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

 
Date: September 20th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


263/18:05:08 491 0 1 0 8 0 9
N/A -0 8 0 1 222 0
000/00:00:16 983 0 2 -0 0 215 2

264/18:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 215 5

267/01:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 215 7

268/12:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 215 8

271/01:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 216 1

274/09:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 216 3

277/08:22:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 216 5

Coasting Arc #1 (Orbit 1317)
---------------------------------------

Vector Time (GMT): 2018/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3969620
58                 A    =         6780087
74  meter
 Y    =        2639199
31  meter          E    =           
0006673
 Z    =        4815358
16                 I    =           51
24435
 XDOT =      -1706
857336                 Wp   =           97
31198
 YDOT =       7063
277715  meter/sec      RA   =          267
80274  deg
 ZDOT =      -2462
057071                 TA   =           16
99852
                                          MA   =           16
97618
                                          Ha   =            221
991  n
mi
                                          Hp   =            214
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13023689
57                 X    =         3916422
89
 Y    =        8658790
38  feet           Y    =         2683293
21  meter
 Z    =       15798419
15                 Z    =         4834511
77
 XDOT =      -5599
925643                 XDOT =       -1773
754671
 YDOT =      23173
483318  feet/sec       YDOT =        7043
816257  meter/sec
 ZDOT =      -8077
615063                 ZDOT =       -2470
511279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12522793
63                 X    =        -3816947
50
 Y    =       -9222732
70  feet           Y    =        -2811088
93  meter
 Z    =       15884018
06                 Z    =         4841448
71
 XDOT =       5892
869352                 XDOT =        1796
146579
 YDOT =     -21991
796613  feet/sec       YDOT =       -6703
099608  meter/sec
 ZDOT =      -8116
345727                 ZDOT =       -2473
862178


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   18262
54391625  
00016717  00000-0  10270-3 0  9001
2 25544  51
6384 268
4917 0004425 173
8677 186
2530 15
53882239 13184


Satellite: ISS
Catalog Number: 25544
Epoch time:      18262
54391625   =   yrday
fracday
Element set:     900
Inclination:       51
6384  deg
RA of node:       268
4917  deg
Eccentricity:     
0004425     
Arg of perigee:   173
8677  deg
Mean anomaly:     186
2530  deg
Mean motion:   15
53882239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1318
Checksum:              329


Coasting Arc #2 (Orbit 1332)
---------------------------------------

Vector Time (GMT): 2018/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3704618
48                 A    =         6783496
82  meter
 Y    =       -4107284
13  meter          E    =           
0009186
 Z    =       -3937817
59                 I    =           51
25692
 XDOT =       2464
344665                 Wp   =          133
10650
 YDOT =      -6052
114940  meter/sec      RA   =          262
78767  deg
 ZDOT =       3993
923995                 TA   =          178
85576
                                          MA   =          178
85365
                                          Ha   =            222
100  n
mi
                                          Hp   =            214
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12154260
10                 X    =        -3639286
59
 Y    =      -13475341
64  feet           Y    =        -4148346
74  meter
 Z    =      -12919349
05                 Z    =        -3955654
29
 XDOT =       8085
120291                 XDOT =        2512
437642
 YDOT =     -19856
020144  feet/sec       YDOT =       -6024
287735  meter/sec
 ZDOT =      13103
425181                 ZDOT =        4006
012123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11699436
42                 X    =         3565988
22
 Y    =       13797556
86  feet           Y    =         4205495
33  meter
 Z    =      -12998886
99                 Z    =        -3962060
76
 XDOT =      -7525
451801                 XDOT =       -2293
757709
 YDOT =      18778
497036  feet/sec       YDOT =        5723
685897  meter/sec
 ZDOT =      13158
323427                 ZDOT =        4010
656981


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   18263
50860944  
00016717  00000-0  10270-3 0  9014
2 25544  51
6375 263
6853 0004319 176
5026 183
6158 15
53850188 13332


Satellite: ISS
Catalog Number: 25544
Epoch time:      18263
50860944   =   yrday
fracday
Element set:     901
Inclination:       51
6375  deg
RA of node:       263
6853  deg
Eccentricity:     
0004319     
Arg of perigee:   176
5026  deg
Mean anomaly:     183
6158  deg
Mean motion:   15
53850188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1333
Checksum:              320


Coasting Arc #3 (Orbit 1336)
---------------------------------------

Vector Time (GMT): 2018/263/18:05:16
983
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4272663
34                 A    =         6780227
39  meter
 Y    =       -1928501
25  meter          E    =           
0013424
 Z    =       -4910979
81                 I    =           51
24778
 XDOT =        723
609142                 Wp   =          123
46356
 YDOT =      -7289
521251  meter/sec      RA   =          261
52504  deg
 ZDOT =       2230
137104                 TA   =          168
48072
                                          MA   =          168
44997
                                          Ha   =            221
983  n
mi
                                          Hp   =            215
239

