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

 
Date: February 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) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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


057/06:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 213 9

058/23:08:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 213 9

060/14:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 214 1

063/17:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 214 0

Coasting Arc #1 (Orbit 2051)
---------------------------------------

Vector Time (GMT): 2018/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -390935
41                 A    =         6781688
14  meter
 Y    =        5286866
02  meter          E    =           
0010400
 Z    =       -4239149
53                 I    =           51
32025
 XDOT =      -5901
301629                 Wp   =           83
10306
 YDOT =      -3309
936565  meter/sec      RA   =          234
42442  deg
 ZDOT =      -3590
154077                 TA   =          150
02755
                                          MA   =          149
96797
                                          Ha   =            222
015  n
mi
                                          Hp   =            213
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1282596
50                 X    =         -429434
15
 Y    =       17345360
97  feet           Y    =         5282278
69  meter
 Z    =      -13907970
90                 Z    =        -4241142
51
 XDOT =     -19361
225817                 XDOT =       -5846
411499
 YDOT =     -10859
371931  feet/sec       YDOT =       -3375
622375  meter/sec
 ZDOT =     -11778
720725                 ZDOT =       -3618
686701

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9580461
31                 X    =        -2920124
61
 Y    =       14507101
01  feet           Y    =         4421764
39  meter
 Z    =      -13917508
28                 Z    =        -4242056
52
 XDOT =     -10373
081414                 XDOT =       -3161
715215
 YDOT =     -18251
780837  feet/sec       YDOT =       -5563
142799  meter/sec
 ZDOT =     -11905
330996                 ZDOT =       -3628
744887


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   18052
52275071  
00016717  00000-0  10270-3 0  9002
2 25544  51
6362 235
3312 0003074 119
0394 241
1067 15
54136406 20520


Satellite: ISS
Catalog Number: 25544
Epoch time:      18052
52275071   =   yrday
fracday
Element set:     900
Inclination:       51
6362  deg
RA of node:       235
3312  deg
Eccentricity:     
0003074     
Arg of perigee:   119
0394  deg
Mean anomaly:     241
1067  deg
Mean motion:   15
54136406  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2052
Checksum:              266


Coasting Arc #2 (Orbit 2067)
---------------------------------------

Vector Time (GMT): 2018/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1658503
99                 A    =         6778645
40  meter
 Y    =       -4237773
71  meter          E    =           
0008676
 Z    =        5019156
74                 I    =           51
33020
 XDOT =       5884
754125                 Wp   =          123
94337
 YDOT =       4546
729915  meter/sec      RA   =          229
40877  deg
 ZDOT =       1887
256840                 TA   =          307
65320
                                          MA   =          307
73188
                                          Ha   =            221
950  n
mi
                                          Hp   =            213
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5441286
04                 X    =         1681388
43
 Y    =      -13903457
06  feet           Y    =        -4219098
88  meter
 Z    =       16467049
68                 Z    =         5027268
99
 XDOT =      19306
936105                 XDOT =        5824
306767
 YDOT =      14917
092896  feet/sec       YDOT =        4612
199427  meter/sec
 ZDOT =       6191
787532                 ZDOT =        1915
695574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11324480
94                 X    =         3451701
79
 Y    =       -9667554
25  feet           Y    =        -2946670
54  meter
 Z    =       16503695
45                 Z    =         5030326
37
 XDOT =       9097
278570                 XDOT =        2772
850508
 YDOT =      21481
525169  feet/sec       YDOT =        6547
568872  meter/sec
 ZDOT =       6317
841164                 ZDOT =        1925
677987


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   18053
55158377  
00016717  00000-0  10270-3 0  9016
2 25544  51
6366 230
2018 0002952 123
0133 237
1303 15
54105474 20687


Satellite: ISS
Catalog Number: 25544
Epoch time:      18053
55158377   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       230
2018  deg
Eccentricity:     
0002952     
Arg of perigee:   123
0133  deg
Mean anomaly:     237
1303  deg
Mean motion:   15
54105474  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2068
Checksum:              277


