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

 
Date: October 22nd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 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


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 1830)
---------------------------------------

Vector Time (GMT): 2018/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -940426
97                 A    =         6786442
23  meter
 Y    =       -6035017
36  meter          E    =           
0010399
 Z    =        2950665
10                 I    =           52
01376
 XDOT =       4802
624972                 Wp   =           83
49006
 YDOT =      -3218
758498  meter/sec      RA   =          103
30622  deg
 ZDOT =      -5036
347301                 TA   =           63
01168
                                          MA   =           62
90553
                                          Ha   =            220
900  n
mi
                                          Hp   =            216
078

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3085390
32                 X    =         -887204
89
 Y    =      -19799925
73  feet           Y    =        -6045236
02  meter
 Z    =        9680659
79                 Z    =         2946226
57
 XDOT =      15756
643610                 XDOT =        4862
725484
 YDOT =     -10560
231294  feet/sec       YDOT =       -3164
716627  meter/sec
 ZDOT =     -16523
449150                 ZDOT =       -5012
871090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12624837
10                 X    =         3848050
35
 Y    =       15573815
66  feet           Y    =         4746899
01  meter
 Z    =        9661346
71                 Z    =         2944778
48
 XDOT =      -7326
955045                 XDOT =       -2233
255898
 YDOT =      16157
580543  feet/sec       YDOT =        4924
830549  meter/sec
 ZDOT =     -16417
489388                 ZDOT =       -5004
050765


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
53819223  
00016717  00000-0  10270-3 0  9005
2 25544  51
6360 104
0933 0004083 317
4381  42
6455 15
53857956 18318


Satellite: ISS
Catalog Number: 25544
Epoch time:      18295
53819223   =   yrday
fracday
Element set:     900
Inclination:       51
6360  deg
RA of node:       104
0933  deg
Eccentricity:     
0004083     
Arg of perigee:   317
4381  deg
Mean anomaly:      42
6455  deg
Mean motion:   15
53857956  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1831
Checksum:              307


Coasting Arc #2 (Orbit 1845)
---------------------------------------

Vector Time (GMT): 2018/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         199529
08                 A    =         6789196
04  meter
 Y    =        6615858
64  meter          E    =           
0010059
 Z    =       -1485113
03                 I    =           52
03015
 XDOT =      -4794
165109                 Wp   =           16
35069
 YDOT =       1444
266318  meter/sec      RA   =           98
35767  deg
 ZDOT =       5808
688625                 TA   =          327
52543
                                          MA   =          327
58728
                                          Ha   =            221
080  n
mi
                                          Hp   =            215
887

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         654622
96                 X    =          132747
94
 Y    =       21705572
96  feet           Y    =         6617716
39  meter
 Z    =       -4872418
08                 Z    =        -1484306
52
 XDOT =     -15728
888154                 XDOT =       -4838
175199
 YDOT =       4738
406554  feet/sec       YDOT =        1390
409042  meter/sec
 ZDOT =      19057
377379                 ZDOT =        5785
292670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11760370
66                 X    =        -3584560
98
 Y    =      -18256021
38  feet           Y    =        -5564435
32  meter
 Z    =       -4869522
76                 Z    =        -1484230
54
 XDOT =       9823
309035                 XDOT =        2994
144594
 YDOT =     -11366
694063  feet/sec       YDOT =       -3464
568351  meter/sec
 ZDOT =      18951
965374                 ZDOT =        5776
559046


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
50289686  
00016717  00000-0  10270-3 0  9018
2 25544  51
6366  99
2854 0003806 323
4376  36
6516 15
53852375 18461


Satellite: ISS
Catalog Number: 25544
Epoch time:      18296
50289686   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:        99
2854  deg
Eccentricity:     
0003806     
Arg of perigee:   323
4376  deg
Mean anomaly:      36
6516  deg
Mean motion:   15
53852375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1846
Checksum:              343