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14017924
33                 X    =        -4226925
90
 Y    =       -6327103
82  feet           Y    =        -1976025
77  meter
 Z    =      -16112138
48                 Z    =        -4931623
60
 XDOT =       2374
045743                 XDOT =         794
236028
 YDOT =     -23915
752135  feet/sec       YDOT =       -7281
034283  meter/sec
 ZDOT =       7316
722781                 ZDOT =        2233
824224

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6322958
44                 X    =         1927237
73
 Y    =      -13912920
80  feet           Y    =        -4240658
26  meter
 Z    =      -16204514
29                 Z    =        -4939135
96
 XDOT =      22901
562147                 XDOT =        6980
396142
 YDOT =       1855
130867  feet/sec       YDOT =         565
443888  meter/sec
 ZDOT =       7334
075685                 ZDOT =        2235
426269


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   18263
76586200  
00016717  00000-0  10270-3 0  9023
2 25544  51
6396 262
4037 0003981 188
2178 171
8909 15
53712409 13378


Satellite: ISS
Catalog Number: 25544
Epoch time:      18263
76586200   =   yrday
fracday
Element set:     902
Inclination:       51
6396  deg
RA of node:       262
4037  deg
Eccentricity:     
0003981     
Arg of perigee:   188
2178  deg
Mean anomaly:     171
8909  deg
Mean motion:   15
53712409  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1337
Checksum:              325


Coasting Arc #4 (Orbit 1352)
---------------------------------------

Vector Time (GMT): 2018/264/18:05:16
983
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4198190
23                 A    =         6783295
80  meter
 Y    =        3386561
48  meter          E    =           
0009393
 Z    =        4104241
55                 I    =           51
26352
 XDOT =      -1551
106813                 Wp   =           98
88203
 YDOT =       6499
103223  meter/sec      RA   =          256
51064  deg
 ZDOT =      -3770
057440                 TA   =           30
19446
                                          MA   =           30
14036
                                          Ha   =            221
775  n
mi
                                          Hp   =            215
496

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13773590
01                 X    =         4140072
58
 Y    =       11110766
01  feet           Y    =         3433183
98  meter
 Z    =       13465359
42                 Z    =         4124493
35
 XDOT =      -5088
933115                 XDOT =       -1605
353431
 YDOT =      21322
517135  feet/sec       YDOT =        6481
454012  meter/sec
 ZDOT =     -12368
954857                 ZDOT =       -3777
724500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10869417
37                 X    =        -3312998
41
 Y    =       13877035
74  feet           Y    =         4229720
49  meter
 Z    =       13555827
25                 Z    =         4131816
15
 XDOT =     -20394
429208                 XDOT =       -6216
222023
 YDOT =      -3838
295022  feet/sec       YDOT =       -1169
912323  meter/sec
 ZDOT =     -12404
053621                 ZDOT =       -3780
755544


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   18264
79497072  
00016717  00000-0  10270-3 0  9036
2 25544  51
6391 257
2776 0004020 192
2048 167
9008 15
53711304 13538


Satellite: ISS
Catalog Number: 25544
Epoch time:      18264
79497072   =   yrday
fracday
Element set:     903
Inclination:       51
6391  deg
RA of node:       257
2776  deg
Eccentricity:     
0004020     
Arg of perigee:   192
2048  deg
Mean anomaly:     167
9008  deg
Mean motion:   15
53711304  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1353
Checksum:              308


Coasting Arc #5 (Orbit 1352)
---------------------------------------

Vector Time (GMT): 2018/264/18:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2477813
65                 A    =         6789982
82  meter
 Y    =        6196865
34  meter          E    =           
0015613
 Z    =        1199675
70                 I    =           51
28599
 XDOT =      -4135
538505                 Wp   =          136
33824
 YDOT =       2788
791271  meter/sec      RA   =          256
49029  deg
 ZDOT =      -5829
435782                 TA   =           30
55647
                                          MA   =           30
46560
                                          Ha   =            221
918  n
mi
                                          Hp   =            215
526

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8129309
88                 X    =         2402507
06
 Y    =       20330923
03  feet           Y    =         6224153
01  meter
 Z    =        3935943
91                 Z    =         1211528
54
 XDOT =     -13568
039715                 XDOT =       -4138
099970
 YDOT =       9149
577660  feet/sec       YDOT =        2742
529952  meter/sec
 ZDOT =     -19125
445478                 ZDOT =       -5849
531187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19807820
24                 X    =        -6037423
61
 Y    =        9309480
53  feet           Y    =         2837529
67  meter
 Z    =        3988432
58                 Z    =         1215674
25
 XDOT =      -9260
092576                 XDOT =       -2822
476217
 YDOT =     -11422
453300  feet/sec       YDOT =       -3481
563766  meter/sec
 ZDOT =     -19215
885394                 ZDOT =       -5857
001868


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   18264
79497089  
00016717  00000-0  10270-3 0  9045
2 25544  51
6395 257
2773 0004165 192
3396 167
7655 15
53689889 13534


