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

 
Date: July 22nd 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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


209/14:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 212 3

209/15:41:14 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 3

209/20:00:20 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 3

212/23:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 212 1

214/15:20:50 280 -0 6 0 7 0 7
N/A 0 1 -0 0 223 0
000/00:01:40 559 0 1 -0 0 212 6

216/02:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 7

Coasting Arc #1 (Orbit 2708)
---------------------------------------

Vector Time (GMT): 2017/202/12:49:52
952
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4510652
67                 A    =         6789076
31  meter
 Y    =        5059366
16  meter          E    =           
0013906
 Z    =        -330291
06                 I    =           51
38381
 XDOT =      -3762
330193                 Wp   =          111
34885
 YDOT =       2977
609931  meter/sec      RA   =          226
05091  deg
 ZDOT =      -5978
365194                 TA   =           72
22251
                                          MA   =           72
07082
                                          Ha   =            222
988  n
mi
                                          Hp   =            212
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14798729
23                 X    =         4455346
63
 Y    =       16598970
35  feet           Y    =         5109498
15  meter
 Z    =       -1083632
08                 Z    =         -308513
68
 XDOT =     -12343
602994                 XDOT =       -3766
307381
 YDOT =       9769
061455  feet/sec       YDOT =        2935
515492  meter/sec
 ZDOT =     -19614
059034                 ZDOT =       -5996
650505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2781290
43                 X    =          847737
32
 Y    =      -22067857
30  feet           Y    =        -6726282
91  meter
 Z    =        -988210
26                 Z    =         -301206
49
 XDOT =      13780
173749                 XDOT =        4200
196959
 YDOT =       2585
144798  feet/sec       YDOT =         787
952135  meter/sec
 ZDOT =     -19695
289975                 ZDOT =       -6003
124384


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   17202
56626944  
00016717  00000-0  10270-3 0  9001
2 25544  51
6379 226
9595 0006168  56
5504 303
6238 15
54200987 27091


Satellite: ISS
Catalog Number: 25544
Epoch time:      17202
56626944   =   yrday
fracday
Element set:     900
Inclination:       51
6379  deg
RA of node:       226
9595  deg
Eccentricity:     
0006168     
Arg of perigee:    56
5504  deg
Mean anomaly:     303
6238  deg
Mean motion:   15
54200987  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2709
Checksum:              326


Coasting Arc #2 (Orbit 2724)
---------------------------------------

Vector Time (GMT): 2017/203/12:49:52
952
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3685085
18                 A    =         6787407
55  meter
 Y    =       -5325754
73  meter          E    =           
0019923
 Z    =        1998016
58                 I    =           51
40095
 XDOT =       5101
094655                 Wp   =           65
62204
 YDOT =      -1433
510403  meter/sec      RA   =          221
06229  deg
 ZDOT =       5551
638241                 TA   =          316
53867
                                          MA   =          316
69553
                                          Ha   =            222
926  n
mi
                                          Hp   =            212
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12090174
49                 X    =        -3634962
52
 Y    =      -17472948
58  feet           Y    =        -5366683
82  meter
 Z    =        6555172
49                 Z    =         1980237
02
 XDOT =      16735
874854                 XDOT =        5089
778762
 YDOT =      -4703
118119  feet/sec       YDOT =       -1376
530399  meter/sec
 ZDOT =      18214
036223                 ZDOT =        5576
389704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4840516
45                 X    =        -1475389
41
 Y    =       20713735
52  feet           Y    =         6313546
59  meter
 Z    =        6477429
96                 Z    =         1974320
65
 XDOT =     -13113
242522                 XDOT =       -3996
916321
 YDOT =      -8831
381594  feet/sec       YDOT =       -2691
805110  meter/sec
 ZDOT =      18323
606795                 ZDOT =        5585
035351


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   17203
59505033  
00016717  00000-0  10270-3 0  9011
2 25544  51
6372 221
8306 0006027  59
2335 300
9410 15
54223063 27254


Satellite: ISS
Catalog Number: 25544
Epoch time:      17203
59505033   =   yrday
fracday
Element set:     901
Inclination:       51
6372  deg
RA of node:       221
8306  deg
Eccentricity:     
0006027     
Arg of perigee:    59
2335  deg
Mean anomaly:     300
9410  deg
Mean motion:   15
54223063  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2725
Checksum:              269


