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

 
Date: November 29th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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


334/13:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 214 6

340/13:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 215 1

341/18:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 215 2

342/18:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 215 4

344/22:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 215 4

348/01:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 215 5

348/05:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 6

Coasting Arc #1 (Orbit 748)
---------------------------------------

Vector Time (GMT): 2017/333/16:38:16
467
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3250065
88                 A    =         6778064
93  meter
 Y    =        2958894
78  meter          E    =           
0003455
 Z    =        5156786
18                 I    =           51
27771
 XDOT =      -3837
719457                 Wp   =          101
47276
 YDOT =       6510
452899  meter/sec      RA   =          292
48730  deg
 ZDOT =      -1316
811674                 TA   =            1
23778
                                          MA   =            1
23692
                                          Ha   =            221
216  n
mi
                                          Hp   =            214
719

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10662945
79                 X    =         3191687
57
 Y    =        9707660
04  feet           Y    =         2994912
73  meter
 Z    =       16918589
82                 Z    =         5172432
55
 XDOT =     -12590
943101                 XDOT =       -3903
839313
 YDOT =      21359
753605  feet/sec       YDOT =        6467
167223  meter/sec
 ZDOT =      -4320
248275                 ZDOT =       -1335
614948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1208691
26                 X    =          368409
10
 Y    =       14287763
62  feet           Y    =         4354910
35  meter
 Z    =       16987484
64                 Z    =         5177785
32
 XDOT =     -22655
937021                 XDOT =       -6905
529604
 YDOT =       7153
912973  feet/sec       YDOT =        2180
512674  meter/sec
 ZDOT =      -4404
725695                 ZDOT =       -1342
560392


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   17333
73918845  
00016717  00000-0  10270-3 0  9009
2 25544  51
6421 293
0212 0003179 183
3839 176
7293 15
54085708  7493


Satellite: ISS
Catalog Number: 25544
Epoch time:      17333
73918845   =   yrday
fracday
Element set:     900
Inclination:       51
6421  deg
RA of node:       293
0212  deg
Eccentricity:     
0003179     
Arg of perigee:   183
3839  deg
Mean anomaly:     176
7293  deg
Mean motion:   15
54085708  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             749
Checksum:              326


Coasting Arc #2 (Orbit 761)
---------------------------------------

Vector Time (GMT): 2017/334/13:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4047735
48                 A    =         6777610
02  meter
 Y    =       -1286879
91  meter          E    =           
0014983
 Z    =       -5294377
03                 I    =           51
26307
 XDOT =       2359
210895                 Wp   =          101
83935
 YDOT =      -7285
066460  meter/sec      RA   =          288
16055  deg
 ZDOT =        -36
055982                 TA   =          167
83291
                                          MA   =          167
79668
                                          Ha   =            221
382  n
mi
                                          Hp   =            214
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13279972
03                 X    =        -4007326
37
 Y    =       -4222046
96  feet           Y    =        -1331918
35  meter
 Z    =      -17370003
39                 Z    =        -5313941
99
 XDOT =       7740
193225                 XDOT =        2440
674264
 YDOT =     -23901
136681  feet/sec       YDOT =       -7258
228661  meter/sec
 ZDOT =       -118
293904                 ZDOT =         -24
397781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4225991
96                 X    =         1288082
35
 Y    =      -13164724
54  feet           Y    =        -4012608
04  meter
 Z    =      -17456556
79                 Z    =        -5320758
51
 XDOT =      22939
708258                 XDOT =        6992
023077
 YDOT =       7437
106417  feet/sec       YDOT =        2266
830036  meter/sec
 ZDOT =        -65
383570                 ZDOT =         -19
928912


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   17334
57516154  
00016717  00000-0  10270-3 0  9010
2 25544  51
6397 288
8530 0003160 184
0271 176
0857 15
54041882  7627


Satellite: ISS
Catalog Number: 25544
Epoch time:      17334
57516154   =   yrday
fracday
Element set:     901
Inclination:       51
6397  deg
RA of node:       288
8530  deg
Eccentricity:     
0003160     
Arg of perigee:   184
0271  deg
Mean anomaly:     176
0857  deg
Mean motion:   15
54041882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             762
Checksum:              311


Coasting Arc #3 (Orbit 777)
---------------------------------------

Vector Time (GMT): 2017/335/13:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3452766
59                 A    =         6778711
15  meter
 Y    =        2953076
07  meter          E    =           
0004103
 Z    =        5027213
88                 I    =           51
25827
 XDOT =      -3100
603788                 Wp   =           89
63836
 YDOT =       6769
586516  meter/sec      RA   =          283
13678  deg
 ZDOT =      -1845
701332                 TA   =           18
33623
                                          MA   =           18
32144
                                          Ha   =            221
150  n
mi
                                          Hp   =            214
886