Satellite: ISS
Catalog Number: 25544
Epoch time:      18264
79497089   =   yrday
fracday
Element set:     904
Inclination:       51
6395  deg
RA of node:       257
2773  deg
Eccentricity:     
0004165     
Arg of perigee:   192
3396  deg
Mean anomaly:     167
7655  deg
Mean motion:   15
53689889  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1353
Checksum:              373


Coasting Arc #6 (Orbit 1368)
---------------------------------------

Vector Time (GMT): 2018/265/18:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1878241
08                 A    =         6790467
79  meter
 Y    =       -6512167
28  meter          E    =           
0009531
 Z    =         356387
72                 I    =           51
29752
 XDOT =       4700
388643                 Wp   =           61
31566
 YDOT =      -1022
646898  meter/sec      RA   =          251
49674  deg
 ZDOT =       5968
321660                 TA   =          302
54248
                                          MA   =          302
63451
                                          Ha   =            221
748  n
mi
                                          Hp   =            215
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6162208
26                 X    =        -1807011
76
 Y    =      -21365378
21  feet           Y    =        -6532772
77  meter
 Z    =        1169251
07                 Z    =          347437
61
 XDOT =      15421
222581                 XDOT =        4682
483933
 YDOT =      -3355
140743  feet/sec       YDOT =        -970
183356  meter/sec
 ZDOT =      19581
107807                 ZDOT =        5991
111080

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20825034
89                 X    =         6347470
64
 Y    =       -7801334
80  feet           Y    =        -2377846
85  meter
 Z    =        1129797
25                 Z    =          344362
20
 XDOT =       3955
634367                 XDOT =        1205
677355
 YDOT =      13467
467568  feet/sec       YDOT =        4104
884115  meter/sec
 ZDOT =      19683
440242                 ZDOT =        5999
512586


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   18265
82407518  
00016717  00000-0  10270-3 0  9059
2 25544  51
6403 252
1495 0003967 198
1651 161
9361 15
53719331 13699


Satellite: ISS
Catalog Number: 25544
Epoch time:      18265
82407518   =   yrday
fracday
Element set:     905
Inclination:       51
6403  deg
RA of node:       252
1495  deg
Eccentricity:     
0003967     
Arg of perigee:   198
1651  deg
Mean anomaly:     161
9361  deg
Mean motion:   15
53719331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1369
Checksum:              322


Coasting Arc #7 (Orbit 1383)
---------------------------------------

Vector Time (GMT): 2018/266/18:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1116986
62                 A    =         6789059
38  meter
 Y    =        6412166
63  meter          E    =           
0009717
 Z    =       -1912562
65                 I    =           51
30395
 XDOT =      -5203
289528                 Wp   =          162
45228
 YDOT =       -753
629333  meter/sec      RA   =          246
50423  deg
 ZDOT =      -5582
038666                 TA   =           38
72315
                                          MA   =           38
65353
                                          Ha   =            221
711  n
mi
                                          Hp   =            215
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3664654
25                 X    =         1054491
20
 Y    =       21037292
10  feet           Y    =         6424307
88  meter
 Z    =       -6274811
84                 Z    =        -1907289
28
 XDOT =     -17071
159870                 XDOT =       -5167
360904
 YDOT =      -2472
537183  feet/sec       YDOT =        -811
615915  meter/sec
 ZDOT =     -18313
775151                 ZDOT =       -5607
227091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20593239
12                 X    =        -6276819
28
 Y    =        5674842
09  feet           Y    =         1729691
87  meter
 Z    =       -6251822
36                 Z    =        -1905555
46
 XDOT =       1277
286176                 XDOT =         389
316826
 YDOT =     -15605
156844  feet/sec       YDOT =       -4756
451806  meter/sec
 ZDOT =     -18426
686069                 ZDOT =       -5616
453914


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   18266
78885976  
00016717  00000-0  10270-3 0  9064
2 25544  51
6402 247
3434 0004091 201
4399 158
6583 15
53691296 13848


Satellite: ISS
Catalog Number: 25544
Epoch time:      18266
78885976   =   yrday
fracday
Element set:     906
Inclination:       51
6402  deg
RA of node:       247
3434  deg
Eccentricity:     
0004091     
Arg of perigee:   201
4399  deg
Mean anomaly:     158
6583  deg
Mean motion:   15
53691296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1384
Checksum:              346


Coasting Arc #8 (Orbit 1388)
---------------------------------------

Vector Time (GMT): 2018/267/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3932681
89                 A    =         6778585
66  meter
 Y    =       -1595252
68  meter          E    =           
0003913
 Z    =        5284668
99                 I    =           51
27055
 XDOT =       3101
498765                 Wp   =          164
59507
 YDOT =       7011
360779  meter/sec      RA   =          244
96742  deg
 ZDOT =       -195
232779                 TA   =          287
25354
                                          MA   =          287
29636
                                          Ha   =            221
693  n
mi
                                          Hp   =            215
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12902499
64                 X    =         3924557
99
 Y    =       -5233768
63  feet           Y    =        -1551319
47  meter
 Z    =       17338152
86                 Z    =         5303753
09
 XDOT =      10175
520881                 XDOT =        3023
813610
 YDOT =      23003
152161  feet/sec       YDOT =        7045
609501  meter/sec
 ZDOT =       -640
527490                 ZDOT =        -180
356309