Coasting Arc #3 (Orbit 2739)
---------------------------------------

Vector Time (GMT): 2017/204/12:49:52
952
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2478449
03                 A    =         6783973
65  meter
 Y    =        5262616
88  meter          E    =           
0010974
 Z    =       -3502797
40                 I    =           51
41429
 XDOT =      -6196
249523                 Wp   =           73
85916
 YDOT =        -71
144836  meter/sec      RA   =          216
06667  deg
 ZDOT =      -4499
900647                 TA   =          147
43594
                                          MA   =          147
36820
                                          Ha   =            223
050  n
mi
                                          Hp   =            212
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8131394
46                 X    =         2436431
37
 Y    =       17265803
43  feet           Y    =         5290097
98  meter
 Z    =      -11492117
44                 Z    =        -3490859
67
 XDOT =     -20328
902633                 XDOT =       -6173
135606
 YDOT =       -233
414815  feet/sec       YDOT =        -140
305841  meter/sec
 ZDOT =     -14763
453566                 ZDOT =       -4529
943336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7012423
00                 X    =         2137386
53
 Y    =      -17783280
30  feet           Y    =        -5420343
83  meter
 Z    =      -11440156
14                 Z    =        -3486959
59
 XDOT =      12344
317225                 XDOT =        3762
547890
 YDOT =      14431
950059  feet/sec       YDOT =        4398
858378  meter/sec
 ZDOT =     -14896
191853                 ZDOT =       -4540
359277


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   17204
55953080  
00016717  00000-0  10270-3 0  9028
2 25544  51
6369 217
0210 0006190  62
7094 297
4688 15
54199527 27404


Satellite: ISS
Catalog Number: 25544
Epoch time:      17204
55953080   =   yrday
fracday
Element set:     902
Inclination:       51
6369  deg
RA of node:       217
0210  deg
Eccentricity:     
0006190     
Arg of perigee:    62
7094  deg
Mean anomaly:     297
4688  deg
Mean motion:   15
54199527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2740
Checksum:              316


Coasting Arc #4 (Orbit 2755)
---------------------------------------

Vector Time (GMT): 2017/205/12:49:52
952
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1007917
76                 A    =         6780162
88  meter
 Y    =       -4878726
19  meter          E    =           
0013355
 Z    =        4588117
62                 I    =           51
42756
 XDOT =       6930
953206                 Wp   =           93
94436
 YDOT =       1389
594131  meter/sec      RA   =          211
06333  deg
 ZDOT =       2991
774161                 TA   =          326
11024
                                          MA   =          326
19550
                                          Ha   =            223
031  n
mi
                                          Hp   =            212
457

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3306816
79                 X    =         -975573
95
 Y    =      -16006319
50  feet           Y    =        -4889816
88  meter
 Z    =       15052879
34                 Z    =         4583299
80
 XDOT =      22739
347790                 XDOT =        6900
367043
 YDOT =       4559
035864  feet/sec       YDOT =        1466
929530  meter/sec
 ZDOT =       9815
532025                 ZDOT =        3025
367622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9137600
02                 X    =        -2785140
49
 Y    =       13574257
53  feet           Y    =         4137433
69  meter
 Z    =       15032307
75                 Z    =         4581847
40
 XDOT =     -11495
372351                 XDOT =       -3503
789493
 YDOT =     -18802
871985  feet/sec       YDOT =       -5731
115381  meter/sec
 ZDOT =       9963
785469                 ZDOT =        3036
961811


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   17205
58830587  
00016717  00000-0  10270-3 0  9039
2 25544  51
6359 211
8918 0006131  64
6780 295
5008 15
54210867 27561


Satellite: ISS
Catalog Number: 25544
Epoch time:      17205
58830587   =   yrday
fracday
Element set:     903
Inclination:       51
6359  deg
RA of node:       211
8918  deg
Eccentricity:     
0006131     
Arg of perigee:    64
6780  deg
Mean anomaly:     295
5008  deg
Mean motion:   15
54210867  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2756
Checksum:              324


Coasting Arc #5 (Orbit 2770)
---------------------------------------

Vector Time (GMT): 2017/206/12:49:52
952
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -665666
56                 A    =         6777598
99  meter
 Y    =        4299970
62  meter          E    =           
0020224
 Z    =       -5214300
14                 I    =           51
44766
 XDOT =      -7148
500178                 Wp   =           77
65765
 YDOT =      -2486
018786  meter/sec      RA   =          206
05217  deg
 ZDOT =      -1137
015077                 TA   =          181
38851
                                          MA   =          181
39413
                                          Ha   =            223
071  n
mi
                                          Hp   =            212
339

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2183945
40                 X    =         -688372
54
 Y    =       14107515
16  feet           Y    =         4292399
96  meter
 Z    =      -17107283
92                 Z    =        -5217588
63
 XDOT =     -23453
084575                 XDOT =       -7114
646635
 YDOT =      -8156
229614  feet/sec       YDOT =       -2565
768834  meter/sec
 ZDOT =      -3730
364425                 ZDOT =       -1171
657392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11435433
03                 X    =         3485519
99
 Y    =       -8514901
69  feet           Y    =        -2595342
04  meter
 Z    =      -17122443
91                 Z    =        -5218920
90
 XDOT =      10188
454333                 XDOT =        3105
440881
 YDOT =      21494
702106  feet/sec       YDOT =        6551
585202  meter/sec
 ZDOT =      -3883
114766                 ZDOT =       -1183
573381


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   17206
55278098  
00016717  00000-0  10270-3 0  9041
2 25544  51
6361 207
0830 0006180  68
8435 291
3378 15
54207199 27716


