT =        7363
950857  meter/sec
 ZDOT =       5033
268833                 ZDOT =        1541
328364

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14530457
40                 X    =        -4428883
42
 Y    =         231463
02  feet           Y    =           70549
93  meter
 Z    =      -16870424
59                 Z    =        -5142105
42
 XDOT =      -6225
836106                 XDOT =       -1897
634845
 YDOT =     -22748
224002  feet/sec       YDOT =       -6933
658676  meter/sec
 ZDOT =       5064
675127                 ZDOT =        1543
712979


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   18302
41967895  
00016717  00000-0  10270-3 0  9145
2 25544  51
6387  69
8023 0004039 348
0941  12
0115 15
53885692 19388


Satellite: ISS
Catalog Number: 25544
Epoch time:      18302
41967895   =   yrday
fracday
Element set:     914
Inclination:       51
6387  deg
RA of node:        69
8023  deg
Eccentricity:     
0004039     
Arg of perigee:   348
0941  deg
Mean anomaly:      12
0115  deg
Mean motion:   15
53885692  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1938
Checksum:              327


Coasting Arc #16 (Orbit 1953)
---------------------------------------

Vector Time (GMT): 2018/303/09:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4759659
27                 A    =         6781644
00  meter
 Y    =       -1740966
95  meter          E    =           
0010738
 Z    =        4503350
50                 I    =           51
97382
 XDOT =       -544
599884                 Wp   =           47
24692
 YDOT =      -6928
289882  meter/sec      RA   =           64
10923  deg
 ZDOT =      -3242
042785                 TA   =           75
27096
                                          MA   =           75
15199
                                          Ha   =            221
870  n
mi
                                          Hp   =            215
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15615680
03                 X    =        -4761712
81
 Y    =       -5711833
84  feet           Y    =        -1794204
35  meter
 Z    =       14774772
00                 Z    =         4480224
32
 XDOT =      -1786
745027                 XDOT =        -451
336947
 YDOT =     -22730
609850  feet/sec       YDOT =       -6933
858441  meter/sec
 ZDOT =     -10636
623312                 ZDOT =       -3244
461933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16076411
31                 X    =         4900090
17
 Y    =        4591398
38  feet           Y    =         1399458
23  meter
 Z    =       14670939
17                 Z    =         4471702
26
 XDOT =       3645
284897                 XDOT =        1111
082837
 YDOT =      21382
095885  feet/sec       YDOT =        6517
262826  meter/sec
 ZDOT =     -10646
612126                 ZDOT =       -3245
087376


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   18303
44867587  
00016717  00000-0  10270-3 0  9157
2 25544  51
6375  64
6740 0004003 352
3013   7
8077 15
53855137 19541


Satellite: ISS
Catalog Number: 25544
Epoch time:      18303
44867587   =   yrday
fracday
Element set:     915
Inclination:       51
6375  deg
RA of node:        64
6740  deg
Eccentricity:     
0004003     
Arg of perigee:   352
3013  deg
Mean anomaly:       7
8077  deg
Mean motion:   15
53855137  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1954
Checksum:              312


Coasting Arc #17 (Orbit 1960)
---------------------------------------

Vector Time (GMT): 2018/303/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4835076
54                 A    =         6785079
47  meter
 Y    =        3258667
19  meter          E    =           
0006275
 Z    =       -3469341
57                 I    =           51
97834
 XDOT =       -807
410892                 Wp   =           45
49763
 YDOT =       6080
973704  meter/sec      RA   =           61
70421  deg
 ZDOT =       4595
836789                 TA   =          274
02904
                                          MA   =          274
10076
                                          Ha   =            221
996  n
mi
                                          Hp   =            215
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15863112
00                 X    =         4815130
33
 Y    =       10691165
33  feet           Y    =         3312624
91  meter
 Z    =      -11382354
22                 Z    =        -3445902
49
 XDOT =      -2648
985867                 XDOT =        -897
674501
 YDOT =      19950
701128  feet/sec       YDOT =        6071
439903  meter/sec
 ZDOT =      15078
204687                 ZDOT =        4591
695472

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15799431
43                 X    =         4815666
70
 Y    =       10894839
94  feet           Y    =         3320747
21  meter
 Z    =      -11277311
53                 Z    =        -3437324
55
 XDOT =      -2211
690270                 XDOT =        -674
123194
 YDOT =      18762
607424  feet/sec       YDOT =        5718
842743  meter/sec
 ZDOT =      15058
778642                 ZDOT =        4589
915730


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   18303
89885976  
00016717  00000-0  10270-3 0  9169
2 25544  51
6376  62
4353 0004497 354
5309   5
5793 15
53866648 19614


Satellite: ISS
Catalog Number: 25544
Epoch time:      18303
89885976   =   yrday
fracday
Element set:     916
Inclination:       51
6376  deg
RA of node:        62
4353  deg
Eccentricity:     
0004497     
Arg of perigee:   354
5309  deg
Mean anomaly:       5
5793  deg
Mean motion:   15
53866648  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1961
Checksum:              357


Coasting Arc #18 (Orbit 1976)
---------------------------------------

Vector Time (GMT): 2018/304/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4777292
45                 A    =         6788257
37  meter
 Y    =       -4358162
59  meter          E    =           
0012721
 Z    =        2053114
63                 I    =           51
97290
 XDOT =       2025
613944                 Wp   =           92
08451
 YDOT =      -4859
756644  meter/sec      RA   =           56
75001  deg
 ZDOT =      -5573
271267                 TA   =           65
32375
                                          MA   =           65
19135
                                          Ha   =            221
947  n
mi
                                          Hp   =            214
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15673531
64                 X    =        -4738176
26
 Y    =      -14298433
71  feet           Y    =        -4411366
88  meter
 Z    =        6735940
40                 Z    =         2030002
94
 XDOT =       6645
715039                 XDOT =        2106
878879
 YDOT =     -15944
083479  feet/sec       YDOT =       -4836
650446  meter/sec
 ZDOT =     -18285
010719                 ZDOT =       -5563
234038

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15779573
03                 X    =        -4809613
86
 Y    =      -14229984
25  feet           Y    =        -4337299
20  meter
 Z    =        6632519
64                 Z    =         2021591
99
 XDOT =       5660
724730                 XDOT =        1725
388898
 YDOT =     -14823
809262  feet/sec       YDOT =       -4518
297063  meter/sec
 ZDOT =     -18239
207150                 ZDOT =       -5559
310339


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   18304
92785238  
00016717  00000-0  10270-3 0  9175
2 25544  51
6379  57
3069 0004576 356
8373   3
2750 15
53902093 19778


Satellite: ISS
Catalog Number: 25544
Epoch time:      18304
92785238   =   yrday
fracday
Element set:     917
Inclination:       51
6379  deg
RA of node:        57
3069  deg
Eccentricity:     
0004576     
Arg of perigee:   356
8373  deg
Mean anomaly:       3
2750  deg
Mean motion:   15
53902093  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1977
Checksum:              337
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