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9472344
21                 X    =         2887170
51
 Y    =      -10057828
10  feet           Y    =        -3065626
00  meter
 Z    =       17423925
07                 Z    =         5310812
36
 XDOT =      18057
827173                 XDOT =        5504
025722
 YDOT =      16032
158862  feet/sec       YDOT =        4886
602021  meter/sec
 ZDOT =       -574
517039                 ZDOT =        -175
112793


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   18267
11045516  
00016717  00000-0  10270-3 0  9071
2 25544  51
6376 245
7354 0004341 198
6420 161
4574 15
53706611 13896


Satellite: ISS
Catalog Number: 25544
Epoch time:      18267
11045516   =   yrday
fracday
Element set:     907
Inclination:       51
6376  deg
RA of node:       245
7354  deg
Eccentricity:     
0004341     
Arg of perigee:   198
6420  deg
Mean anomaly:     161
4574  deg
Mean motion:   15
53706611  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1389
Checksum:              311


Coasting Arc #9 (Orbit 1403)
---------------------------------------

Vector Time (GMT): 2018/268/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909575
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4583537
77                 A    =         6779749
14  meter
 Y    =          89577
13  meter          E    =           
0013042
 Z    =       -5006385
02                 I    =           51
29041
 XDOT =      -2271
987428                 Wp   =          124
32240
 YDOT =      -7048
336166  meter/sec      RA   =          239
94823  deg
 ZDOT =       1950
411557                 TA   =          164
74699
                                          MA   =          164
70763
                                          Ha   =            221
669  n
mi
                                          Hp   =            215
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15037853
59                 X    =        -4559880
28
 Y    =         293888
22  feet           Y    =           38452
46  meter
 Z    =      -16425147
71                 Z    =        -5028592
93
 XDOT =      -7454
026994                 XDOT =       -2202
476239
 YDOT =     -23124
462487  feet/sec       YDOT =       -7073
354194  meter/sec
 ZDOT =       6398
988048                 ZDOT =        1939
544711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13354141
91                 X    =        -4070342
46
 Y    =        6678875
41  feet           Y    =         2035721
23  meter
 Z    =      -16524781
55                 Z    =        -5036753
42
 XDOT =     -16218
228557                 XDOT =       -4943
316064
 YDOT =     -16685
477367  feet/sec       YDOT =       -5085
733501  meter/sec
 ZDOT =       6350
950265                 ZDOT =        1935
769641


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   18268
07523699  
00016717  00000-0  10270-3 0  9081
2 25544  51
6383 240
9295 0004435 202
7045 157
3912 15
53734483 14045


Satellite: ISS
Catalog Number: 25544
Epoch time:      18268
07523699   =   yrday
fracday
Element set:     908
Inclination:       51
6383  deg
RA of node:       240
9295  deg
Eccentricity:     
0004435     
Arg of perigee:   202
7045  deg
Mean anomaly:     157
3912  deg
Mean motion:   15
53734483  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1404
Checksum:              320


Coasting Arc #10 (Orbit 1410)
---------------------------------------

Vector Time (GMT): 2018/268/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1066274
39                 A    =         6782074
46  meter
 Y    =        5004702
72  meter          E    =           
0007023
 Z    =       -4457063
10                 I    =           51
30420
 XDOT =      -5627
181864                 Wp   =           92
38392
 YDOT =      -4073
333297  meter/sec      RA   =          237
78307  deg
 ZDOT =      -3232
330123                 TA   =          144
91966
                                          MA   =          144
87339
                                          Ha   =            221
505  n
mi
                                          Hp   =            215
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3498275
57                 X    =        -1100508
90
 Y    =       16419628
34  feet           Y    =         4992586
91  meter
 Z    =      -14622910
42                 Z    =        -4462326
52
 XDOT =     -18461
882755                 XDOT =       -5565
513422
 YDOT =     -13363
954386  feet/sec       YDOT =       -4135
915956  meter/sec
 ZDOT =     -10604
757621                 ZDOT =       -3259
514910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2063804
21                 X    =          629047
52
 Y    =      -16639623
18  feet           Y    =        -5071757
14  meter
 Z    =      -14647023
20                 Z    =        -4464412
67
 XDOT =      18196
927074                 XDOT =        5546
423372
 YDOT =      11685
198736  feet/sec       YDOT =        3561
648575  meter/sec
 ZDOT =     -10726
303686                 ZDOT =       -3269
377363


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   18268
52546799  
00016717  00000-0  10270-3 0  9098
2 25544  51
6371 238
6891 0003947 206
3201 153
7751 15
53720964 14117