Satellite: ISS
Catalog Number: 25544
Epoch time:      17206
55278098   =   yrday
fracday
Element set:     904
Inclination:       51
6361  deg
RA of node:       207
0830  deg
Eccentricity:     
0006180     
Arg of perigee:    68
8435  deg
Mean anomaly:     291
3378  deg
Mean motion:   15
54207199  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2771
Checksum:              321


Coasting Arc #6 (Orbit 2786)
---------------------------------------

Vector Time (GMT): 2017/207/12:49:52
952
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2382028
79                 A    =         6777271
50  meter
 Y    =       -3558368
71  meter          E    =           
0009281
 Z    =        5246069
68                 I    =           51
47729
 XDOT =       6854
929959                 Wp   =           68
41968
 YDOT =       3349
700223  meter/sec      RA   =          201
03887  deg
 ZDOT =       -835
932177                 TA   =           29
60872
                                          MA   =           29
55621
                                          Ha   =            222
950  n
mi
                                          Hp   =            212
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7815055
09                 X    =         2396160
04
 Y    =      -11674438
03  feet           Y    =        -3531652
36  meter
 Z    =       17211514
69                 Z    =         5257674
84
 XDOT =      22489
927688                 XDOT =        6821
023726
 YDOT =      10989
830127  feet/sec       YDOT =        3426
167146  meter/sec
 ZDOT =      -2742
559637                 ZDOT =        -802
715979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13648509
00                 X    =        -4160065
54
 Y    =        3049534
89  feet           Y    =          929498
24  meter
 Z    =       17263324
31                 Z    =         5261861
25
 XDOT =      -8339
466245                 XDOT =       -2541
869312
 YDOT =     -22542
988395  feet/sec       YDOT =       -6871
102863  meter/sec
 ZDOT =      -2596
216236                 ZDOT =        -791
326709


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   17207
58155047  
00016717  00000-0  10270-3 0  9054
2 25544  51
6367 201
9534 0006102  71
7255 288
4561 15
54224463 27874


Satellite: ISS
Catalog Number: 25544
Epoch time:      17207
58155047   =   yrday
fracday
Element set:     905
Inclination:       51
6367  deg
RA of node:       201
9534  deg
Eccentricity:     
0006102     
Arg of perigee:    71
7255  deg
Mean anomaly:     288
4561  deg
Mean motion:   15
54224463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2787
Checksum:              312


Coasting Arc #7 (Orbit 2801)
---------------------------------------

Vector Time (GMT): 2017/208/12:49:52
952
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3988951
85                 A    =         6779484
19  meter
 Y    =        2776185
10  meter          E    =           
0016652
 Z    =       -4741995
01                 I    =           51
51579
 XDOT =      -5967
761105                 Wp   =           96
99519
 YDOT =      -3956
367468  meter/sec      RA   =          196
03130  deg
 ZDOT =       2710
031205                 TA   =          199
85818
                                          MA   =          199
92308
                                          Ha   =            223
089  n
mi
                                          Hp   =            212
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13087112
38                 X    =        -3996665
52
 Y    =        9108218
82  feet           Y    =         2731534
86  meter
 Z    =      -15557726
42                 Z    =        -4761390
49
 XDOT =     -19579
268718                 XDOT =       -5936
240212
 YDOT =     -12980
208229  feet/sec       YDOT =       -4022
926819  meter/sec
 ZDOT =       8891
178495                 ZDOT =        2681
118654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15707426
67                 X    =         4787623
65
 Y    =        2195739
42  feet           Y    =          669261
38  meter
 Z    =      -15643864
22                 Z    =        -4768249
81
 XDOT =       5669
286430                 XDOT =        1727
998504
 YDOT =      21739
727847  feet/sec       YDOT =        6626
269048  meter/sec
 ZDOT =       8763
927235                 ZDOT =        2671
245021


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   17208
54601899  
00016717  00000-0  10270-3 0  9063
2 25544  51
6371 197
1451 0006196  74
2665 285
9171 15
54208627 28020


Satellite: ISS
Catalog Number: 25544
Epoch time:      17208
54601899   =   yrday
fracday
Element set:     906
Inclination:       51
6371  deg
RA of node:       197
1451  deg
Eccentricity:     
0006196     
Arg of perigee:    74
2665  deg
Mean anomaly:     285
9171  deg
Mean motion:   15
54208627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2802
Checksum:              327