Coasting Arc #3 (Orbit 2082)
---------------------------------------

Vector Time (GMT): 2018/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2993209
11                 A    =         6777318
29  meter
 Y    =        3003693
40  meter          E    =           
0017560
 Z    =       -5301989
07                 I    =           51
34878
 XDOT =      -5452
724254                 Wp   =           96
47892
 YDOT =      -5373
609470  meter/sec      RA   =          224
38865  deg
 ZDOT =         32
187612                 TA   =          173
84036
                                          MA   =          173
81874
                                          Ha   =            222
004  n
mi
                                          Hp   =            213
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9820239
86                 X    =        -3000820
73
 Y    =        9854637
15  feet           Y    =         2970178
45  meter
 Z    =      -17394977
26                 Z    =        -5316547
55
 XDOT =     -17889
515270                 XDOT =       -5392
386191
 YDOT =     -17629
952330  feet/sec       YDOT =       -5434
248205  meter/sec
 ZDOT =        105
602402                 ZDOT =           5
847246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13161500
74                 X    =        -4011625
42
 Y    =        4248935
66  feet           Y    =         1295075
59  meter
 Z    =      -17460173
61                 Z    =        -5321860
92
 XDOT =      -7400
567631                 XDOT =       -2255
693014
 YDOT =     -22944
445796  feet/sec       YDOT =       -6993
467079  meter/sec
 ZDOT =        -11
024738                 ZDOT =          -3
360340


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   18054
51610893  
00016717  00000-0  10270-3 0  9020
2 25544  51
6370 225
3935 0003200 126
1246 234
0203 15
54143113 20835


Satellite: ISS
Catalog Number: 25544
Epoch time:      18054
51610893   =   yrday
fracday
Element set:     902
Inclination:       51
6370  deg
RA of node:       225
3935  deg
Eccentricity:     
0003200     
Arg of perigee:   126
1246  deg
Mean anomaly:     234
0203  deg
Mean motion:   15
54143113  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2083
Checksum:              259


Coasting Arc #4 (Orbit 2098)
---------------------------------------

Vector Time (GMT): 2018/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4239507
43                 A    =         6778620
90  meter
 Y    =       -1693920
71  meter          E    =           
0007236
 Z    =        5004786
80                 I    =           51
37574
 XDOT =       4623
095212                 Wp   =           81
55429
 YDOT =       5806
227536  meter/sec      RA   =          219
36994  deg
 ZDOT =      -1947
544508                 TA   =           27
42281
                                          MA   =           27
38463
                                          Ha   =            221
891  n
mi
                                          Hp   =            213
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13909145
11                 X    =         4233823
91
 Y    =       -5557482
65  feet           Y    =        -1646543
21  meter
 Z    =       16419904
21                 Z    =         5025366
87
 XDOT =      15167
635209                 XDOT =        4567
284835
 YDOT =      19049
302939  feet/sec       YDOT =        5857
614028  meter/sec
 ZDOT =      -6389
581718                 ZDOT =       -1925
223175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14828524
77                 X    =         4519734
35
 Y    =        1199902
95  feet           Y    =          365730
42  meter
 Z    =       16511761
61                 Z    =         5032784
94
 XDOT =       5176
042690                 XDOT =        1577
657812
 YDOT =      22757
549040  feet/sec       YDOT =        6936
500947  meter/sec
 ZDOT =      -6290
884096                 ZDOT =       -1917
461472


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   18055
54493345  
00016717  00000-0  10270-3 0  9036
2 25544  51
6356 220
2642 0003205 130
7876 229
3555 15
54108786 20994


Satellite: ISS
Catalog Number: 25544
Epoch time:      18055
54493345   =   yrday
fracday
Element set:     903
Inclination:       51
6356  deg
RA of node:       220
2642  deg
Eccentricity:     
0003205     
Arg of perigee:   130
7876  deg
Mean anomaly:     229
3555  deg
Mean motion:   15
54108786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2099
Checksum:              314