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11327974
38                 X    =         3395067
58
 Y    =        9688569
79  feet           Y    =         2991364
38  meter
 Z    =       16493483
86                 Z    =         5043846
76
 XDOT =     -10172
584607                 XDOT =       -3167
106953
 YDOT =      22209
929516  feet/sec       YDOT =        6734
541703  meter/sec
 ZDOT =      -6055
450564                 ZDOT =       -1860
924627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9497688
58                 X    =        -2894895
48
 Y    =       11382561
73  feet           Y    =         3469404
82  meter
 Z    =       16566761
85                 Z    =         5049549
01
 XDOT =     -21548
563197                 XDOT =       -6568
002062
 YDOT =      -9060
631534  feet/sec       YDOT =       -2761
680492  meter/sec
 ZDOT =      -6124
078297                 ZDOT =       -1866
619065


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   17335
60404517  
00016717  00000-0  10270-3 0  9025
2 25544  51
6403 283
7256 0003167 189
1906 170
9189 15
54055462  7789


Satellite: ISS
Catalog Number: 25544
Epoch time:      17335
60404517   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:       283
7256  deg
Eccentricity:     
0003167     
Arg of perigee:   189
1906  deg
Mean anomaly:     170
9189  deg
Mean motion:   15
54055462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             778
Checksum:              318


Coasting Arc #4 (Orbit 792)
---------------------------------------

Vector Time (GMT): 2017/336/13:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2819638
11                 A    =         6781733
72  meter
 Y    =       -4464745
30  meter          E    =           
0009317
 Z    =       -4265349
37                 I    =           51
26280
 XDOT =       3682
292560                 Wp   =          129
61885
 YDOT =      -5707
701091  meter/sec      RA   =          278
11626  deg
 ZDOT =       3539
668220                 TA   =          176
71605
                                          MA   =          176
70993
                                          Ha   =            221
197  n
mi
                                          Hp   =            214
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9250781
19                 X    =        -2748783
11
 Y    =      -14648114
51  feet           Y    =        -4495879
91  meter
 Z    =      -13993928
38                 Z    =        -4278874
87
 XDOT =      12081
012336                 XDOT =        3728
649558
 YDOT =     -18726
053449  feet/sec       YDOT =       -5666
264265  meter/sec
 ZDOT =      11613
084712                 ZDOT =        3557
668211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14327417
88                 X    =         4366996
97
 Y    =       -9654396
35  feet           Y    =        -2942660
01  meter
 Z    =      -14053183
66                 Z    =        -4283410
38
 XDOT =      18420
763850                 XDOT =        5614
648821
 YDOT =      10312
015874  feet/sec       YDOT =        3143
102438  meter/sec
 ZDOT =      11693
848110                 ZDOT =        3564
284904


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   17336
56861697  
00016717  00000-0  10270-3 0  9038
2 25544  51
6411 278
9168 0003131 192
1153 167
9925 15
54070329  7935


Satellite: ISS
Catalog Number: 25544
Epoch time:      17336
56861697   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:       278
9168  deg
Eccentricity:     
0003131     
Arg of perigee:   192
1153  deg
Mean anomaly:     167
9925  deg
Mean motion:   15
54070329  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             793
Checksum:              327


Coasting Arc #5 (Orbit 808)
---------------------------------------

Vector Time (GMT): 2017/337/13:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2139307
77                 A    =         6785532
45  meter
 Y    =        5664654
91  meter          E    =           
0012919
 Z    =        3046529
49                 I    =           51
27189
 XDOT =      -4155
421158                 Wp   =          109
57446
 YDOT =       4205
934135  meter/sec      RA   =          273
10693  deg
 ZDOT =      -4889
730354                 TA   =           35
24708
                                          MA   =           35
16172
                                          Ha   =            221
068  n
mi
                                          Hp   =            214
979

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7018726
27                 X    =         2061006
24
 Y    =       18584825
82  feet           Y    =         5688139
98  meter
 Z    =        9995175
50                 Z    =         3056732
20
 XDOT =     -13633
271515                 XDOT =       -4178
391819
 YDOT =      13798
996506  feet/sec       YDOT =        4159
337450  meter/sec
 ZDOT =     -16042
422421                 ZDOT =       -4909
971860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18203765
02                 X    =        -5548507
58
 Y    =        7898925
98  feet           Y    =         2407592
64  meter
 Z    =       10039507
44                 Z    =         3060041
87
 XDOT =     -13898
652672                 XDOT =       -4236
309334
 YDOT =     -11473
041333  feet/sec       YDOT =       -3496
982998  meter/sec
 ZDOT =     -16132
881627                 ZDOT =       -4917
302320


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   17337
59748847  
00016717  00000-0  10270-3 0  9044
2 25544  51
6411 273
7892 0003095 195
3300 164
7760 15
54068253  8093


Satellite: ISS
Catalog Number: 25544
Epoch time:      17337
59748847   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:       273
7892  deg
Eccentricity:     
0003095     
Arg of perigee:   195
3300  deg
Mean anomaly:     164
7760  deg
Mean motion:   15
54068253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             809
Checksum:              331