Satellite: ISS
Catalog Number: 25544
Epoch time:      18268
52546799   =   yrday
fracday
Element set:     909
Inclination:       51
6371  deg
RA of node:       238
6891  deg
Eccentricity:     
0003947     
Arg of perigee:   206
3201  deg
Mean anomaly:     153
7751  deg
Mean motion:   15
53720964  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1411
Checksum:              329


Coasting Arc #11 (Orbit 1426)
---------------------------------------

Vector Time (GMT): 2018/269/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2141542
32                 A    =         6779366
24  meter
 Y    =       -3925331
00  meter          E    =           
0006531
 Z    =        5095401
39                 I    =           51
31485
 XDOT =       5495
534230                 Wp   =          162
21731
 YDOT =       5099
053062  meter/sec      RA   =          232
76984  deg
 ZDOT =       1611
772036                 TA   =          272
12424
                                          MA   =          272
19903
                                          Ha   =            221
282  n
mi
                                          Hp   =            215
970

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7026057
48                 X    =         2160526
23
 Y    =      -12878382
55  feet           Y    =        -3901276
02  meter
 Z    =       16717196
16                 Z    =         5105850
97
 XDOT =      18029
967946                 XDOT =        5430
277531
 YDOT =      16729
176711  feet/sec       YDOT =        5160
143265  meter/sec
 ZDOT =       5287
965998                 ZDOT =        1638
308615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5620877
31                 X    =        -1713243
40
 Y    =       13492272
05  feet           Y    =         4112444
52  meter
 Z    =       16764462
46                 Z    =         5109808
16
 XDOT =     -18561
916386                 XDOT =       -5657
672114
 YDOT =     -14477
678374  feet/sec       YDOT =       -4412
796369  meter/sec
 ZDOT =       5406
516279                 ZDOT =        1647
906162


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   18269
55456496  
00016717  00000-0  10270-3 0  9108
2 25544  51
6380 233
5626 0003928 212
7844 147
3065 15
53746071 14271


Satellite: ISS
Catalog Number: 25544
Epoch time:      18269
55456496   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:       233
5626  deg
Eccentricity:     
0003928     
Arg of perigee:   212
7844  deg
Mean anomaly:     147
3065  deg
Mean motion:   15
53746071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1427
Checksum:              323


Coasting Arc #12 (Orbit 1441)
---------------------------------------

Vector Time (GMT): 2018/270/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3266481
14                 A    =         6778543
76  meter
 Y    =        2708346
45  meter          E    =           
0013069
 Z    =       -5297199
96                 I    =           51
33256
 XDOT =      -5048
421972                 Wp   =          105
39077
 YDOT =      -5756
721649  meter/sec      RA   =          227
75208  deg
 ZDOT =        166
726242                 TA   =          166
22481
                                          MA   =          166
18911
                                          Ha   =            221
264  n
mi
                                          Hp   =            215
932

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10716801
62                 X    =        -3270792
45
 Y    =        8885651
09  feet           Y    =         2671793
70  meter
 Z    =      -17379264
96                 Z    =        -5313078
40
 XDOT =     -16563
064213                 XDOT =       -4984
483381
 YDOT =     -18886
882052  feet/sec       YDOT =       -5812
819086  meter/sec
 ZDOT =        547
002105                 ZDOT =         142
358325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9508947
21                 X    =         2898327
11
 Y    =      -10044605
07  feet           Y    =        -3061595
62  meter
 Z    =      -17450768
32                 Z    =        -5318994
18
 XDOT =      17896
010224                 XDOT =        5454
703916
 YDOT =      16162
946056  feet/sec       YDOT =        4926
465958  meter/sec
 ZDOT =        438
231244                 ZDOT =         133
572883


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   18270
51934317  
00016717  00000-0  10270-3 0  9110
2 25544  51
6377 228
7556 0003846 215
6788 144
4108 15
53723077 14427


Satellite: ISS
Catalog Number: 25544
Epoch time:      18270
51934317   =   yrday
fracday
Element set:     911
Inclination:       51
6377  deg
RA of node:       228
7556  deg
Eccentricity:     
0003846     
Arg of perigee:   215
6788  deg
Mean anomaly:     144
4108  deg
Mean motion:   15
53723077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1442
Checksum:              321


Coasting Arc #13 (Orbit 1450)
---------------------------------------

Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -430685
57                 A    =         6782707
31  meter
 Y    =       -5256865
94  meter          E    =           
0009593
 Z    =        4262430
32                 I    =           51
36102
 XDOT =       6370
000401                 Wp   =          132
74240
 YDOT =       2366
750920  meter/sec      RA   =          225
07434  deg
 ZDOT =       3551
067760                 TA   =          280
83793
                                          MA   =          280
94589
                                          Ha   =            221
322  n
mi
                                          Hp   =            216
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1413010
41                 X    =         -392574
81
 Y    =      -17246935
51  feet           Y    =        -5261468
64  meter
 Z    =       13984351
43                 Z    =         4260431
26
 XDOT =      20898
951448                 XDOT =        6325
811798
 YDOT =       7764
930840  feet/sec       YDOT =        2437
737973  meter/sec
 ZDOT =      11650
484778                 ZDOT =        3581
903955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7724792
17                 X    =        -2354516
65
 Y    =      -15492500
54  feet           Y    =        -4722114
17  meter
 Z    =       13975889
27                 Z    =         4259851
05
 XDOT =      21088
613177                 XDOT =        6427
809296
 YDOT =        153
520138  feet/sec       YDOT =          46
792938  meter/sec
 ZDOT =      11788
612343                 ZDOT =        3593
169042