Coasting Arc #3 (Orbit 1861)
---------------------------------------

Vector Time (GMT): 2018/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         518396
91                 A    =         6790011
91  meter
 Y    =       -6765260
84  meter          E    =           
0007948
 Z    =        -146677
70                 I    =           52
03616
 XDOT =       4693
312545                 Wp   =          129
68019
 YDOT =        485
807745  meter/sec      RA   =           93
41531  deg
 ZDOT =      -6041
394250                 TA   =           51
89067
                                          MA   =           51
81903
                                          Ha   =            221
119  n
mi
                                          Hp   =            215
769

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1700777
25                 X    =          594721
91
 Y    =      -22195737
67  feet           Y    =        -6759037
02  meter
 Z    =        -481226
06                 Z    =         -143973
60
 XDOT =      15398
007039                 XDOT =        4716
877998
 YDOT =       1593
857432  feet/sec       YDOT =         538
422979  meter/sec
 ZDOT =     -19820
847276                 ZDOT =       -6018
537941

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10303837
98                 X    =         3140609
82
 Y    =       19732881
62  feet           Y    =         6014582
32  meter
 Z    =        -468293
15                 Z    =         -142735
75
 XDOT =     -12579
278119                 XDOT =       -3834
163971
 YDOT =       6118
267610  feet/sec       YDOT =        1864
847967  meter/sec
 ZDOT =     -19718
076361                 ZDOT =       -6010
069675


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
53191072  
00016717  00000-0  10270-3 0  9024
2 25544  51
6358  94
1576 0004007 327
8320  32
2587 15
53889726 18626


Satellite: ISS
Catalog Number: 25544
Epoch time:      18297
53191072   =   yrday
fracday
Element set:     902
Inclination:       51
6358  deg
RA of node:        94
1576  deg
Eccentricity:     
0004007     
Arg of perigee:   327
8320  deg
Mean anomaly:      32
2587  deg
Mean motion:   15
53889726  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1862
Checksum:              324


Coasting Arc #4 (Orbit 1877)
---------------------------------------

Vector Time (GMT): 2018/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1185786
74                 A    =         6788785
04  meter
 Y    =        6445457
05  meter          E    =           
0014102
 Z    =        1739330
73                 I    =           52
03489
 XDOT =      -4526
807290                 Wp   =           49
18745
 YDOT =      -2381
521104  meter/sec      RA   =           88
47224  deg
 ZDOT =       5717
893866                 TA   =          329
80072
                                          MA   =          329
88193
                                          Ha   =            221
201  n
mi
                                          Hp   =            215
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3890376
46                 X    =        -1266222
51
 Y    =       21146512
64  feet           Y    =         6431747
10  meter
 Z    =        5706465
64                 Z    =         1733374
74
 XDOT =     -14851
729954                 XDOT =       -4527
615351
 YDOT =      -7813
389448  feet/sec       YDOT =       -2432
147254  meter/sec
 ZDOT =      18759
494310                 ZDOT =        5695
901705

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8204730
92                 X    =        -2500801
99
 Y    =      -19882304
52  feet           Y    =        -6060126
42  meter
 Z    =        5678920
08                 Z    =         1730934
84
 XDOT =      15366
472353                 XDOT =        4683
700773
 YDOT =       -991
217748  feet/sec       YDOT =        -302
123169  meter/sec
 ZDOT =      18660
831254                 ZDOT =        5687
821366


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
56092344  
00016717  00000-0  10270-3 0  9031
2 25544  51
6378  89
0297 0003795 329
5665  30
5266 15
53880298 18782


Satellite: ISS
Catalog Number: 25544
Epoch time:      18298
56092344   =   yrday
fracday
Element set:     903
Inclination:       51
6378  deg
RA of node:        89
0297  deg
Eccentricity:     
0003795     
Arg of perigee:   329
5665  deg
Mean anomaly:      30
5266  deg
Mean motion:   15
53880298  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1878
Checksum:              357