Coasting Arc #5 (Orbit 2113)
---------------------------------------

Vector Time (GMT): 2018/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5311865
44                 A    =         6781651
63  meter
 Y    =         433249
55  meter          E    =           
0011055
 Z    =       -4205624
84                 I    =           51
41426
 XDOT =      -3364
889210                 Wp   =          117
27843
 YDOT =      -5830
116755  meter/sec      RA   =          214
35964  deg
 ZDOT =       3651
831720                 TA   =          190
30232
                                          MA   =          190
32500
                                          Ha   =            221
899  n
mi
                                          Hp   =            213
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17427380
07                 X    =        -5295887
00
 Y    =        1421422
41  feet           Y    =          373937
81  meter
 Z    =      -13797981
77                 Z    =        -4231388
83
 XDOT =     -11039
662761                 XDOT =       -3317
183563
 YDOT =     -19127
679644  feet/sec       YDOT =       -5867
478386  meter/sec
 ZDOT =      11981
075196                 ZDOT =        3635
602603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16251009
62                 X    =        -4953307
73
 Y    =       -6201400
65  feet           Y    =        -1890186
92  meter
 Z    =      -13912786
74                 Z    =        -4240617
40
 XDOT =      -2226
138945                 XDOT =        -678
527151
 YDOT =     -20867
295608  feet/sec       YDOT =       -6360
351701  meter/sec
 ZDOT =      11909
493033                 ZDOT =        3630
013477


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   18056
50945067  
00016717  00000-0  10270-3 0  9047
2 25544  51
6375 215
4558 0003155 134
7342 225
4068 15
54152051 21141


Satellite: ISS
Catalog Number: 25544
Epoch time:      18056
50945067   =   yrday
fracday
Element set:     904
Inclination:       51
6375  deg
RA of node:       215
4558  deg
Eccentricity:     
0003155     
Arg of perigee:   134
7342  deg
Mean anomaly:     225
4068  deg
Mean motion:   15
54152051  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2114
Checksum:              292


Coasting Arc #6 (Orbit 2126)
---------------------------------------

Vector Time (GMT): 2018/057/06:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1701033
67                 A    =         6781536
23  meter
 Y    =       -4965467
57  meter          E    =           
0012320
 Z    =        4287191
06                 I    =           51
43795
 XDOT =       6776
832365                 Wp   =          112
17061
 YDOT =        729
319199  meter/sec      RA   =          210
46087  deg
 ZDOT =       3520
870822                 TA   =          301
82939
                                          MA   =          301
94928
                                          Ha   =            221
812  n
mi
                                          Hp   =            213
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5580819
14                 X    =        -1666206
55
 Y    =      -16290904
10  feet           Y    =        -4984294
79  meter
 Z    =       14065587
46                 Z    =         4279012
98
 XDOT =      22233
701985                 XDOT =        6751
071061
 YDOT =       2392
779525  feet/sec       YDOT =         804
958498  meter/sec
 ZDOT =      11551
413458                 ZDOT =        3553
727070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17035443
89                 X    =         5192403
30
 Y    =       -2709172
37  feet           Y    =         -825755
74  meter
 Z    =       14029750
02                 Z    =         4276267
81
 XDOT =      -6464
547288                 XDOT =       -1970
394013
 YDOT =      20144
364715  feet/sec       YDOT =        6140
002365  meter/sec
 ZDOT =      11697
684826                 ZDOT =        3565
454335


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   18057
34536211  
00016717  00000-0  10270-3 0  9058
2 25544  51
6402 211
2933 0002596 130
5276 229
6103 15
54139173 21271


Satellite: ISS
Catalog Number: 25544
Epoch time:      18057
34536211   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       211
2933  deg
Eccentricity:     
0002596     
Arg of perigee:   130
5276  deg
Mean anomaly:     229
6103  deg
Mean motion:   15
54139173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2127
Checksum:              283