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   18271
09820811  
00016717  00000-0  10270-3 0  9128
2 25544  51
6398 225
8684 0004391 214
4381 145
6488 15
53760899 14519


Satellite: ISS
Catalog Number: 25544
Epoch time:      18271
09820811   =   yrday
fracday
Element set:     912
Inclination:       51
6398  deg
RA of node:       225
8684  deg
Eccentricity:     
0004391     
Arg of perigee:   214
4381  deg
Mean anomaly:     145
6488  deg
Mean motion:   15
53760899  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1451
Checksum:              331


Coasting Arc #14 (Orbit 1465)
---------------------------------------

Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -878011
67                 A    =         6779829
41  meter
 Y    =        4492005
06  meter          E    =           
0009673
 Z    =       -5010050
46                 I    =           51
37620
 XDOT =      -6547
253246                 Wp   =           91
01206
 YDOT =      -3461
194303  meter/sec      RA   =          220
06645  deg
 ZDOT =      -1959
348683                 TA   =          159
89726
                                          MA   =          159
85914
                                          Ha   =            221
197  n
mi
                                          Hp   =            216
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2880615
73                 X    =         -903840
64
 Y    =       14737549
41  feet           Y    =         4482041
69  meter
 Z    =      -16437173
44                 Z    =        -5014378
72
 XDOT =     -21480
489652                 XDOT =       -6498
544946
 YDOT =     -11355
624353  feet/sec       YDOT =       -3534
138048  meter/sec
 ZDOT =      -6428
309327                 ZDOT =       -1991
034948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3078173
94                 X    =          938227
42
 Y    =       14675324
80  feet           Y    =         4473039
00  meter
 Z    =      -16457024
87                 Z    =        -5016101
18
 XDOT =     -23080
974299                 XDOT =       -7035
080966
 YDOT =      -2513
870143  feet/sec       YDOT =        -766
227619  meter/sec
 ZDOT =      -6570
161494                 ZDOT =       -2002
585223


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   18272
06298336  
00016717  00000-0  10270-3 0  9138
2 25544  51
6407 221
0626 0004327 218
5822 141
5021 15
53733338 14660


Satellite: ISS
Catalog Number: 25544
Epoch time:      18272
06298336   =   yrday
fracday
Element set:     913
Inclination:       51
6407  deg
RA of node:       221
0626  deg
Eccentricity:     
0004327     
Arg of perigee:   218
5822  deg
Mean anomaly:     141
5021  deg
Mean motion:   15
53733338  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1466
Checksum:              292


Coasting Arc #15 (Orbit 1481)
---------------------------------------

Vector Time (GMT): 2018/273/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2236296
25                 A    =         6778385
19  meter
 Y    =       -3594373
07  meter          E    =           
0003625
 Z    =        5294449
29                 I    =           51
39799
 XDOT =       6367
218624                 Wp   =          187
07141
 YDOT =       4267
865930  meter/sec      RA   =          215
05387  deg
 ZDOT =        204
498634                 TA   =          260
95244
                                          MA   =          260
99346
                                          Ha   =            220
966  n
mi
                                          Hp   =            216
225

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7336929
96                 X    =         2250605
23
 Y    =      -11792562
56  feet           Y    =        -3569284
92  meter
 Z    =       17370240
47                 Z    =         5305347
61
 XDOT =      20889
824882                 XDOT =        6318
027571
 YDOT =      14002
184809  feet/sec       YDOT =        4338
793554  meter/sec
 ZDOT =        670
927276                 ZDOT =         235
309168

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1924823
10                 X    =          586686
08
 Y    =      -13692214
61  feet           Y    =        -4173387
01  meter
 Z    =       17419490
29                 Z    =         5309460
64
 XDOT =      23736
237841                 XDOT =        7234
805294
 YDOT =       4380
378426  feet/sec       YDOT =        1335
139344  meter/sec
 ZDOT =        808
791310                 ZDOT =         246
519591


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   18273
09207148  
00016717  00000-0  10270-3 0  9144
2 25544  51
6408 215
9353 0004225 222
9549 137
1274 15
53779261 14826


Satellite: ISS
Catalog Number: 25544
Epoch time:      18273
09207148   =   yrday
fracday
Element set:     914
Inclination:       51
6408  deg
RA of node:       215
9353  deg
Eccentricity:     
0004225     
Arg of perigee:   222
9549  deg
Mean anomaly:     137
1274  deg
Mean motion:   15
53779261  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1482
Checksum:              314