Coasting Arc #5 (Orbit 1892)
---------------------------------------

Vector Time (GMT): 2018/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1864200
22                 A    =         6785784
00  meter
 Y    =       -5691864
58  meter          E    =           
0003904
 Z    =       -3195261
77                 I    =           52
02347
 XDOT =       4273
558895                 Wp   =           46
80190
 YDOT =       4118
617466  meter/sec      RA   =           83
52367  deg
 ZDOT =      -4844
491481                 TA   =          169
86268
                                          MA   =          169
85481
                                          Ha   =            221
335  n
mi
                                          Hp   =            215
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6116142
45                 X    =         1943231
05
 Y    =      -18674096
39  feet           Y    =        -5670575
99  meter
 Z    =      -10483142
30                 Z    =        -3186013
76
 XDOT =      14020
862515                 XDOT =        4250
718442
 YDOT =      13512
524496  feet/sec       YDOT =        4166
279539  meter/sec
 ZDOT =     -15894
000921                 ZDOT =       -4823
786966

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5292523
92                 X    =         1613161
29
 Y    =       18947376
33  feet           Y    =         5775160
30  meter
 Z    =      -10440855
70                 Z    =        -3182372
82
 XDOT =     -17881
172730                 XDOT =       -5450
181448
 YDOT =      -3710
515308  feet/sec       YDOT =       -1130
965066  meter/sec
 ZDOT =     -15801
343289                 ZDOT =       -4816
249435


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
52562000  
00016717  00000-0  10270-3 0  9040
2 25544  51
6384  84
2224 0003908 335
7442  24
3525 15
53872311 18937


Satellite: ISS
Catalog Number: 25544
Epoch time:      18299
52562000   =   yrday
fracday
Element set:     904
Inclination:       51
6384  deg
RA of node:        84
2224  deg
Eccentricity:     
0003908     
Arg of perigee:   335
7442  deg
Mean anomaly:      24
3525  deg
Mean motion:   15
53872311  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1893
Checksum:              301


Coasting Arc #6 (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    =        3387617
26                 A    =         6779563
60  meter
 Y    =       -3085832
65  meter          E    =           
0012983
 Z    =       -5008036
92                 I    =           51
99692
 XDOT =       2989
878832                 Wp   =           56
25471
 YDOT =       6724
628418  meter/sec      RA   =           79
02503  deg
 ZDOT =      -2118
016452                 TA   =          193
18036
                                          MA   =          193
21431
                                          Ha   =            221
494  n
mi
                                          Hp   =            215
556

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11114229
86                 X    =         3446199
24
 Y    =      -10124122
86  feet           Y    =        -3047622
43  meter
 Z    =      -16430567
33                 Z    =        -4991438
27
 XDOT =       9809
313753                 XDOT =        2924
748453
 YDOT =      22062
429194  feet/sec       YDOT =        6757
699141  meter/sec
 ZDOT =      -6948
872873                 ZDOT =       -2103
650466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11031124
38                 X    =        -3362286
71
 Y    =       10334363
31  feet           Y    =         3149913
94  meter
 Z    =      -16355511
06                 Z    =        -4985159
77
 XDOT =      -9514
439731                 XDOT =       -2900
001230
 YDOT =     -21068
496273  feet/sec       YDOT =       -6421
677664  meter/sec
 ZDOT =      -6885
059973                 ZDOT =       -2098
566280


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
42600084  
00016717  00000-0  10270-3 0  9058
2 25544  51
6369  79
7374 0004057 341
1893  18
9109 15
53873080 19079


Satellite: ISS
Catalog Number: 25544
Epoch time:      18300
42600084   =   yrday
fracday
Element set:     905
Inclination:       51
6369  deg
RA of node:        79
7374  deg
Eccentricity:     
0004057     
Arg of perigee:   341
1893  deg
Mean anomaly:      18
9109  deg
Mean motion:   15
53873080  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1907
Checksum:              311