Coasting Arc #7 (Orbit 2141)
---------------------------------------

Vector Time (GMT): 2018/058/06:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          68611
65                 A    =         6778308
32  meter
 Y    =        4509209
34  meter          E    =           
0014654
 Z    =       -5073395
05                 I    =           51
45495
 XDOT =      -7211
535931                 Wp   =           85
37376
 YDOT =      -1873
865208  meter/sec      RA   =          205
45221  deg
 ZDOT =      -1766
266297                 TA   =          167
49202
                                          MA   =          167
45561
                                          Ha   =            221
665  n
mi
                                          Hp   =            213
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         225103
84                 X    =           42826
65
 Y    =       14793993
90  feet           Y    =         4509832
14  meter
 Z    =      -16644996
88                 Z    =        -5073124
65
 XDOT =     -23659
894787                 XDOT =       -7181
466501
 YDOT =      -6147
851732  feet/sec       YDOT =       -1954
341528  meter/sec
 ZDOT =      -5794
836932                 ZDOT =       -1801
223478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14656618
65                 X    =        -4467337
36
 Y    =       -2029516
50  feet           Y    =         -618596
63  meter
 Z    =      -16644321
57                 Z    =        -5073189
22
 XDOT =       9690
312274                 XDOT =        2953
607181
 YDOT =     -21268
810026  feet/sec       YDOT =       -6482
733296  meter/sec
 ZDOT =      -5950
356019                 ZDOT =       -1813
668515


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   18058
30987078  
00016717  00000-0  10270-3 0  9067
2 25544  51
6387 206
4839 0002546 135
0902 225
0457 15
54175507 21425


Satellite: ISS
Catalog Number: 25544
Epoch time:      18058
30987078   =   yrday
fracday
Element set:     906
Inclination:       51
6387  deg
RA of node:       206
4839  deg
Eccentricity:     
0002546     
Arg of perigee:   135
0902  deg
Mean anomaly:     225
0457  deg
Mean motion:   15
54175507  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2142
Checksum:              316


Coasting Arc #8 (Orbit 2152)
---------------------------------------

Vector Time (GMT): 2018/058/23:08:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1315275
45                 A    =         6779541
73  meter
 Y    =       -4630944
52  meter          E    =           
0010144
 Z    =        4768632
89                 I    =           51
47713
 XDOT =       7180
528755                 Wp   =          124
06028
 YDOT =        665
755937  meter/sec      RA   =          202
09253  deg
 ZDOT =       2617
484832                 TA   =          300
03399
                                          MA   =          300
13459
                                          Ha   =            221
698  n
mi
                                          Hp   =            213
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4315208
17                 X    =        -1286556
15
 Y    =      -15193387
52  feet           Y    =        -4645491
91  meter
 Z    =       15645121
05                 Z    =         4762313
99
 XDOT =      23558
165206                 XDOT =        7159
836378
 YDOT =       2184
238640  feet/sec       YDOT =         745
938033  meter/sec
 ZDOT =       8587
548660                 ZDOT =        2652
314178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5359569
50                 X    =        -1633596
78
 Y    =       14886182
16  feet           Y    =         4537308
32  meter
 Z    =       15617504
73                 Z    =         4760215
44
 XDOT =     -16638
326293                 XDOT =       -5071
361854
 YDOT =     -15195
558571  feet/sec       YDOT =       -4631
606252  meter/sec
 ZDOT =       8742
654893                 ZDOT =        2664
761211


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   18059
01717673  
00016717  00000-0  10270-3 0  9079
2 25544  51
6365 202
9577 0002693 139
4350 220
7004 15
54185068 21534


Satellite: ISS
Catalog Number: 25544
Epoch time:      18059
01717673   =   yrday
fracday
Element set:     907
Inclination:       51
6365  deg
RA of node:       202
9577  deg
Eccentricity:     
0002693     
Arg of perigee:   139
4350  deg
Mean anomaly:     220
7004  deg
Mean motion:   15
54185068  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2153
Checksum:              307


Coasting Arc #9 (Orbit 2167)
---------------------------------------

Vector Time (GMT): 2018/059/23:08:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -436746
47                 A    =         6777455
85  meter
 Y    =        4253140
41  meter          E    =           
0016225
 Z    =       -5272673
97                 I    =           51
50194
 XDOT =      -7435
407716                 Wp   =           92
42412
 YDOT =      -1672
670937  meter/sec      RA   =          197
08345  deg
 ZDOT =       -735
984074                 TA   =          170
53626
                                          MA   =          170
50565
                                          Ha   =            221
691  n
mi
                                          Hp   =            213
902