Coasting Arc #6 (Orbit 823)
---------------------------------------

Vector Time (GMT): 2017/338/13:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1446440
76                 A    =         6788445
51  meter
 Y    =       -6450318
17  meter          E    =           
0005225
 Z    =       -1537372
74                 I    =           51
28116
 XDOT =       4512
349519                 Wp   =           47
71380
 YDOT =      -2372
140335  meter/sec      RA   =          268
10630  deg
 ZDOT =       5723
244438                 TA   =          295
40870
                                          MA   =          295
46277
                                          Ha   =            221
004  n
mi
                                          Hp   =            215
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4745540
56                 X    =        -1366736
17
 Y    =      -21162461
17  feet           Y    =        -6466047
42  meter
 Z    =       -5043873
82                 Z    =        -1544206
38
 XDOT =      14804
296321                 XDOT =        4510
738955
 YDOT =      -7782
612647  feet/sec       YDOT =       -2321
689846  meter/sec
 ZDOT =      18777
048682                 ZDOT =        5745
160153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20789977
36                 X    =         6336785
10
 Y    =       -6152283
82  feet           Y    =        -1875216
11  meter
 Z    =       -5073147
59                 Z    =        -1546295
38
 XDOT =       8320
662160                 XDOT =        2536
137827
 YDOT =      12596
421024  feet/sec       YDOT =        3839
389128  meter/sec
 ZDOT =      18874
640256                 ZDOT =        5752
990350


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   17338
56205064  
00016717  00000-0  10270-3 0  9052
2 25544  51
6413 268
9815 0003135 200
8273 159
2753 15
54082036  8245


Satellite: ISS
Catalog Number: 25544
Epoch time:      17338
56205064   =   yrday
fracday
Element set:     905
Inclination:       51
6413  deg
RA of node:       268
9815  deg
Eccentricity:     
0003135     
Arg of perigee:   200
8273  deg
Mean anomaly:     159
2753  deg
Mean motion:   15
54082036  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             824
Checksum:              301


Coasting Arc #7 (Orbit 839)
---------------------------------------

Vector Time (GMT): 2017/339/13:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 933812
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         685035
65                 A    =         6789488
30  meter
 Y    =        6745291
00  meter          E    =           
0013320
 Z    =        -160804
47                 I    =           51
28737
 XDOT =      -4787
948909                 Wp   =          148
81403
 YDOT =        349
204159  meter/sec      RA   =          263
11181  deg
 ZDOT =      -5982
773914                 TA   =           32
92729
                                          MA   =           32
84439
                                          Ha   =            220
934  n
mi
                                          Hp   =            215
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2247492
28                 X    =          610338
20
 Y    =       22130219
83  feet           Y    =         6752533
90  meter
 Z    =        -527573
73                 Z    =         -157657
38
 XDOT =     -15708
493797                 XDOT =       -4762
436352
 YDOT =       1145
682937  feet/sec       YDOT =         295
805410  meter/sec
 ZDOT =     -19628
523339                 ZDOT =       -6005
970460

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21855777
73                 X    =        -6661641
05
 Y    =        4139597
04  feet           Y    =         1261749
18  meter
 Z    =        -514685
47                 Z    =         -156876
13
 XDOT =      -2173
333405                 XDOT =        -662
432022
 YDOT =     -13829
947086  feet/sec       YDOT =       -4215
367872  meter/sec
 ZDOT =     -19731
480109                 ZDOT =       -6014
155137


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   17339
59091108  
00016717  00000-0  10270-3 0  9069
2 25544  51
6420 263
8534 0003215 204
2909 155
8092 15
54070917  8409


Satellite: ISS
Catalog Number: 25544
Epoch time:      17339
59091108   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       263
8534  deg
Eccentricity:     
0003215     
Arg of perigee:   204
2909  deg
Mean anomaly:     155
8092  deg
Mean motion:   15
54070917  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             840
Checksum:              302


Coasting Arc #8 (Orbit 854)
---------------------------------------

Vector Time (GMT): 2017/340/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3666662
11                 A    =         6784761
62  meter
 Y    =       -4680043
69  meter          E    =           
0003933
 Z    =       -3274204
68                 I    =           51
27671
 XDOT =       2712
086703                 Wp   =          124
88270
 YDOT =      -5410
613017  meter/sec      RA   =          258
12686  deg
 ZDOT =       4698
409898                 TA   =          196
92355
                                          MA   =          196
93667
                                          Ha   =            220
808  n
mi
                                          Hp   =            215
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12029731
35                 X    =        -3598151
58
 Y    =      -15354474
05  feet           Y    =        -4720663
39  meter
 Z    =      -10742141
33                 Z    =        -3291850
33
 XDOT =       8897
922253                 XDOT =        2749
565438
 YDOT =     -17751
355044  feet/sec       YDOT =       -5380
075561  meter/sec
 ZDOT =      15414
730636                 ZDOT =        4711
674855