Coasting Arc #7 (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    =       -3913789
05                 A    =         6778250
12  meter
 Y    =        1475450
46  meter          E    =           
0003615
 Z    =        5332543
83                 I    =           51
98459
 XDOT =      -2336
098542                 Wp   =           21
91324
 YDOT =      -7298
726678  meter/sec      RA   =           74
05272  deg
 ZDOT =        308
101844                 TA   =           65
18283
                                          MA   =           65
14524
                                          Ha   =            221
791  n
mi
                                          Hp   =            215
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12840515
25                 X    =        -3955900
42
 Y    =        4840716
74  feet           Y    =         1431448
23  meter
 Z    =       17495222
53                 Z    =         5313429
24
 XDOT =      -7664
365296                 XDOT =       -2255
805157
 YDOT =     -23945
953668  feet/sec       YDOT =       -7324
401609  meter/sec
 ZDOT =       1010
832822                 ZDOT =         296
948524

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12774041
00                 X    =         3893527
70
 Y    =       -5305046
17  feet           Y    =        -1616978
07  meter
 Z    =       17409036
26                 Z    =         5306274
25
 XDOT =       8140
695937                 XDOT =        2481
284122
 YDOT =      22722
874576  feet/sec       YDOT =        6925
932171  meter/sec
 ZDOT =        961
562761                 ZDOT =         293
084330


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
45500718  
00016717  00000-0  10270-3 0  9066
2 25544  51
6368  74
6093 0004090 344
4767  15
6259 15
53828011 19235


Satellite: ISS
Catalog Number: 25544
Epoch time:      18301
45500718   =   yrday
fracday
Element set:     906
Inclination:       51
6368  deg
RA of node:        74
6093  deg
Eccentricity:     
0004090     
Arg of perigee:   344
4767  deg
Mean anomaly:      15
6259  deg
Mean motion:   15
53828011  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1923
Checksum:              305


Coasting Arc #8 (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    =        4389908
48                 A    =         6778850
57  meter
 Y    =         155018
27  meter          E    =           
0012621
 Z    =       -5173620
58                 I    =           51
97880
 XDOT =       1532
421280                 Wp   =           84
35260
 YDOT =       7347
660355  meter/sec      RA   =           69
07950  deg
 ZDOT =       1524
842442                 TA   =          200
26093
                                          MA   =          200
31105
                                          Ha   =            221
689  n
mi
                                          Hp   =            215
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14402586
86                 X    =         4412980
00
 Y    =         508590
12  feet           Y    =          204238
39  meter
 Z    =      -16973820
80                 Z    =        -5152239
43
 XDOT =       5027
628871                 XDOT =        1442
736763
 YDOT =      24106
497227  feet/sec       YDOT =        7364
295461  meter/sec
 ZDOT =       5002
763916                 ZDOT =        1532
068907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14521668
71                 X    =        -4426204
62
 Y    =         265075
83  feet           Y    =           80795
11  meter
 Z    =      -16877637
20                 Z    =        -5144303
82
 XDOT =      -6249
489425                 XDOT =       -1904
844377
 YDOT =     -22748
314280  feet/sec       YDOT =       -6933
686192  meter/sec
 ZDOT =       5034
343143                 ZDOT =        1534
467790


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
41969534  
00016717  00000-0  10270-3 0  9079
2 25544  51
6386  69
8023 0004037 348
4808  11
6251 15
53881922 19389


Satellite: ISS
Catalog Number: 25544
Epoch time:      18302
41969534   =   yrday
fracday
Element set:     907
Inclination:       51
6386  deg
RA of node:        69
8023  deg
Eccentricity:     
0004037     
Arg of perigee:   348
4808  deg
Mean anomaly:      11
6251  deg
Mean motion:   15
53881922  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1938
Checksum:              322