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1432895
25                 X    =         -458662
55
 Y    =       13953872
75  feet           Y    =         4248133
36  meter
 Z    =      -17298799
10                 Z    =        -5274849
12
 XDOT =     -24394
382269                 XDOT =       -7412
575913
 YDOT =      -5487
765541  feet/sec       YDOT =       -1755
691187  meter/sec
 ZDOT =      -2414
645913                 ZDOT =        -772
046187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9088862
45                 X    =         2770285
27
 Y    =      -10667898
66  feet           Y    =        -3251575
51  meter
 Z    =      -17308978
06                 Z    =        -5275776
51
 XDOT =      16033
462056                 XDOT =        4886
999235
 YDOT =      17824
472785  feet/sec       YDOT =        5432
899305  meter/sec
 ZDOT =      -2575
150596                 ZDOT =        -784
905902


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   18059
98168131  
00016717  00000-0  10270-3 0  9085
2 25544  51
6376 198
1485 0002723 140
3057 219
8295 15
54165182 21681


Satellite: ISS
Catalog Number: 25544
Epoch time:      18059
98168131   =   yrday
fracday
Element set:     908
Inclination:       51
6376  deg
RA of node:       198
1485  deg
Eccentricity:     
0002723     
Arg of perigee:   140
3057  deg
Mean anomaly:     219
8295  deg
Mean motion:   15
54165182  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2168
Checksum:              330


Coasting Arc #10 (Orbit 2177)
---------------------------------------

Vector Time (GMT): 2018/060/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3807270
93                 A    =         6783005
73  meter
 Y    =        4092440
45  meter          E    =           
0007513
 Z    =       -3848119
85                 I    =           51
54404
 XDOT =      -6173
705735                 Wp   =           98
71202
 YDOT =       1857
552155  meter/sec      RA   =          193
92302  deg
 ZDOT =      -4140
718150                 TA   =          127
68463
                                          MA   =          127
61647
                                          Ha   =            221
677  n
mi
                                          Hp   =            214
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12491046
37                 X    =         3779916
89
 Y    =       13426641
89  feet           Y    =         4134862
59  meter
 Z    =      -12625065
11                 Z    =        -3829692
79
 XDOT =     -20254
940076                 XDOT =       -6173
905597
 YDOT =       6094
331216  feet/sec       YDOT =        1788
511945  meter/sec
 ZDOT =     -13585
033302                 ZDOT =       -4170
707856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15572984
72                 X    =         4746645
74
 Y    =        9789699
81  feet           Y    =         2983900
50  meter
 Z    =      -12543410
45                 Z    =        -3823231
50
 XDOT =     -17240
664263                 XDOT =       -5254
954467
 YDOT =       9881
801696  feet/sec       YDOT =        3011
973157  meter/sec
 ZDOT =     -13718
889825                 ZDOT =       -4181
517619


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   18060
62468064  
00016717  00000-0  10270-3 0  9097
2 25544  51
6410 194
9408 0002970 150
4787 209
6533 15
54172864 21783


Satellite: ISS
Catalog Number: 25544
Epoch time:      18060
62468064   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:       194
9408  deg
Eccentricity:     
0002970     
Arg of perigee:   150
4787  deg
Mean anomaly:     209
6533  deg
Mean motion:   15
54172864  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2178
Checksum:              324


Coasting Arc #11 (Orbit 2193)
---------------------------------------

Vector Time (GMT): 2018/061/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2235949
53                 A    =         6779298
08  meter
 Y    =       -4215955
55  meter          E    =           
0009899
 Z    =        4810931
28                 I    =           51
56471
 XDOT =       7183
572080                 Wp   =          128
92277
 YDOT =       -907
254841  meter/sec      RA   =          188
92695  deg
 ZDOT =       2534
012782                 TA   =          296
08404
                                          MA   =          296
18589
                                          Ha   =            221
583  n
mi
                                          Hp   =            214
001

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7335792
41                 X    =        -2212007
89
 Y    =      -13831875
17  feet           Y    =        -4240824
97  meter
 Z    =       15783895
26                 Z    =         4800128
74
 XDOT =      23568
149868                 XDOT =        7180
874703
 YDOT =      -2976
557878  feet/sec       YDOT =        -826
937941  meter/sec
 ZDOT =       8313
690231                 ZDOT =        2568
900949

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10906131
36                 X    =        -3324188
84
 Y    =      -11300158
25  feet           Y    =        -3444288
23  meter
 Z    =       15736222
33                 Z    =         4796400
56
 XDOT =      21005
172948                 XDOT =        6402
376714
 YDOT =      -8434
695289  feet/sec       YDOT =       -2570
895124  meter/sec
 ZDOT =       8469
283102                 ZDOT =        2581
437489