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14897544
13                 X    =         4540771
45
 Y    =      -12524589
21  feet           Y    =        -3817494
79  meter
 Z    =      -10819692
87                 Z    =        -3297842
39
 XDOT =      17153
191574                 XDOT =        5228
292792
 YDOT =       7040
228674  feet/sec       YDOT =        2145
861700  meter/sec
 ZDOT =      15474
428655                 ZDOT =        4716
605854


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   17340
55546129  
00016717  00000-0  10270-3 0  9076
2 25544  51
6418 259
0454 0003038 207
8401 152
2590 15
54114218  8556


Satellite: ISS
Catalog Number: 25544
Epoch time:      17340
55546129   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:       259
0454  deg
Eccentricity:     
0003038     
Arg of perigee:   207
8401  deg
Mean anomaly:     152
2590  deg
Mean motion:   15
54114218  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             855
Checksum:              296


Coasting Arc #9 (Orbit 870)
---------------------------------------

Vector Time (GMT): 2017/341/13:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3212901
17                 A    =         6788101
41  meter
 Y    =        5701660
94  meter          E    =           
0013965
 Z    =        1771616
57                 I    =           51
29427
 XDOT =      -3577
491083                 Wp   =          127
52007
 YDOT =       3775
240834  meter/sec      RA   =          253
12656  deg
 ZDOT =      -5639
814580                 TA   =           32
91738
                                          MA   =           32
83049
                                          Ha   =            220
749  n
mi
                                          Hp   =            215
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10541014
33                 X    =         3140299
24
 Y    =       18706236
68  feet           Y    =         5737183
70  meter
 Z    =        5812390
32                 Z    =         1787048
00
 XDOT =     -11737
175469                 XDOT =       -3592
045525
 YDOT =      12385
960741  feet/sec       YDOT =        3735
153998  meter/sec
 ZDOT =     -18503
328674                 ZDOT =       -5657
227930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18105716
21                 X    =        -5518622
30
 Y    =       11507781
67  feet           Y    =         3507571
85  meter
 Z    =        5879979
29                 Z    =         1792217
69
 XDOT =     -12160
622905                 XDOT =       -3706
557862
 YDOT =      -9601
804318  feet/sec       YDOT =       -2926
629956  meter/sec
 ZDOT =     -18581
172535                 ZDOT =       -5663
541389


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   17341
58431155  
00016717  00000-0  10270-3 0  9083
2 25544  51
6409 253
9179 0003141 210
8032 149
2937 15
54083451  8715


Satellite: ISS
Catalog Number: 25544
Epoch time:      17341
58431155   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       253
9179  deg
Eccentricity:     
0003141     
Arg of perigee:   210
8032  deg
Mean anomaly:     149
2937  deg
Mean motion:   15
54083451  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             871
Checksum:              302


Coasting Arc #10 (Orbit 873)
---------------------------------------

Vector Time (GMT): 2017/341/18:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1562056
15                 A    =         6782891
54  meter
 Y    =        5332132
12  meter          E    =           
0004677
 Z    =       -3893750
18                 I    =           51
27512
 XDOT =      -4820
972298                 Wp   =          101
29644
 YDOT =      -4367
422294  meter/sec      RA   =          252
13804  deg
 ZDOT =      -4051
802879                 TA   =          126
06279
                                          MA   =          126
01946
                                          Ha   =            220
689  n
mi
                                          Hp   =            215
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5124856
13                 X    =        -1602651
48
 Y    =       17493871
78  feet           Y    =         5314437
48  meter
 Z    =      -12774770
94                 Z    =        -3901436
32
 XDOT =     -15816
838248                 XDOT =       -4752
094661
 YDOT =     -14328
813301  feet/sec       YDOT =       -4420
948246  meter/sec
 ZDOT =     -13293
316531                 ZDOT =       -4075
054711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8824276
37                 X    =        -2689639
44
 Y    =       15922888
04  feet           Y    =         4853296
27  meter
 Z    =      -12809693
82                 Z    =        -3904394
68
 XDOT =     -10965
781249                 XDOT =       -3342
370125
 YDOT =     -16840
518392  feet/sec       YDOT =       -5132
990006  meter/sec
 ZDOT =     -13395
814005                 ZDOT =       -4083
044109


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   17341
77721835  
00016717  00000-0  10270-3 0  9092
2 25544  51
6369 252
9524 0003158 211
7956 148
3006 15
54120291  8740


Satellite: ISS
Catalog Number: 25544
Epoch time:      17341
77721835   =   yrday
fracday
Element set:     909
Inclination:       51
6369  deg
RA of node:       252
9524  deg
Eccentricity:     
0003158     
Arg of perigee:   211
7956  deg
Mean anomaly:     148
3006  deg
Mean motion:   15
54120291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             874
Checksum:              316