Coasting Arc #16 (Orbit 1496)
---------------------------------------

Vector Time (GMT): 2018/274/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3593731
82                 A    =         6779188
54  meter
 Y    =        2636741
22  meter          E    =           
0011851
 Z    =       -5118199
08                 I    =           51
42788
 XDOT =      -5765
415545                 Wp   =          119
01651
 YDOT =      -4788
662385  meter/sec      RA   =          210
04404  deg
 ZDOT =       1578
341831                 TA   =          166
28219
                                          MA   =          166
24996
                                          Ha   =            220
949  n
mi
                                          Hp   =            216
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11790458
72                 X    =        -3598087
62
 Y    =        8650725
78  feet           Y    =         2596529
03  meter
 Z    =      -16791991
74                 Z    =        -5135667
14
 XDOT =     -18915
405330                 XDOT =       -5719
105758
 YDOT =     -15710
834595  feet/sec       YDOT =       -4852
876256  meter/sec
 ZDOT =       5178
286846                 ZDOT =        1550
447722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7047271
60                 X    =        -2148008
38
 Y    =       12709773
97  feet           Y    =         3873939
11  meter
 Z    =      -16870642
21                 Z    =        -5142171
74
 XDOT =     -22827
832159                 XDOT =       -6957
923242
 YDOT =      -5937
164954  feet/sec       YDOT =       -1809
647878  meter/sec
 ZDOT =       5053
540559                 ZDOT =        1540
319163


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   18274
05684180  
00016717  00000-0  10270-3 0  9157
2 25544  51
6403 211
1302 0004144 225
4101 134
6713 15
53769629 14978


Satellite: ISS
Catalog Number: 25544
Epoch time:      18274
05684180   =   yrday
fracday
Element set:     915
Inclination:       51
6403  deg
RA of node:       211
1302  deg
Eccentricity:     
0004144     
Arg of perigee:   225
4101  deg
Mean anomaly:     134
6713  deg
Mean motion:   15
53769629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1497
Checksum:              289


Coasting Arc #17 (Orbit 1502)
---------------------------------------

Vector Time (GMT): 2018/274/09:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5510002
18                 A    =         6789942
41  meter
 Y    =       -3843129
11  meter          E    =           
0009541
 Z    =         956360
23                 I    =           51
46984
 XDOT =       3452
944623                 Wp   =           58
34851
 YDOT =      -3473
116290  meter/sec      RA   =          208
38598  deg
 ZDOT =       5898
670310                 TA   =          312
03087
                                          MA   =          312
11204
                                          Ha   =            220
862  n
mi
                                          Hp   =            216
273

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18077434
96                 X    =        -5471263
28
 Y    =      -12608691
32  feet           Y    =        -3904529
14  meter
 Z    =        3137664
79                 Z    =          929688
43
 XDOT =      11328
558473                 XDOT =        3462
872325
 YDOT =     -11394
738483  feet/sec       YDOT =       -3434
447320  meter/sec
 ZDOT =      19352
592880                 ZDOT =        5915
467997

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7971144
89                 X    =         2429604
96
 Y    =       20566194
40  feet           Y    =         6268576
05  meter
 Z    =        3018308
93                 Z    =          919980
56
 XDOT =     -14153
501217                 XDOT =       -4313
987171
 YDOT =       2615
085669  feet/sec       YDOT =         797
078112  meter/sec
 ZDOT =      19428
315827                 ZDOT =        5921
750664


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   18274
44274721  
00016717  00000-0  10270-3 0  9167
2 25544  51
6365 209
2100 0003973 227
9168 132
1647 15
53794538 15032


Satellite: ISS
Catalog Number: 25544
Epoch time:      18274
44274721   =   yrday
fracday
Element set:     916
Inclination:       51
6365  deg
RA of node:       209
2100  deg
Eccentricity:     
0003973     
Arg of perigee:   227
9168  deg
Mean anomaly:     132
1647  deg
Mean motion:   15
53794538  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1503
Checksum:              313


Coasting Arc #18 (Orbit 1517)
---------------------------------------

Vector Time (GMT): 2018/275/09:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4729817
88                 A    =         6787896
23  meter
 Y    =        4189640
82  meter          E    =           
0005924
 Z    =       -2471332
20                 I    =           51
49304
 XDOT =      -4951
257125                 Wp   =          171
07045
 YDOT =       2461
330206  meter/sec      RA   =          203
40333  deg
 ZDOT =      -5310
839310                 TA   =           36
67077
                                          MA   =           36
63025
                                          Ha   =            220
795  n
mi
                                          Hp   =            216
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15517775
19                 X    =         4694621
16
 Y    =       13745540
75  feet           Y    =         4242336
04  meter
 Z    =       -8108045
26                 Z    =        -2448441
80
 XDOT =     -16244
281906                 XDOT =       -4952
614916
 YDOT =       8075
230336  feet/sec       YDOT =        2405
954034  meter/sec
 ZDOT =     -17424
013484                 ZDOT =       -5334
894409