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   18061
65347522  
00016717  00000-0  10270-3 0  9108
2 25544  51
6414 189
8123 0002893 153
3988 206
7313 15
54218663 21943


Satellite: ISS
Catalog Number: 25544
Epoch time:      18061
65347522   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       189
8123  deg
Eccentricity:     
0002893     
Arg of perigee:   153
3988  deg
Mean anomaly:     206
7313  deg
Mean motion:   15
54218663  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2194
Checksum:              315


Coasting Arc #12 (Orbit 2208)
---------------------------------------

Vector Time (GMT): 2018/062/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         428369
85                 A    =         6777364
92  meter
 Y    =        4232818
81  meter          E    =           
0015706
 Z    =       -5289055
82                 I    =           51
58993
 XDOT =      -7630
731744                 Wp   =           95
01573
 YDOT =        -18
358950  meter/sec      RA   =          183
92508  deg
 ZDOT =       -635
689600                 TA   =          168
91983
                                          MA   =          168
88521
                                          Ha   =            221
507  n
mi
                                          Hp   =            214
136

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1405412
89                 X    =          406696
54
 Y    =       13887200
82  feet           Y    =         4237487
19  meter
 Z    =      -17352545
33                 Z    =        -5287028
23
 XDOT =     -25035
209135                 XDOT =       -7626
871524
 YDOT =        -60
232775  feet/sec       YDOT =        -103
669547  meter/sec
 ZDOT =      -2085
595802                 ZDOT =        -672
747091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5444311
78                 X    =         1659426
23
 Y    =       12864145
15  feet           Y    =         3920991
44  meter
 Z    =      -17343978
79                 Z    =        -5286444
73
 XDOT =     -23045
829622                 XDOT =       -7024
368869
 YDOT =       6731
929593  feet/sec       YDOT =        2051
892140  meter/sec
 ZDOT =      -2250
768871                 ZDOT =        -686
034352


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   18062
61796838  
00016717  00000-0  10270-3 0  9114
2 25544  51
6408 185
0048 0002813 157
3498 202
7779 15
54179324 22091


Satellite: ISS
Catalog Number: 25544
Epoch time:      18062
61796838   =   yrday
fracday
Element set:     911
Inclination:       51
6408  deg
RA of node:       185
0048  deg
Eccentricity:     
0002813     
Arg of perigee:   157
3498  deg
Mean anomaly:     202
7779  deg
Mean motion:   15
54179324  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2209
Checksum:              329


Coasting Arc #13 (Orbit 2224)
---------------------------------------

Vector Time (GMT): 2018/063/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1415193
62                 A    =         6777552
89  meter
 Y    =       -4129734
35  meter          E    =           
0004332
 Z    =        5180593
51                 I    =           51
62514
 XDOT =       7502
167891                 Wp   =           92
78100
 YDOT =        908
093986  meter/sec      RA   =          178
92234  deg
 ZDOT =      -1324
741100                 TA   =            9
94700
                                          MA   =            9
93843
                                          Ha   =            221
304  n
mi
                                          Hp   =            214
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4643023
67                 X    =         1436103
93
 Y    =      -13548997
20  feet           Y    =        -4113791
02  meter
 Z    =       16996697
85                 Z    =         5187519
33
 XDOT =      24613
411717                 XDOT =        7497
890588
 YDOT =       2979
310978  feet/sec       YDOT =         991
964280  meter/sec
 ZDOT =      -4346
263452                 ZDOT =       -1288
309099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         202839
20                 X    =           61825
39
 Y    =      -14283760
00  feet           Y    =        -4353690
05  meter
 Z    =       17028029
49                 Z    =         5190143
39
 XDOT =      23340
978110                 XDOT =        7114
330128
 YDOT =      -4659
278147  feet/sec       YDOT =       -1420
147979  meter/sec
 ZDOT =      -4183
961848                 ZDOT =       -1275
271571


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   18063
64675266  
00016717  00000-0  10270-3 0  9120
2 25544  51
6418 179
8757 0002694 161
1587 198
9665 15
54241518 22252