Coasting Arc #11 (Orbit 889)
---------------------------------------

Vector Time (GMT): 2017/342/18:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2482263
82                 A    =         6779476
02  meter
 Y    =       -4065230
34  meter          E    =           
0007411
 Z    =        4823015
83                 I    =           51
27467
 XDOT =       4530
075528                 Wp   =          145
61013
 YDOT =       5682
126809  meter/sec      RA   =          247
12139  deg
 ZDOT =       2450
001662                 TA   =          280
17441
                                          MA   =          280
25799
                                          Ha   =            220
574  n
mi
                                          Hp   =            215
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8143910
18                 X    =         2504110
03
 Y    =      -13337369
89  feet           Y    =        -4037350
12  meter
 Z    =       15823542
75                 Z    =         4835126
69
 XDOT =      14862
452519                 XDOT =        4454
298891
 YDOT =      18642
148323  feet/sec       YDOT =        5732
361365  meter/sec
 ZDOT =       8038
063196                 ZDOT =        2471
823635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10623624
23                 X    =         3238080
67
 Y    =      -11385261
96  feet           Y    =        -3470227
85  meter
 Z    =       15877897
59                 Z    =         4839583
19
 XDOT =       9803
844853                 XDOT =        2988
211911
 YDOT =      20527
580941  feet/sec       YDOT =        6256
806671  meter/sec
 ZDOT =       8134
037225                 ZDOT =        2479
254546


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   17342
80606201  
00016717  00000-0  10270-3 0  9108
2 25544  51
6370 247
8229 0003215 217
7128 142
3799 15
54099423  8901


Satellite: ISS
Catalog Number: 25544
Epoch time:      17342
80606201   =   yrday
fracday
Element set:     910
Inclination:       51
6370  deg
RA of node:       247
8229  deg
Eccentricity:     
0003215     
Arg of perigee:   217
7128  deg
Mean anomaly:     142
3799  deg
Mean motion:   15
54099423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             890
Checksum:              303


Coasting Arc #12 (Orbit 889)
---------------------------------------

Vector Time (GMT): 2017/342/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4715103
63                 A    =         6781189
97  meter
 Y    =        2138768
08  meter          E    =           
0006878
 Z    =        4373566
13                 I    =           51
28066
 XDOT =         -4
449274                 Wp   =           86
31633
 YDOT =       6895
011227  meter/sec      RA   =          247
02584  deg
 ZDOT =      -3361
994743                 TA   =           37
88345
                                          MA   =           37
83507
                                          Ha   =            220
533  n
mi
                                          Hp   =            215
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15469500
09                 X    =         4669592
31
 Y    =        7016955
63  feet           Y    =         2191240
85  meter
 Z    =       14348970
26                 Z    =         4396360
20
 XDOT =        -14
597355                 XDOT =         -65
219914
 YDOT =      22621
427911  feet/sec       YDOT =        6894
621891  meter/sec
 ZDOT =     -11030
166479                 ZDOT =       -3362
163531

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14220778
27                 X    =         4334493
22
 Y    =        9132851
78  feet           Y    =         2783693
22  meter
 Z    =       14449793
45                 Z    =         4404297
04
 XDOT =      -2492
804296                 XDOT =        -759
806749
 YDOT =      21361
928680  feet/sec       YDOT =        6511
115862  meter/sec
 ZDOT =     -11031
956978                 ZDOT =       -3362
540487


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   17342
80606173  
00016717  00000-0  10270-3 0  9117
2 25544  51
6371 247
8226 0003340 215
9329 144
1599 15
54095378  8904


Satellite: ISS
Catalog Number: 25544
Epoch time:      17342
80606173   =   yrday
fracday
Element set:     911
Inclination:       51
6371  deg
RA of node:       247
8226  deg
Eccentricity:     
0003340     
Arg of perigee:   215
9329  deg
Mean anomaly:     144
1599  deg
Mean motion:   15
54095378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             890
Checksum:              315


Coasting Arc #13 (Orbit 904)
---------------------------------------

Vector Time (GMT): 2017/343/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919378
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4803450
00                 A    =         6784886
44  meter
 Y    =       -3563139
26  meter          E    =           
0003313
 Z    =       -3208569
19                 I    =           51
30749
 XDOT =       1188
555930                 Wp   =          126
73009
 YDOT =      -5886
412321  meter/sec      RA   =          242
01547  deg
 ZDOT =       4759
032706                 TA   =          195
99136
                                          MA   =          196
00182
                                          Ha   =            220
633  n
mi
                                          Hp   =            215
234