Coasting Arc #9 (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    =       -4758763
06                 A    =         6781636
05  meter
 Y    =       -1729695
15  meter          E    =           
0010744
 Z    =        4508614
18                 I    =           51
97385
 XDOT =       -554
510247                 Wp   =           47
19703
 YDOT =      -6931
897882  meter/sec      RA   =           64
10917  deg
 ZDOT =      -3232
668804                 TA   =           75
21549
                                          MA   =           75
09647
                                          Ha   =            221
885  n
mi
                                          Hp   =            215
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15612739
69                 X    =        -4760968
27
 Y    =       -5674852
85  feet           Y    =        -1782923
37  meter
 Z    =       14792041
27                 Z    =         4485491
98
 XDOT =      -1819
259339                 XDOT =        -461
251761
 YDOT =     -22742
447118  feet/sec       YDOT =       -6937
577290  meter/sec
 ZDOT =     -10605
868778                 ZDOT =       -3235
136103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16070991
83                 X    =         4898438
31
 Y    =        4554706
44  feet           Y    =         1388274
52  meter
 Z    =       14688224
92                 Z    =         4476970
95
 XDOT =       3676
078931                 XDOT =        1120
468858
 YDOT =      21391
995568  feet/sec       YDOT =        6520
280249  meter/sec
 ZDOT =     -10616
073793                 ZDOT =       -3235
779292


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
44869488  
00016717  00000-0  10270-3 0  9081
2 25544  51
6375  64
6739 0004002 352
6965   7
4128 15
53850990 19542


Satellite: ISS
Catalog Number: 25544
Epoch time:      18303
44869488   =   yrday
fracday
Element set:     908
Inclination:       51
6375  deg
RA of node:        64
6739  deg
Eccentricity:     
0004002     
Arg of perigee:   352
6965  deg
Mean anomaly:       7
4128  deg
Mean motion:   15
53850990  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1954
Checksum:              337


Coasting Arc #10 (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    =        4836496
40                 A    =         6785068
80  meter
 Y    =        3248057
96  meter          E    =           
0006286
 Z    =       -3477364
59                 I    =           51
97837
 XDOT =       -796
639044                 Wp   =           45
96692
 YDOT =       6088
185218  meter/sec      RA   =           61
70412  deg
 ZDOT =       4588
092125                 TA   =          273
44684
                                          MA   =          273
51874
                                          Ha   =            222
010  n
mi
                                          Hp   =            215
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15867770
34                 X    =         4816707
70
 Y    =       10656358
15  feet           Y    =         3302032
44  meter
 Z    =      -11408676
46                 Z    =        -3453918
23
 XDOT =      -2613
645159                 XDOT =        -886
946475
 YDOT =      19974
360953  feet/sec       YDOT =        6078
771632  meter/sec
 ZDOT =      15052
795686                 ZDOT =        4584
003029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15804713
00                 X    =         4817276
52
 Y    =       10860096
01  feet           Y    =         3310157
26  meter
 Z    =      -11303599
64                 Z    =        -3445337
17
 XDOT =      -2179
022619                 XDOT =        -664
166094
 YDOT =      18786
335881  feet/sec       YDOT =        5726
075177  meter/sec
 ZDOT =      15033
603674                 ZDOT =        4582
242400


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
89887997  
00016717  00000-0  10270-3 0  9096
2 25544  51
6376  62
4353 0004496 354
8711   5
2395 15
53862310 19610


Satellite: ISS
Catalog Number: 25544
Epoch time:      18303
89887997   =   yrday
fracday
Element set:     909
Inclination:       51
6376  deg
RA of node:        62
4353  deg
Eccentricity:     
0004496     
Arg of perigee:   354
8711  deg
Mean anomaly:       5
2395  deg
Mean motion:   15
53862310  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1961
Checksum:              340