Coasting Arc #8 (Orbit 2817)
---------------------------------------

Vector Time (GMT): 2017/209/12:49:52
952
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5346839
85                 A    =         6783131
90  meter
 Y    =       -1936817
38  meter          E    =           
0017761
 Z    =        3684277
64                 I    =           51
55958
 XDOT =       4580
007254                 Wp   =           82
39055
 YDOT =       4386
947031  meter/sec      RA   =          191
03404  deg
 ZDOT =      -4320
398670                 TA   =           53
64689
                                          MA   =           53
48310
                                          Ha   =            222
942  n
mi
                                          Hp   =            212
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17542125
49                 X    =         5350204
29
 Y    =       -6354387
72  feet           Y    =        -1877006
61  meter
 Z    =       12087525
06                 Z    =         3710258
74
 XDOT =      15026
270518                 XDOT =        4551
596963
 YDOT =      14392
870836  feet/sec       YDOT =        4438
004980  meter/sec
 ZDOT =     -14174
536318                 ZDOT =       -4298
219660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17226554
84                 X    =        -5250653
91
 Y    =       -6968027
16  feet           Y    =        -2123854
68  meter
 Z    =       12202666
84                 Z    =         3719372
85
 XDOT =      -2107
959652                 XDOT =        -642
506102
 YDOT =     -19555
758201  feet/sec       YDOT =       -5960
595100  meter/sec
 ZDOT =     -14077
099769                 ZDOT =       -4290
700009


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   17209
57478301  
00016717  00000-0  10270-3 0  9078
2 25544  51
6368 192
0158 0006105  77
4529 282
7306 15
54240445 28184


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
57478301   =   yrday
fracday
Element set:     907
Inclination:       51
6368  deg
RA of node:       192
0158  deg
Eccentricity:     
0006105     
Arg of perigee:    77
4529  deg
Mean anomaly:     282
7306  deg
Mean motion:   15
54240445  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2818
Checksum:              316


Coasting Arc #9 (Orbit 2818)
---------------------------------------

Vector Time (GMT): 2017/209/14:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3163345
08                 A    =         6780994
14  meter
 Y    =        4125352
02  meter          E    =           
0014806
 Z    =       -4368767
72                 I    =           51
55657
 XDOT =      -6681
367353                 Wp   =           73
27482
 YDOT =       1505
055882  meter/sec      RA   =          190
67424  deg
 ZDOT =      -3422
123972                 TA   =          161
95321
                                          MA   =          161
90059
                                          Ha   =            223
051  n
mi
                                          Hp   =            212
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10378428
73                 X    =         3138200
26
 Y    =       13534619
49  feet           Y    =         4160586
15  meter
 Z    =      -14333227
44                 Z    =        -4353462
40
 XDOT =     -21920
496565                 XDOT =       -6681
077928
 YDOT =       4937
847381  feet/sec       YDOT =        1430
341947  meter/sec
 ZDOT =     -11227
440854                 ZDOT =       -3454
578849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7320196
10                 X    =        -2231195
77
 Y    =      -15467094
36  feet           Y    =        -4714370
36  meter
 Z    =      -14266143
04                 Z    =        -4348320
40
 XDOT =      21269
142362                 XDOT =        6482
834592
 YDOT =        405
444082  feet/sec       YDOT =         123
579356  meter/sec
 ZDOT =     -11371
144363                 ZDOT =       -3465
924802


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   17209
63908114  
00016717  00000-0  10270-3 0  9086
2 25544  51
6386 191
6952 0006155  77
5438 282
6403 15
54245131 28191


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
63908114   =   yrday
fracday
Element set:     908
Inclination:       51
6386  deg
RA of node:       191
6952  deg
Eccentricity:     
0006155     
Arg of perigee:    77
5438  deg
Mean anomaly:     282
6403  deg
Mean motion:   15
54245131  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2819
Checksum:              321


Coasting Arc #10 (Orbit 2819)
---------------------------------------

Vector Time (GMT): 2017/209/15:41:14
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -154485
05                 A    =         6777175
02  meter
 Y    =       -4270533
57  meter          E    =           
0008709
 Z    =        5252650
15                 I    =           51
54583
 XDOT =       7595
491970                 Wp   =           93
31354
 YDOT =        739
548121  meter/sec      RA   =          190
47406  deg
 ZDOT =        822
989615                 TA   =          348
80728
                                          MA   =          348
82664
                                          Ha   =            222
925  n
mi
                                          Hp   =            212
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -506840
70                 X    =         -132233
80
 Y    =      -14010936
91  feet           Y    =        -4272136
77  meter
 Z    =       17233104
17                 Z    =         5251953
72
 XDOT =      24919
593079                 XDOT =        7582
660009
 YDOT =       2426
338980  feet/sec       YDOT =         824
414317  meter/sec
 ZDOT =       2700
097163                 ZDOT =         859
854535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         849241
40                 X    =          258848
78
 Y    =       13997403
87  feet           Y    =         4266408
70  meter
 Z    =       17230629
53                 Z    =         5251895
88
 XDOT =     -23917
108663                 XDOT =       -7289
934720
 YDOT =      -2079
961734  feet/sec       YDOT =        -633
972337  meter/sec
 ZDOT =       2862
981448                 ZDOT =         872
636745


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   17209
70337756  
00016717  00000-0  10270-3 0  9093
2 25544  51
6390 191
3758 0005935  77
8849 282
2969 15
54272239 28205