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15759350
39                 X    =        -4747663
37
 Y    =      -11690089
42  feet           Y    =        -3616542
65  meter
 Z    =      -10526801
81                 Z    =        -3231767
53
 XDOT =       3899
461714                 XDOT =        1231
173994
 YDOT =     -19312
376380  feet/sec       YDOT =       -5872
883005  meter/sec
 ZDOT =      15613
624364                 ZDOT =        4764
909581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14103563
24                 X    =        -4298766
07
 Y    =      -13562376
40  feet           Y    =        -4133812
33  meter
 Z    =      -10629220
22                 Z    =        -3239786
32
 XDOT =       5194
265369                 XDOT =        1583
212084
 YDOT =     -17655
733769  feet/sec       YDOT =       -5381
467653  meter/sec
 ZDOT =      15640
579395                 ZDOT =        4767
248600


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   17343
77059780  
00016717  00000-0  10270-3 0  9121
2 25544  51
6375 243
0137 0003243 215
5933 144
5003 15
54126440  9052


Satellite: ISS
Catalog Number: 25544
Epoch time:      17343
77059780   =   yrday
fracday
Element set:     912
Inclination:       51
6375  deg
RA of node:       243
0137  deg
Eccentricity:     
0003243     
Arg of perigee:   215
5933  deg
Mean anomaly:     144
5003  deg
Mean motion:   15
54126440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             905
Checksum:              287


Coasting Arc #14 (Orbit 920)
---------------------------------------

Vector Time (GMT): 2017/344/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4630894
39                 A    =         6788054
68  meter
 Y    =        4656595
39  meter          E    =           
0013354
 Z    =        1686522
04                 I    =           51
33331
 XDOT =      -2477
014915                 Wp   =          129
34911
 YDOT =       4527
178747  meter/sec      RA   =          237
01711  deg
 ZDOT =      -5676
534637                 TA   =           32
07454
                                          MA   =           31
99335
                                          Ha   =            220
406  n
mi
                                          Hp   =            215
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15193223
07                 X    =         4570286
60
 Y    =       15277543
94  feet           Y    =         4708042
28  meter
 Z    =        5533208
79                 Z    =         1708870
52
 XDOT =      -8126
689355                 XDOT =       -2499
881057
 YDOT =      14852
948646  feet/sec       YDOT =        4499
351441  meter/sec
 ZDOT =     -18623
801301                 ZDOT =       -5688
622601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13417051
12                 X    =         4089517
18
 Y    =       16826180
61  feet           Y    =         5128619
85  meter
 Z    =        5631710
28                 Z    =         1716545
29
 XDOT =      -8334
813160                 XDOT =       -2540
451051
 YDOT =      12921
228215  feet/sec       YDOT =        3938
390360  meter/sec
 ZDOT =     -18678
111960                 ZDOT =       -5693
088525


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   17344
79943165  
00016717  00000-0  10270-3 0  9134
2 25544  51
6365 237
8851 0003293 222
6332 137
4566 15
54138173  9211


Satellite: ISS
Catalog Number: 25544
Epoch time:      17344
79943165   =   yrday
fracday
Element set:     913
Inclination:       51
6365  deg
RA of node:       237
8851  deg
Eccentricity:     
0003293     
Arg of perigee:   222
6332  deg
Mean anomaly:     137
4566  deg
Mean motion:   15
54138173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             921
Checksum:              319


Coasting Arc #15 (Orbit 923)
---------------------------------------

Vector Time (GMT): 2017/344/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         564433
84                 A    =         6781588
91  meter
 Y    =       -5259274
38  meter          E    =           
0009083
 Z    =        4241192
86                 I    =           51
31930
 XDOT =       5801
067854                 Wp   =          126
84125
 YDOT =       3515
714662  meter/sec      RA   =          236
18949  deg
 ZDOT =       3576
942337                 TA   =          286
41704
                                          MA   =          286
51686
                                          Ha   =            220
431  n
mi
                                          Hp   =            215
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1851817
07                 X    =          602600
81
 Y    =      -17254837
20  feet           Y    =        -5252749
25  meter
 Z    =       13914674
73                 Z    =         4244027
21
 XDOT =      19032
374850                 XDOT =        5743
947958
 YDOT =      11534
496923  feet/sec       YDOT =        3580
266656  meter/sec
 ZDOT =      11735
375121                 ZDOT =        3604
983612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13409964
77                 X    =        -4087357
26
 Y    =      -10998173
59  feet           Y    =        -3352243
31  meter
 Z    =       13928023
15                 Z    =         4245261
45
 XDOT =      19284
337763                 XDOT =        5877
866150
 YDOT =      -8450
317852  feet/sec       YDOT =       -2575
656881  meter/sec
 ZDOT =      11859
311509                 ZDOT =        3614
718148


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   17344
99233670  
00016717  00000-0  10270-3 0  9140
2 25544  51
6409 236
9249 0003494 221
9389 138
1497 15
54161806  9241


Satellite: ISS
Catalog Number: 25544
Epoch time:      17344
99233670   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:       236
9249  deg
Eccentricity:     
0003494     
Arg of perigee:   221
9389  deg
Mean anomaly:     138
1497  deg
Mean motion:   15
54161806  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             924
Checksum:              335