Coasting Arc #11 (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    =       -4781303
04                 A    =         6788251
79  meter
 Y    =       -4348522
89  meter          E    =           
0012757
 Z    =        2064148
67                 I    =           51
97293
 XDOT =       2013
493993                 Wp   =           91
92790
 YDOT =      -4870
779201  meter/sec      RA   =           56
74990  deg
 ZDOT =      -5568
052826                 TA   =           65
35215
                                          MA   =           65
21933
                                          Ha   =            221
961  n
mi
                                          Hp   =            214
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15686689
77                 X    =        -4742347
95
 Y    =      -14266807
39  feet           Y    =        -4401772
93  meter
 Z    =        6772141
30                 Z    =         2041017
10
 XDOT =       6605
951420                 XDOT =        2094
857737
 YDOT =     -15980
246724  feet/sec       YDOT =       -4847
807984  meter/sec
 ZDOT =     -18267
889849                 ZDOT =       -5558
074232

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15792835
19                 X    =        -4813656
17
 Y    =      -14198297
77  feet           Y    =        -4327641
16  meter
 Z    =        6668629
85                 Z    =         2032598
38
 XDOT =       5623
002970                 XDOT =        1713
891305
 YDOT =     -14858
831757  feet/sec       YDOT =       -4528
971920  meter/sec
 ZDOT =     -18222
348667                 ZDOT =       -5554
171874


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
92787550  
00016717  00000-0  10270-3 0  9107
2 25544  51
6379  57
3069 0004573 357
1719   2
9407 15
53897522 19778


Satellite: ISS
Catalog Number: 25544
Epoch time:      18304
92787550   =   yrday
fracday
Element set:     910
Inclination:       51
6379  deg
RA of node:        57
3069  deg
Eccentricity:     
0004573     
Arg of perigee:   357
1719  deg
Mean anomaly:       2
9407  deg
Mean motion:   15
53897522  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1977
Checksum:              339


Coasting Arc #12 (Orbit 1991)
---------------------------------------

Vector Time (GMT): 2018/305/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4476987
04                 A    =         6789875
68  meter
 Y    =        5070338
22  meter          E    =           
0014823
 Z    =        -489432
93                 I    =           51
96016
 XDOT =      -3268
915360                 Wp   =           30
34673
 YDOT =       3458
317851  meter/sec      RA   =           51
80173  deg
 ZDOT =       6016
737805                 TA   =          324
39562
                                          MA   =          324
49442
                                          Ha   =            222
043  n
mi
                                          Hp   =            214
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14688277
70                 X    =         4422333
80
 Y    =       16634967
92  feet           Y    =         5120097
40  meter
 Z    =       -1605751
09                 Z    =         -467817
89
 XDOT =     -10724
787925                 XDOT =       -3336
570749
 YDOT =      11346
187175  feet/sec       YDOT =        3421
384415  meter/sec
 ZDOT =      19739
953429                 ZDOT =        6000
693970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15053153
45                 X    =         4588201
17
 Y    =       16314750
52  feet           Y    =         4972735
96  meter
 Z    =       -1509166
22                 Z    =         -459993
87
 XDOT =      -9419
579053                 XDOT =       -2871
087695
 YDOT =      10480
880110  feet/sec       YDOT =        3194
572258  meter/sec
 ZDOT =      19667
303853                 ZDOT =        5994
594214


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   18305
89255547  
00016717  00000-0  10270-3 0  9111
2 25544  51
6385  52
5000 0004463   1
7489 358
3679 15
53910043 19921


Satellite: ISS
Catalog Number: 25544
Epoch time:      18305
89255547   =   yrday
fracday
Element set:     911
Inclination:       51
6385  deg
RA of node:        52
5000  deg
Eccentricity:     
0004463     
Arg of perigee:     1
7489  deg
Mean anomaly:     358
3679  deg
Mean motion:   15
53910043  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1992
Checksum:              316