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
70337756   =   yrday
fracday
Element set:     909
Inclination:       51
6390  deg
RA of node:       191
3758  deg
Eccentricity:     
0005935     
Arg of perigee:    77
8849  deg
Mean anomaly:     282
2969  deg
Mean motion:   15
54272239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2820
Checksum:              352


Coasting Arc #11 (Orbit 2822)
---------------------------------------

Vector Time (GMT): 2017/209/20:00:20
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6481982
78                 A    =         6788661
00  meter
 Y    =       -1791598
39  meter          E    =           
0018931
 Z    =         867979
57                 I    =           51
59052
 XDOT =       2029
025788                 Wp   =           61
80372
 YDOT =      -4425
020380  meter/sec      RA   =          189
57714  deg
 ZDOT =       5929
076940                 TA   =          307
59812
                                          MA   =          307
76984
                                          Ha   =            222
940  n
mi
                                          Hp   =            212
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21266347
70                 X    =        -6465683
07
 Y    =       -5877947
46  feet           Y    =        -1863993
20  meter
 Z    =        2847701
99                 Z    =          836532
05
 XDOT =       6656
908754                 XDOT =        2049
556537
 YDOT =     -14517
783398  feet/sec       YDOT =       -4402
215710  meter/sec
 ZDOT =      19452
352165                 ZDOT =        5938
983012

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14058975
74                 X    =         4285175
81
 Y    =      -17027160
52  feet           Y    =        -5189878
53  meter
 Z    =        2708915
48                 Z    =          825677
44
 XDOT =       9341
264442                 XDOT =        2847
217402
 YDOT =      10863
971961  feet/sec       YDOT =        3311
338654  meter/sec
 ZDOT =      19496
775955                 ZDOT =        5942
617311


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   17209
89626931  
00016717  00000-0  10270-3 0  9101
2 25544  51
6397 190
4142 0005927  78
5958 281
5860 15
54260815 28231


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
89626931   =   yrday
fracday
Element set:     910
Inclination:       51
6397  deg
RA of node:       190
4142  deg
Eccentricity:     
0005927     
Arg of perigee:    78
5958  deg
Mean anomaly:     281
5860  deg
Mean motion:   15
54260815  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2823
Checksum:              336


Coasting Arc #12 (Orbit 2837)
---------------------------------------

Vector Time (GMT): 2017/210/20:00:20
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5773710
33                 A    =         6786350
91  meter
 Y    =        2494002
14  meter          E    =           
0010099
 Z    =       -2553556
24                 I    =           51
61484
 XDOT =      -3993
767253                 Wp   =          105
02860
 YDOT =       3868
375870  meter/sec      RA   =          184
60073  deg
 ZDOT =      -5271
930179                 TA   =          103
65171
                                          MA   =          103
53923
                                          Ha   =            222
987  n
mi
                                          Hp   =            212
453

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18942619
20                 X    =         5757796
43
 Y    =        8182421
71  feet           Y    =         2558478
76  meter
 Z    =       -8377809
17                 Z    =        -2525548
21
 XDOT =     -13102
910935                 XDOT =       -4011
119426
 YDOT =      12691
521882  feet/sec       YDOT =        3823
617926  meter/sec
 ZDOT =     -17296
358855                 ZDOT =       -5291
372550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14984617
07                 X    =        -4567311
28
 Y    =       14257982
74  feet           Y    =         4345833
14  meter
 Z    =       -8254314
83                 Z    =        -2515915
16
 XDOT =      -5529
913855                 XDOT =       -1685
517743
 YDOT =     -15836
590980  feet/sec       YDOT =       -4826
992931  meter/sec
 ZDOT =     -17382
875263                 ZDOT =       -5298
300380


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   17210
86073212  
00016717  00000-0  10270-3 0  9119
2 25544  51
6398 185
6051 0005808  81
4375 278
7435 15
54228351 28382


Satellite: ISS
Catalog Number: 25544
Epoch time:      17210
86073212   =   yrday
fracday
Element set:     911
Inclination:       51
6398  deg
RA of node:       185
6051  deg
Eccentricity:     
0005808     
Arg of perigee:    81
4375  deg
Mean anomaly:     278
7435  deg
Mean motion:   15
54228351  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2838
Checksum:              315


Coasting Arc #13 (Orbit 2853)
---------------------------------------

Vector Time (GMT): 2017/211/20:00:20
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4603745
60                 A    =         6782635
35  meter
 Y    =       -3065935
55  meter          E    =           
0017069
 Z    =        3911767
59                 I    =           51
63404
 XDOT =       5636
924468                 Wp   =           94
13037
 YDOT =      -3256
123629  meter/sec      RA   =          179
61693  deg
 ZDOT =       4065
523577                 TA   =          313
29808
                                          MA   =          313
44031
                                          Ha   =            223
110  n
mi
                                          Hp   =            212
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15104152
23                 X    =        -4588120
63
 Y    =      -10058843
68  feet           Y    =        -3117330
51  meter
 Z    =       12833883
17                 Z    =         3889442
07
 XDOT =      18493
846679                 XDOT =        5653
168198
 YDOT =     -10682
820306  feet/sec       YDOT =       -3192
997001  meter/sec
 ZDOT =      13338
331946                 ZDOT =        4092
945148