Coasting Arc #16 (Orbit 938)
---------------------------------------

Vector Time (GMT): 2017/345/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1827023
88                 A    =         6778555
48  meter
 Y    =        4161390
49  meter          E    =           
0010085
 Z    =       -5038229
96                 I    =           51
32792
 XDOT =      -5720
727347                 Wp   =           85
56985
 YDOT =      -4747
743053  meter/sec      RA   =          231
17428  deg
 ZDOT =      -1849
383149                 TA   =          166
43231
                                          MA   =          166
40517
                                          Ha   =            220
337  n
mi
                                          Hp   =            215
528

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5994172
83                 X    =        -1848948
48
 Y    =       13652855
94  feet           Y    =         4140837
07  meter
 Z    =      -16529625
86                 Z    =        -5047158
22
 XDOT =     -18768
790507                 XDOT =       -5658
228182
 YDOT =     -15576
584819  feet/sec       YDOT =       -4811
366611  meter/sec
 ZDOT =      -6067
530018                 ZDOT =       -1877
021224

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8341461
85                 X    =         2542477
57
 Y    =       12305243
60  feet           Y    =         3750638
25  meter
 Z    =      -16569855
42                 Z    =        -5050491
93
 XDOT =     -22309
042266                 XDOT =       -6799
796083
 YDOT =       6798
985734  feet/sec       YDOT =        2072
330852  meter/sec
 ZDOT =      -6189
514237                 ZDOT =       -1886
563939


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   17345
95686579  
00016717  00000-0  10270-3 0  9158
2 25544  51
6410 232
1172 0003487 227
9645 132
1212 15
54119938  9393


Satellite: ISS
Catalog Number: 25544
Epoch time:      17345
95686579   =   yrday
fracday
Element set:     915
Inclination:       51
6410  deg
RA of node:       232
1172  deg
Eccentricity:     
0003487     
Arg of perigee:   227
9645  deg
Mean anomaly:     132
1212  deg
Mean motion:   15
54119938  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             939
Checksum:              325


Coasting Arc #17 (Orbit 954)
---------------------------------------

Vector Time (GMT): 2017/346/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3100731
76                 A    =         6777216
55  meter
 Y    =       -2882523
50  meter          E    =           
0002008
 Z    =        5292397
00                 I    =           51
34592
 XDOT =       5276
234826                 Wp   =          187
69773
 YDOT =       5565
011693  meter/sec      RA   =          226
15402  deg
 ZDOT =        -62
215564                 TA   =          262
88608
                                          MA   =          262
90892
                                          Ha   =            220
090  n
mi
                                          Hp   =            215
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10173004
46                 X    =         3107026
37
 Y    =       -9457098
08  feet           Y    =        -2847814
05  meter
 Z    =       17363507
23                 Z    =         5307474
68
 XDOT =      17310
481713                 XDOT =        5213
915445
 YDOT =      18257
912379  feet/sec       YDOT =        5623
665712  meter/sec
 ZDOT =       -204
119303                 ZDOT =         -36
736134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2792404
80                 X    =         -851124
98
 Y    =      -13519841
80  feet           Y    =        -4120847
78  meter
 Z    =       17430847
95                 Z    =         5312922
46
 XDOT =      23632
231991                 XDOT =        7203
104311
 YDOT =      -4991
162219  feet/sec       YDOT =       -1521
306244  meter/sec
 ZDOT =        -91
817283                 ZDOT =         -27
985908


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   17346
98569058  
00016717  00000-0  10270-3 0  9165
2 25544  51
6415 226
9885 0003359 232
6580 127
4267 15
54173350  9552


Satellite: ISS
Catalog Number: 25544
Epoch time:      17346
98569058   =   yrday
fracday
Element set:     916
Inclination:       51
6415  deg
RA of node:       226
9885  deg
Eccentricity:     
0003359     
Arg of perigee:   232
6580  deg
Mean anomaly:     127
4267  deg
Mean motion:   15
54173350  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             955
Checksum:              341


Coasting Arc #18 (Orbit 969)
---------------------------------------

Vector Time (GMT): 2017/347/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4317159
83                 A    =         6778526
83  meter
 Y    =        1538665
47  meter          E    =           
0011047
 Z    =       -5004358
01                 I    =           51
37228
 XDOT =      -4408
675005                 Wp   =          117
47143
 YDOT =      -5944
983738  meter/sec      RA   =          221
13622  deg
 ZDOT =       1973
761792                 TA   =          171
79633
                                          MA   =          171
77825
                                          Ha   =            220
163  n
mi
                                          Hp   =            215
439