Coasting Arc #13 (Orbit 2007)
---------------------------------------

Vector Time (GMT): 2018/306/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3862650
95                 A    =         6789379
29  meter
 Y    =       -5458922
77  meter          E    =           
0006551
 Z    =       -1168477
25                 I    =           51
93763
 XDOT =       4506
432662                 Wp   =          112
52855
 YDOT =      -1934
435236  meter/sec      RA   =           46
85340  deg
 ZDOT =      -5888
356190                 TA   =           80
09906
                                          MA   =           80
02512
                                          Ha   =            222
138  n
mi
                                          Hp   =            214
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12672739
34                 X    =        -3795644
75
 Y    =      -17909851
60  feet           Y    =        -5501743
01  meter
 Z    =       -3833586
79                 Z    =        -1187077
95
 XDOT =      14784
884061                 XDOT =        4556
332031
 YDOT =      -6346
572296  feet/sec       YDOT =       -1883
762407  meter/sec
 ZDOT =     -19318
753903                 ZDOT =       -5866
343942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13330767
49                 X    =        -4063217
93
 Y    =      -17407147
68  feet           Y    =        -5305698
61  meter
 Z    =       -3916547
26                 Z    =        -1193763
61
 XDOT =      13386
886238                 XDOT =        4080
322925
 YDOT =      -5948
411463  feet/sec       YDOT =       -1813
075814  meter/sec
 ZDOT =     -19219
453210                 ZDOT =       -5858
089338


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   18306
92154419  
00016717  00000-0  10270-3 0  9123
2 25544  51
6390  47
3716 0004720   4
7149 355
4047 15
53901614 20085


Satellite: ISS
Catalog Number: 25544
Epoch time:      18306
92154419   =   yrday
fracday
Element set:     912
Inclination:       51
6390  deg
RA of node:        47
3716  deg
Eccentricity:     
0004720     
Arg of perigee:     4
7149  deg
Mean anomaly:     355
4047  deg
Mean motion:   15
53901614  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2008
Checksum:              292


Coasting Arc #14 (Orbit 2023)
---------------------------------------

Vector Time (GMT): 2018/307/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2956789
47                 A    =         6786834
99  meter
 Y    =        5477613
82  meter          E    =           
0015600
 Z    =        2681833
64                 I    =           51
90614
 XDOT =      -5607
505425                 Wp   =           62
04268
 YDOT =        464
364668  meter/sec      RA   =           41
90048  deg
 ZDOT =       5218
008829                 TA   =          328
14044
                                          MA   =          328
23470
                                          Ha   =            222
109  n
mi
                                          Hp   =            214
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9700752
85                 X    =         2882290
36
 Y    =       17971173
95  feet           Y    =         5510262
28  meter
 Z    =        8798666
80                 Z    =         2696015
71
 XDOT =     -18397
327510                 XDOT =       -5637
628073
 YDOT =       1523
506128  feet/sec       YDOT =         401
489483  meter/sec
 ZDOT =      17119
451540                 ZDOT =        5190
695877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10631396
53                 X    =         3240449
66
 Y    =       17404807
65  feet           Y    =         5304985
37  meter
 Z    =        8861733
18                 Z    =         2701056
27
 XDOT =     -17127
533190                 XDOT =       -5220
472116
 YDOT =       1781
733323  feet/sec       YDOT =         543
072317  meter/sec
 ZDOT =      16996
504456                 ZDOT =        5180
534558


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   18307
95052976  
00016717  00000-0  10270-3 0  9133
2 25544  51
6392  42
2445 0004547   7
6236 352
4985 15
53922909 20242


Satellite: ISS
Catalog Number: 25544
Epoch time:      18307
95052976   =   yrday
fracday
Element set:     913
Inclination:       51
6392  deg
RA of node:        42
2445  deg
Eccentricity:     
0004547     
Arg of perigee:     7
6236  deg
Mean anomaly:     352
4985  deg
Mean motion:   15
53922909  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2024
Checksum:              319