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15039484
21                 X    =         4584034
79
 Y    =      -10278282
88  feet           Y    =        -3132820
62  meter
 Z    =       12735584
94                 Z    =         3881806
29
 XDOT =       2208
881462                 XDOT =         673
267070
 YDOT =      19977
716548  feet/sec       YDOT =        6089
208004  meter/sec
 ZDOT =      13460
058779                 ZDOT =        4102
625916


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   17211
88948846  
00016717  00000-0  10270-3 0  9127
2 25544  51
6388 180
4750 0005970  84
1007 276
0826 15
54229812 28548


Satellite: ISS
Catalog Number: 25544
Epoch time:      17211
88948846   =   yrday
fracday
Element set:     912
Inclination:       51
6388  deg
RA of node:       180
4750  deg
Eccentricity:     
0005970     
Arg of perigee:    84
1007  deg
Mean anomaly:     276
0826  deg
Mean motion:   15
54229812  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2854
Checksum:              329


Coasting Arc #14 (Orbit 2868)
---------------------------------------

Vector Time (GMT): 2017/212/20:00:20
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3045551
75                 A    =         6778959
01  meter
 Y    =        3597525
69  meter          E    =           
0017550
 Z    =       -4888220
24                 I    =           51
65305
 XDOT =      -6817
479655                 Wp   =           78
45841
 YDOT =       2536
314787  meter/sec      RA   =          174
62509  deg
 ZDOT =      -2384
770607                 TA   =          168
15723
                                          MA   =          168
11591
                                          Ha   =            222
971  n
mi
                                          Hp   =            212
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9991967
70                 X    =         3028841
31
 Y    =       11802905
80  feet           Y    =         3631489
87  meter
 Z    =      -16037467
97                 Z    =        -4873466
45
 XDOT =     -22367
059237                 XDOT =       -6833
750755
 YDOT =       8321
242740  feet/sec       YDOT =        2459
986213  meter/sec
 ZDOT =      -7824
050547                 ZDOT =       -2417
926974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14649715
16                 X    =        -4465233
18
 Y    =        5158136
79  feet           Y    =         1572200
09  meter
 Z    =      -15972722
16                 Z    =        -4868485
72
 XDOT =        668
303707                 XDOT =         203
698970
 YDOT =     -22746
030205  feet/sec       YDOT =       -6932
990006  meter/sec
 ZDOT =      -7971
056139                 ZDOT =       -2429
577911


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   17212
85394375  
00016717  00000-0  10270-3 0  9138
2 25544  51
6373 175
6661 0005905  88
9799 271
2030 15
54250213 28696


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
85394375   =   yrday
fracday
Element set:     913
Inclination:       51
6373  deg
RA of node:       175
6661  deg
Eccentricity:     
0005905     
Arg of perigee:    88
9799  deg
Mean anomaly:     271
2030  deg
Mean motion:   15
54250213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2869
Checksum:              328


Coasting Arc #15 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2666528
08                 A    =         6779389
85  meter
 Y    =        4059848
94  meter          E    =           
0017171
 Z    =       -4745654
89                 I    =           51
65944
 XDOT =      -7010
007113                 Wp   =          103
92736
 YDOT =      -1420
365636  meter/sec      RA   =          173
89710  deg
 ZDOT =       2727
997711                 TA   =          193
07368
                                          MA   =          193
11824
                                          Ha   =            223
058  n
mi
                                          Hp   =            212
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8748451
71                 X    =        -2688676
32
 Y    =       13319714
38  feet           Y    =         4029906
37  meter
 Z    =      -15569733
90                 Z    =        -4758661
59
 XDOT =     -22998
711002                 XDOT =       -7006
854384
 YDOT =      -4659
992244  feet/sec       YDOT =       -1498
738782  meter/sec
 ZDOT =       8950
123723                 ZDOT =        2693
953134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15830628
28                 X    =        -4825175
50
 Y    =       -1236427
14  feet           Y    =         -376862
99  meter
 Z    =      -15627836
33                 Z    =        -4763364
51
 XDOT =      -7007
445203                 XDOT =       -2135
869298
 YDOT =     -21328
419223  feet/sec       YDOT =       -6500
902179  meter/sec
 ZDOT =       8799
746269                 ZDOT =        2682
162663


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   17212
98253952  
00016717  00000-0  10270-3 0  9148
2 25544  51
6375 175
0220 0006168  93
8960 266
2897 15
54248768 28710


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
98253952   =   yrday
fracday
Element set:     914
Inclination:       51
6375  deg
RA of node:       175
0220  deg
Eccentricity:     
0006168     
Arg of perigee:    93
8960  deg
Mean anomaly:     266
2897  deg
Mean motion:   15
54248768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2871
Checksum:              342