Satellite: ISS
Catalog Number: 25544
Epoch time:      18063
64675266   =   yrday
fracday
Element set:     912
Inclination:       51
6418  deg
RA of node:       179
8757  deg
Eccentricity:     
0002694     
Arg of perigee:   161
1587  deg
Mean anomaly:     198
9665  deg
Mean motion:   15
54241518  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2225
Checksum:              346


Coasting Arc #14 (Orbit 2226)
---------------------------------------

Vector Time (GMT): 2018/063/17:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3769425
73                 A    =         6780709
01  meter
 Y    =       -3429541
78  meter          E    =           
0011412
 Z    =        4467622
44                 I    =           51
63765
 XDOT =       6377
084130                 Wp   =          120
02414
 YDOT =      -2757
769286  meter/sec      RA   =          178
35688  deg
 ZDOT =       3251
688735                 TA   =          297
19305
                                          MA   =          297
30932
                                          Ha   =            221
599  n
mi
                                          Hp   =            214
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12366882
32                 X    =        -3752496
64
 Y    =      -11251777
49  feet           Y    =        -3471598
80  meter
 Z    =       14657553
94                 Z    =         4449353
68
 XDOT =      20922
192028                 XDOT =        6391
653475
 YDOT =      -9047
799495  feet/sec       YDOT =       -2686
374421  meter/sec
 ZDOT =      10668
270128                 ZDOT =        3282
701843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15865991
30                 X    =        -4835954
15
 Y    =        5493833
45  feet           Y    =         1674520
44  meter
 Z    =       14576497
41                 Z    =         4442916
41
 XDOT =       2529
105726                 XDOT =         770
871425
 YDOT =     -21472
546692  feet/sec       YDOT =       -6544
832232  meter/sec
 ZDOT =      10806
824513                 ZDOT =        3293
920112


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   18063
77535206  
00016717  00000-0  10270-3 0  9134
2 25544  51
6403 179
2356 0002720 151
1650 208
9653 15
54211433 22279


Satellite: ISS
Catalog Number: 25544
Epoch time:      18063
77535206   =   yrday
fracday
Element set:     913
Inclination:       51
6403  deg
RA of node:       179
2356  deg
Eccentricity:     
0002720     
Arg of perigee:   151
1650  deg
Mean anomaly:     208
9653  deg
Mean motion:   15
54211433  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2227
Checksum:              287


Coasting Arc #15 (Orbit 2241)
---------------------------------------

Vector Time (GMT): 2018/064/17:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2077788
03                 A    =         6777855
96  meter
 Y    =        3875002
29  meter          E    =           
0014549
 Z    =       -5170754
98                 I    =           51
66187
 XDOT =      -7256
309140                 Wp   =           89
43813
 YDOT =       1984
534113  meter/sec      RA   =          173
36208  deg
 ZDOT =      -1431
958309                 TA   =          166
78886
                                          MA   =          166
75072
                                          Ha   =            221
441  n
mi
                                          Hp   =            214
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6816889
85                 X    =         2059418
89
 Y    =       12713262
12  feet           Y    =         3898134
17  meter
 Z    =      -16964419
24                 Z    =        -5160707
00
 XDOT =     -23806
788518                 XDOT =       -7271
005791
 YDOT =       6510
938691  feet/sec       YDOT =        1903
306715  meter/sec
 ZDOT =      -4698
025949                 ZDOT =       -1467
242627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14476338
11                 X    =         4412387
86
 Y    =        -189525
29  feet           Y    =          -57767
31  meter
 Z    =      -16920054
85                 Z    =        -5157232
72
 XDOT =      -5361
113807                 XDOT =       -1634
067488
 YDOT =      23007
972594  feet/sec       YDOT =        7012
830047  meter/sec
 ZDOT =      -4855
550797                 ZDOT =       -1479
971883


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   18064
73983241  
00016717  00000-0  10270-3 0  9148
2 25544  51
6412 174
4276 0002641 156
1587 203
9689 15
54205546 22422