Coasting Arc #15 (Orbit 2038)
---------------------------------------

Vector Time (GMT): 2018/308/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1757426
79                 A    =         6783235
12  meter
 Y    =       -5220350
14  meter          E    =           
0009998
 Z    =       -3970355
68                 I    =           51
86984
 XDOT =       6450
797569                 Wp   =           47
60249
 YDOT =        892
905815  meter/sec      RA   =           36
93668  deg
 ZDOT =      -4029
288294                 TA   =          180
41591
                                          MA   =          180
41675
                                          Ha   =            222
261  n
mi
                                          Hp   =            214
461

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5765835
92                 X    =        -1679634
46
 Y    =      -17127133
00  feet           Y    =        -5239568
15  meter
 Z    =      -13026101
33                 Z    =        -3978703
62
 XDOT =      21164
034018                 XDOT =        6459
905973
 YDOT =       2929
481019  feet/sec       YDOT =         965
093838  meter/sec
 ZDOT =     -13219
449783                 ZDOT =       -3997
929830

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6915188
02                 X    =        -2107749
31
 Y    =      -16667409
39  feet           Y    =        -5080226
38  meter
 Z    =      -13062943
91                 Z    =        -3981585
30
 XDOT =      20193
314366                 XDOT =        6154
922219
 YDOT =       1872
346250  feet/sec       YDOT =         570
691137  meter/sec
 ZDOT =     -13078
496092                 ZDOT =       -3986
325609


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   18308
91520137  
00016717  00000-0  10270-3 0  9140
2 25544  51
6403  37
4369 0004756  11
1127 349
0130 15
53918014 20399


Satellite: ISS
Catalog Number: 25544
Epoch time:      18308
91520137   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:        37
4369  deg
Eccentricity:     
0004756     
Arg of perigee:    11
1127  deg
Mean anomaly:     349
0130  deg
Mean motion:   15
53918014  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2039
Checksum:              283


Coasting Arc #16 (Orbit 2054)
---------------------------------------

Vector Time (GMT): 2018/309/21:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929140
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         339148
53                 A    =         6779820
41  meter
 Y    =        4711480
79  meter          E    =           
0007174
 Z    =        4856885
82                 I    =           51
83169
 XDOT =      -6966
301351                 Wp   =           81
21124
 YDOT =      -2052
904322  meter/sec      RA   =           31
96287  deg
 ZDOT =       2475
845579                 TA   =          344
54645
                                          MA   =          344
56835
                                          Ha   =            222
273  n
mi
                                          Hp   =            214
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1112692
04                 X    =          262845
46
 Y    =       15457614
13  feet           Y    =         4714846
95  meter
 Z    =       15934664
76                 Z    =         4858347
80
 XDOT =     -22855
319393                 XDOT =       -6954
854099
 YDOT =      -6735
250399  feet/sec       YDOT =       -2130
742234  meter/sec
 ZDOT =       8122
852950                 ZDOT =        2442
032759

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2396934
28                 X    =          730585
57
 Y    =       15304958
42  feet           Y    =         4664951
33  meter
 Z    =       15940590
11                 Z    =         4858691
87
 XDOT =     -22306
926636                 XDOT =       -6799
151239
 YDOT =      -4815
536728  feet/sec       YDOT =       -1467
775595  meter/sec
 ZDOT =       7971
030596                 ZDOT =        2429
570126


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   18309
94417804  
00016717  00000-0  10270-3 0  9151
2 25544  51
6405  32
3099 0004711  13
5375 346
5903 15
53949011 20556


Satellite: ISS
Catalog Number: 25544
Epoch time:      18309
94417804   =   yrday
fracday
Element set:     915
Inclination:       51
6405  deg
RA of node:        32
3099  deg
Eccentricity:     
0004711     
Arg of perigee:    13
5375  deg
Mean anomaly:     346
5903  deg
Mean motion:   15
53949011  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2055
Checksum:              301
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