Coasting Arc #16 (Orbit 2886)
---------------------------------------

Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4240861
24                 A    =         6783170
66  meter
 Y    =       -3791830
10  meter          E    =           
0017750
 Z    =        3679177
95                 I    =           51
70452
 XDOT =       5878
347627                 Wp   =           89
54773
 YDOT =       2342
498290  meter/sec      RA   =          168
90858  deg
 ZDOT =      -4343
320204                 TA   =           46
66755
                                          MA   =           46
51974
                                          Ha   =            222
992  n
mi
                                          Hp   =            212
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13913586
76                 X    =         4265075
82
 Y    =      -12440387
47  feet           Y    =        -3744270
70  meter
 Z    =       12070793
79                 Z    =         3699837
18
 XDOT =      19285
917411                 XDOT =        5872
813838
 YDOT =       7685
361845  feet/sec       YDOT =        2408
203244  meter/sec
 ZDOT =     -14249
738203                 ZDOT =       -4314
778583

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17640134
33                 X    =         5376712
94
 Y    =        5911778
29  feet           Y    =         1801910
02  meter
 Z    =       12162719
18                 Z    =         3707196
81
 XDOT =       3289
862160                 XDOT =        1002
749986
 YDOT =      19363
400721  feet/sec       YDOT =        5901
964540  meter/sec
 ZDOT =     -14123
814358                 ZDOT =       -4304
938616


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   17214
01128900  
00016717  00000-0  10270-3 0  9159
2 25544  51
6376 169
8914 0006140  97
8883 262
2967 15
54239517 28873


Satellite: ISS
Catalog Number: 25544
Epoch time:      17214
01128900   =   yrday
fracday
Element set:     915
Inclination:       51
6376  deg
RA of node:       169
8914  deg
Eccentricity:     
0006140     
Arg of perigee:    97
8883  deg
Mean anomaly:     262
2967  deg
Mean motion:   15
54239517  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2887
Checksum:              336


Coasting Arc #17 (Orbit 2896)
---------------------------------------

Vector Time (GMT): 2017/214/15:21:40
559
Vector Time (MET): N/A
Weight (LBS)     : 902208
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -240723
50                 A    =         6777704
99  meter
 Y    =        4324916
67  meter          E    =           
0019728
 Z    =       -5230254
18                 I    =           51
70986
 XDOT =      -7501
533706                 Wp   =           97
82902
 YDOT =        982
033503  meter/sec      RA   =          165
59866  deg
 ZDOT =       1158
431676                 TA   =          183
28297
                                          MA   =          183
29593
                                          Ha   =            222
975  n
mi
                                          Hp   =            212
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -789775
25                 X    =         -263662
21
 Y    =       14189359
14  feet           Y    =         4322096
76  meter
 Z    =      -17159626
58                 Z    =        -5231479
01
 XDOT =     -24611
331055                 XDOT =       -7517
584574
 YDOT =       3221
894695  feet/sec       YDOT =         898
056446  meter/sec
 ZDOT =       3800
628859                 ZDOT =        1121
952975

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         438431
75                 X    =          133634
00
 Y    =      -14197265
31  feet           Y    =        -4327326
47  meter
 Z    =      -17165659
83                 Z    =        -5232093
12
 XDOT =      23542
669267                 XDOT =        7175
805592
 YDOT =      -3668
488414  feet/sec       YDOT =       -1118
155269  meter/sec
 ZDOT =       3639
107871                 ZDOT =        1109
200079


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   17214
65425443  
00016717  00000-0  10270-3 0  9162
2 25544  51
6409 166
6910 0005504  94
4224 265
7557 15
54150308 28970


Satellite: ISS
Catalog Number: 25544
Epoch time:      17214
65425443   =   yrday
fracday
Element set:     916
Inclination:       51
6409  deg
RA of node:       166
6910  deg
Eccentricity:     
0005504     
Arg of perigee:    94
4224  deg
Mean anomaly:     265
7557  deg
Mean motion:   15
54150308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2897
Checksum:              316


Coasting Arc #18 (Orbit 2912)
---------------------------------------

Vector Time (GMT): 2017/215/15:21:40
559
Vector Time (MET): N/A
Weight (LBS)     : 902208
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1970289
66                 A    =         6780091
51  meter
 Y    =       -4550125
28  meter          E    =           
0013263
 Z    =        4614424
36                 I    =           51
74899
 XDOT =       7067
197937                 Wp   =           78
11160
 YDOT =         14
363638  meter/sec      RA   =          160
60889  deg
 ZDOT =      -2993
489698                 TA   =           41
71806
                                          MA   =           41
61699
                                          Ha   =            222
884  n
mi
                                          Hp   =            212
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6464204
91                 X    =         1998609
59
 Y    =      -14928232
56  feet           Y    =        -4527934
10  meter
 Z    =       15139187
53                 Z    =         4624063
81
 XDOT =      23186
344938                 XDOT =        7081
052801
 YDOT =         47
124795  feet/sec       YDOT =          93
471494  meter/sec
 ZDOT =      -9821
160428                 ZDOT =       -2959
126201