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5585550
60                 X    =        -1702475
82
 Y    =      -20004809
69  feet           Y    =        -6097465
99  meter
 Z    =       -8005676
05                 Z    =        -2440130
06
 XDOT =      16465
990607                 XDOT =        5018
833937
 YDOT =       2408
808113  feet/sec       YDOT =         734
204713  meter/sec
 ZDOT =     -17532
230104                 ZDOT =       -5343
823736


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   18275
40751491  
00016717  00000-0  10270-3 0  9179
2 25544  51
6374 204
4026 0003765 235
0059 125
0740 15
53752627 15188


Satellite: ISS
Catalog Number: 25544
Epoch time:      18275
40751491   =   yrday
fracday
Element set:     917
Inclination:       51
6374  deg
RA of node:       204
4026  deg
Eccentricity:     
0003765     
Arg of perigee:   235
0059  deg
Mean anomaly:     125
0740  deg
Mean motion:   15
53752627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1518
Checksum:              301


Coasting Arc #19 (Orbit 1533)
---------------------------------------

Vector Time (GMT): 2018/276/09:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943654
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3620411
48                 A    =         6784459
84  meter
 Y    =       -4343520
60  meter          E    =           
0008871
 Z    =        3744681
20                 I    =           51
51290
 XDOT =       6203
656227                 Wp   =          111
29352
 YDOT =      -1496
407205  meter/sec      RA   =          198
41676  deg
 ZDOT =       4250
787423                 TA   =          293
56786
                                          MA   =          293
66101
                                          Ha   =            220
631  n
mi
                                          Hp   =            216
450

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11877990
43                 X    =        -3589761
74
 Y    =      -14250395
67  feet           Y    =        -4383835
02  meter
 Z    =       12285699
49                 Z    =         3727169
04
 XDOT =      20353
202844                 XDOT =        6199
280204
 YDOT =      -4909
472458  feet/sec       YDOT =       -1427
057903  meter/sec
 ZDOT =      13946
152963                 ZDOT =        4280
912229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2597834
90                 X    =          791820
08
 Y    =       18420850
34  feet           Y    =         5614675
18  meter
 Z    =       12207471
98                 Z    =         3720837
46
 XDOT =     -18441
689204                 XDOT =       -5621
026869
 YDOT =      -6755
746716  feet/sec       YDOT =       -2059
151599  meter/sec
 ZDOT =      14081
546467                 ZDOT =        4292
055363


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   18276
43659295  
00016717  00000-0  10270-3 0  9183
2 25544  51
6376 199
2760 0003898 239
2429 120
8340 15
53785406 15348


Satellite: ISS
Catalog Number: 25544
Epoch time:      18276
43659295   =   yrday
fracday
Element set:     918
Inclination:       51
6376  deg
RA of node:       199
2760  deg
Eccentricity:     
0003898     
Arg of perigee:   239
2429  deg
Mean anomaly:     120
8340  deg
Mean motion:   15
53785406  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1534
Checksum:              345


Coasting Arc #20 (Orbit 1548)
---------------------------------------

Vector Time (GMT): 2018/277/08:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928546
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1856125
33                 A    =         6780532
11  meter
 Y    =       -4390160
06  meter          E    =           
0005995
 Z    =        4822192
51                 I    =           51
52970
 XDOT =       7239
907829                 Wp   =          151
81513
 YDOT =       -300
448733  meter/sec      RA   =          193
57869  deg
 ZDOT =       2506
753608                 TA   =          273
46895
                                          MA   =          273
53753
                                          Ha   =            220
517  n
mi
                                          Hp   =            216
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6089650
04                 X    =        -1830319
12
 Y    =      -14403412
28  feet           Y    =        -4410771
97  meter
 Z    =       15820841
58                 Z    =         4813239
02
 XDOT =      23752
978443                 XDOT =        7230
552925
 YDOT =       -985
724188  feet/sec       YDOT =        -219
539217  meter/sec
 ZDOT =       8224
257244                 ZDOT =        2541
899958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5136831
60                 X    =        -1565706
27
 Y    =       14812597
79  feet           Y    =         4514879
81  meter
 Z    =       15781034
79                 Z    =         4810059
40
 XDOT =     -17083
983313                 XDOT =       -5207
198114
 YDOT =     -14877
252309  feet/sec       YDOT =       -4534
586504  meter/sec
 ZDOT =       8382
108512                 ZDOT =        2554
866675


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   18277
40135254  
00016717  00000-0  10270-3 0  9196
2 25544  51
6369 194
4693 0003887 244
3754 115
6997 15
53779960 15492


Satellite: ISS
Catalog Number: 25544
Epoch time:      18277
40135254   =   yrday
fracday
Element set:     919
Inclination:       51
6369  deg
RA of node:       194
4693  deg
Eccentricity:     
0003887     
Arg of perigee:   244
3754  deg
Mean anomaly:     115
6997  deg
Mean motion:   15
53779960  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1549
Checksum:              362
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