Satellite: ISS
Catalog Number: 25544
Epoch time:      18064
73983241   =   yrday
fracday
Element set:     914
Inclination:       51
6412  deg
RA of node:       174
4276  deg
Eccentricity:     
0002641     
Arg of perigee:   156
1587  deg
Mean anomaly:     203
9689  deg
Mean motion:   15
54205546  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2242
Checksum:              314


Coasting Arc #16 (Orbit 2257)
---------------------------------------

Vector Time (GMT): 2018/065/17:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -259045
90                 A    =         6777131
00  meter
 Y    =       -4217745
11  meter          E    =           
0003902
 Z    =        5295170
66                 I    =           51
69039
 XDOT =       7569
652456                 Wp   =          112
47788
 YDOT =      -1130
307684  meter/sec      RA   =          168
36436  deg
 ZDOT =       -531
150472                 TA   =          342
57727
                                          MA   =          342
59066
                                          Ha   =            221
425  n
mi
                                          Hp   =            214
077

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -849888
11                 X    =         -237583
67
 Y    =      -13837746
43  feet           Y    =        -4220521
34  meter
 Z    =       17372607
16                 Z    =         5293964
92
 XDOT =      24834
817768                 XDOT =        7584
309307
 YDOT =      -3708
358544  feet/sec       YDOT =       -1045
576735  meter/sec
 ZDOT =      -1742
619658                 ZDOT =        -494
344221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12779678
74                 X    =        -3895246
08
 Y    =       -5390334
87  feet           Y    =        -1642974
07  meter
 Z    =       17367703
26                 Z    =         5293675
95
 XDOT =       7522
962825                 XDOT =        2292
999069
 YDOT =     -22909
272928  feet/sec       YDOT =       -6982
746388  meter/sec
 ZDOT =      -1578
386171                 ZDOT =        -481
092105


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   18065
76860547  
00016717  00000-0  10270-3 0  9156
2 25544  51
6393 169
2987 0002642 156
4899 203
6374 15
54228028 22586


Satellite: ISS
Catalog Number: 25544
Epoch time:      18065
76860547   =   yrday
fracday
Element set:     915
Inclination:       51
6393  deg
RA of node:       169
2987  deg
Eccentricity:     
0002642     
Arg of perigee:   156
4899  deg
Mean anomaly:     203
6374  deg
Mean motion:   15
54228028  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2258
Checksum:              346


Coasting Arc #17 (Orbit 2272)
---------------------------------------

Vector Time (GMT): 2018/066/17:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1545298
85                 A    =         6779009
99  meter
 Y    =        4470330
05  meter          E    =           
0013405
 Z    =       -4868917
04                 I    =           51
72983
 XDOT =      -7255
620055                 Wp   =          116
44534
 YDOT =        154
662241  meter/sec      RA   =          163
37051  deg
 ZDOT =       2444
178958                 TA   =          177
54568
                                          MA   =          177
53910
                                          Ha   =            221
285  n
mi
                                          Hp   =            214
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5069878
11                 X    =        -1571521
94
 Y    =       14666437
19  feet           Y    =         4452902
37  meter
 Z    =      -15974137
26                 Z    =        -4876487
64
 XDOT =     -23804
527740                 XDOT =       -7268
682745
 YDOT =        507
422052  feet/sec       YDOT =          73
452107  meter/sec
 ZDOT =       8018
959835                 ZDOT =        2408
902138

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11029153
54                 X    =         3361686
00
 Y    =       10866002
06  feet           Y    =         3311957
43  meter
 Z    =      -16008400
18                 Z    =        -4879360
38
 XDOT =      -9160
592666                 XDOT =       -2792
148645
 YDOT =      20883
298214  feet/sec       YDOT =        6365
229296  meter/sec
 ZDOT =       7861
636034                 ZDOT =        2396
226663


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   18066
73307335  
00016717  00000-0  10270-3 0  9166
2 25544  51
6405 164
4905 0002446 163
4615 196
6618 15
54214389 22737


Satellite: ISS
Catalog Number: 25544
Epoch time:      18066
73307335   =   yrday
fracday
Element set:     916
Inclination:       51
6405  deg
RA of node:       164
4905  deg
Eccentricity:     
0002446     
Arg of perigee:   163
4615  deg
Mean anomaly:     196
6618  deg
Mean motion:   15
54214389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2273
Checksum:              317
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