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5853242
06                 X    =        -1784068
18
 Y    =       15134883
93  feet           Y    =         4613112
62  meter
 Z    =       15182487
20                 Z    =         4627622
10
 XDOT =     -22134
616266                 XDOT =       -6746
631038
 YDOT =       1171
821351  feet/sec       YDOT =         357
171148  meter/sec
 ZDOT =      -9669
116767                 ZDOT =       -2947
146791


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   17215
68307736  
00016717  00000-0  10270-3 0  9171
2 25544  51
6404 161
5627 0005476  97
2660 262
9116 15
54174593 29138


Satellite: ISS
Catalog Number: 25544
Epoch time:      17215
68307736   =   yrday
fracday
Element set:     917
Inclination:       51
6404  deg
RA of node:       161
5627  deg
Eccentricity:     
0005476     
Arg of perigee:    97
2660  deg
Mean anomaly:     262
9116  deg
Mean motion:   15
54174593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2913
Checksum:              323


Coasting Arc #19 (Orbit 2919)
---------------------------------------

Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902208
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         900147
22                 A    =         6777441
51  meter
 Y    =        4143017
09  meter          E    =           
0020053
 Z    =       -5305016
88                 I    =           51
75384
 XDOT =      -7251
483782                 Wp   =           97
42032
 YDOT =       2368
646693  meter/sec      RA   =          158
24434  deg
 ZDOT =        618
884574                 TA   =          178
49246
                                          MA   =          178
48640
                                          Ha   =            222
932  n
mi
                                          Hp   =            212
733

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2953238
91                 X    =          879520
83
 Y    =       13592575
74  feet           Y    =         4152968
14  meter
 Z    =      -17404911
01                 Z    =        -5300694
15
 XDOT =     -23790
957291                 XDOT =       -7280
437871
 YDOT =       7771
150566  feet/sec       YDOT =        2287
393744  meter/sec
 ZDOT =       2030
461202                 ZDOT =         583
589400

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1750970
97                 X    =          533695
95
 Y    =       13822399
86  feet           Y    =         4213067
48  meter
 Z    =      -17386374
71                 Z    =        -5299367
01
 XDOT =     -23430
828593                 XDOT =       -7141
716555
 YDOT =       5327
394216  feet/sec       YDOT =        1623
789757  meter/sec
 ZDOT =       1873
944260                 ZDOT =         571
178211


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   17216
13318632  
00016717  00000-0  10270-3 0  9180
2 25544  51
6399 159
3162 0005404 103
9654 256
2100 15
54138363 29201


Satellite: ISS
Catalog Number: 25544
Epoch time:      17216
13318632   =   yrday
fracday
Element set:     918
Inclination:       51
6399  deg
RA of node:       159
3162  deg
Eccentricity:     
0005404     
Arg of perigee:   103
9654  deg
Mean anomaly:     256
2100  deg
Mean motion:   15
54138363  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2920
Checksum:              295


Coasting Arc #20 (Orbit 2935)
---------------------------------------

Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902208
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         804180
15                 A    =         6779172
33  meter
 Y    =       -4670339
92  meter          E    =           
0011328
 Z    =        4838617
86                 I    =           51
79129
 XDOT =       7121
808748                 Wp   =           80
46149
 YDOT =      -1378
612673  meter/sec      RA   =          153
25514  deg
 ZDOT =      -2507
490111                 TA   =           34
14311
                                          MA   =           34
07030
                                          Ha   =            222
796  n
mi
                                          Hp   =            212
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2638386
32                 X    =          832842
10
 Y    =      -15322637
52  feet           Y    =        -4661187
04  meter
 Z    =       15874730
51                 Z    =         4842593
60
 XDOT =      23365
514264                 XDOT =        7148
875414
 YDOT =      -4523
007457  feet/sec       YDOT =       -1298
820287  meter/sec
 ZDOT =      -8226
673592                 ZDOT =       -2472
829466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3731795
04                 X    =         1137451
13
 Y    =      -15074409
46  feet           Y    =        -4594680
00  meter
 Z    =       15892993
95                 Z    =         4844184
56
 XDOT =      22602
938269                 XDOT =        6889
375584
 YDOT =      -2939
508924  feet/sec       YDOT =        -895
962320  meter/sec
 ZDOT =      -8073
083260                 ZDOT =       -2460
675778


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   17217
16200342  
00016717  00000-0  10270-3 0  9193
2 25544  51
6410 154
1870 0005300 107
5744 252
5988 15
54189748 29362


Satellite: ISS
Catalog Number: 25544
Epoch time:      17217
16200342   =   yrday
fracday
Element set:     919
Inclination:       51
6410  deg
RA of node:       154
1870  deg
Eccentricity:     
0005300     
Arg of perigee:   107
5744  deg
Mean anomaly:     252
5988  deg
Mean motion:   15
54189748  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2936
Checksum:              309
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