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14163910
22                 X    =        -4309735
79
 Y    =        5048115
06  feet           Y    =         1490429
85  meter
 Z    =      -16418497
42                 Z    =        -5025311
53
 XDOT =     -14464
156840                 XDOT =       -4351
456600
 YDOT =     -19504
539824  feet/sec       YDOT =       -5993
964747  meter/sec
 ZDOT =       6475
596429                 ZDOT =        1952
484221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2804506
53                 X    =         -854813
59
 Y    =       14668477
00  feet           Y    =         4470951
79  meter
 Z    =      -16511735
27                 Z    =        -5032776
91
 XDOT =     -23101
512079                 XDOT =       -7041
340882
 YDOT =       2773
130461  feet/sec       YDOT =         845
250164  meter/sec
 ZDOT =       6381
985040                 ZDOT =        1945
229040


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   17347
95021360  
00016717  00000-0  10270-3 0  9173
2 25544  51
6402 222
1813 0003220 235
8645 124
2203 15
54157011  9709


Satellite: ISS
Catalog Number: 25544
Epoch time:      17347
95021360   =   yrday
fracday
Element set:     917
Inclination:       51
6402  deg
RA of node:       222
1813  deg
Eccentricity:     
0003220     
Arg of perigee:   235
8645  deg
Mean anomaly:     124
2203  deg
Mean motion:   15
54157011  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             970
Checksum:              266


Coasting Arc #19 (Orbit 971)
---------------------------------------

Vector Time (GMT): 2017/348/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 940547
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -793675
07                 A    =         6778816
96  meter
 Y    =        4549114
87  meter          E    =           
0009706
 Z    =       -4971486
00                 I    =           51
37603
 XDOT =      -6537
655759                 Wp   =           80
41928
 YDOT =      -3409
979180  meter/sec      RA   =          220
56168  deg
 ZDOT =      -2078
455851                 TA   =          169
27064
                                          MA   =          169
24992
                                          Ha   =            220
209  n
mi
                                          Hp   =            215
521

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2603920
83                 X    =         -820336
22
 Y    =       14924917
56  feet           Y    =         4540090
69  meter
 Z    =      -16310649
61                 Z    =        -4975405
94
 XDOT =     -21449
001835                 XDOT =       -6488
942344
 YDOT =     -11187
595734  feet/sec       YDOT =       -3482
815215  meter/sec
 ZDOT =      -6819
080876                 ZDOT =       -2110
095969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15097681
83                 X    =         4601773
42
 Y    =       -1002229
20  feet           Y    =         -305479
46  meter
 Z    =      -16328698
62                 Z    =        -4976987
34
 XDOT =      -6039
300696                 XDOT =       -1840
778852
 YDOT =      22301
999960  feet/sec       YDOT =        6797
649588  meter/sec
 ZDOT =      -6959
057553                 ZDOT =       -2121
120742


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   17348
07881714  
00016717  00000-0  10270-3 0  9185
2 25544  51
6403 221
5410 0003036 236
0672 124
0193 15
54137237  9720


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
07881714   =   yrday
fracday
Element set:     918
Inclination:       51
6403  deg
RA of node:       221
5410  deg
Eccentricity:     
0003036     
Arg of perigee:   236
0672  deg
Mean anomaly:     124
0193  deg
Mean motion:   15
54137237  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             972
Checksum:              289


Coasting Arc #20 (Orbit 974)
---------------------------------------

Vector Time (GMT): 2017/348/05:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 925316
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         528711
94                 A    =         6779046
44  meter
 Y    =       -4653212
21  meter          E    =           
0005804
 Z    =        4900546
18                 I    =           51
37785
 XDOT =       6615
318947                 Wp   =          148
91543
 YDOT =       3146
798475  meter/sec      RA   =          219
76127  deg
 ZDOT =       2268
177487                 TA   =          278
80651
                                          MA   =          278
87223
                                          Ha   =            220
085  n
mi
                                          Hp   =            215
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1734619
22                 X    =          556901
42
 Y    =      -15266444
26  feet           Y    =        -4647142
49  meter
 Z    =       16077907
42                 Z    =         4903182
70
 XDOT =      21703
802318                 XDOT =        6568
621131
 YDOT =      10324
141978  feet/sec       YDOT =        3220
514245  meter/sec
 ZDOT =       7441
527187                 ZDOT =        2300
199762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6460569
02                 X    =        -1969181
44
 Y    =       13926108
06  feet           Y    =         4244677
74  meter
 Z    =       16090273
26                 Z    =         4904315
29
 XDOT =     -16157
200865                 XDOT =       -4924
714824
 YDOT =     -16280
359609  feet/sec       YDOT =       -4962
253609  meter/sec
 ZDOT =       7583
240727                 ZDOT =        2311
371774


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   17348
27172080  
00016717  00000-0  10270-3 0  9197
2 25544  51
6373 220
5800 0003050 241
5346 118
5499 15
54154809  9757


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
27172080   =   yrday
fracday
Element set:     919
Inclination:       51
6373  deg
RA of node:       220
5800  deg
Eccentricity:     
0003050     
Arg of perigee:   241
5346  deg
Mean anomaly:     118
5499  deg
Mean motion:   15
54154809  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             975
Checksum:              308
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