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

 
Date: October 9th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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


283/16:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 214 4

285/09:32:03 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 214 1

285/12:56:35 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 214 0

286/19:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 214 0

290/03:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 6

294/08:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 213 3

Coasting Arc #1 (Orbit 3905)
---------------------------------------

Vector Time (GMT): 2017/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6472219
97                 A    =         6788945
69  meter
 Y    =        1743598
37  meter          E    =           
0010848
 Z    =        1055903
72                 I    =           51
51152
 XDOT =       -354
801598                 Wp   =          105
28376
 YDOT =       4906
563563  meter/sec      RA   =          202
27267  deg
 ZDOT =      -5879
660837                 TA   =           63
24933
                                          MA   =           63
13837
                                          Ha   =            221
482  n
mi
                                          Hp   =            214
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21234317
49                 X    =         6447112
39
 Y    =        5720467
11  feet           Y    =         1815834
90  meter
 Z    =        3464251
06                 Z    =         1087283
18
 XDOT =      -1164
047239                 XDOT =        -381
080650
 YDOT =      16097
649486  feet/sec       YDOT =        4902
448262  meter/sec
 ZDOT =     -19290
225842                 ZDOT =       -5881
448827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21967762
42                 X    =        -6695773
99
 Y    =        -238266
35  feet           Y    =          -72623
58  meter
 Z    =        3603007
35                 Z    =         1098196
64
 XDOT =      -3035
456290                 XDOT =        -925
207077
 YDOT =     -14242
674131  feet/sec       YDOT =       -4341
167075  meter/sec
 ZDOT =     -19298
765022                 ZDOT =       -5882
263579


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   17279
53431594  
00016717  00000-0  10270-3 0  9007
2 25544  51
6409 203
2543 0004752 348
6563  11
4481 15
54084400 39067


Satellite: ISS
Catalog Number: 25544
Epoch time:      17279
53431594   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       203
2543  deg
Eccentricity:     
0004752     
Arg of perigee:   348
6563  deg
Mean anomaly:      11
4481  deg
Mean motion:   15
54084400  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3906
Checksum:              298


Coasting Arc #2 (Orbit 3921)
---------------------------------------

Vector Time (GMT): 2017/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6278475
00                 A    =         6789295
44  meter
 Y    =       -2479636
08  meter          E    =           
0016143
 Z    =         630785
44                 I    =           51
54313
 XDOT =       2284
796226                 Wp   =           36
86508
 YDOT =      -4250
693147  meter/sec      RA   =          197
29510  deg
 ZDOT =       5965
389448                 TA   =          329
95847
                                          MA   =          330
05098
                                          Ha   =            221
586  n
mi
                                          Hp   =            214
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20598671
25                 X    =        -6253344
53
 Y    =       -8135288
96  feet           Y    =        -2549705
69  meter
 Z    =        2069506
04                 Z    =          600347
16
 XDOT =       7496
050611                 XDOT =        2303
181189
 YDOT =     -13945
843659  feet/sec       YDOT =       -4225
039558  meter/sec
 ZDOT =      19571
487691                 ZDOT =        5976
533648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22034468
72                 X    =         6716106
07
 Y    =        2347127
95  feet           Y    =          715404
60  meter
 Z    =        1934998
01                 Z    =          589787
39
 XDOT =      -3213
233700                 XDOT =        -979
393632
 YDOT =      13796
713691  feet/sec       YDOT =        4205
238333  meter/sec
 ZDOT =      19621
386036                 ZDOT =        5980
598464


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   17280
56316992  
00016717  00000-0  10270-3 0  9017
2 25544  51
6408 198
1258 0004859 352
7631   7
3451 15
54091553 39227


Satellite: ISS
Catalog Number: 25544
Epoch time:      17280
56316992   =   yrday
fracday
Element set:     901
Inclination:       51
6408  deg
RA of node:       198
1258  deg
Eccentricity:     
0004859     
Arg of perigee:   352
7631  deg
Mean anomaly:       7
3451  deg
Mean motion:   15
54091553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3922
Checksum:              318


Coasting Arc #3 (Orbit 3936)
---------------------------------------

Vector Time (GMT): 2017/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5599415
00                 A    =         6787224
50  meter
 Y    =        3081346
24  meter          E    =           
0003834
 Z    =       -2288453
59                 I    =           51
56838
 XDOT =      -4136
312334                 Wp   =           83
42343
 YDOT =       3497
699950  meter/sec      RA   =          192
31783  deg
 ZDOT =      -5418
597615                 TA   =          122
06531
                                          MA   =          122
02807
                                          Ha   =            221
651  n
mi
                                          Hp   =            214
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18370784
13                 X    =         5575658
86
 Y    =       10109403
69  feet           Y    =         3143829
70  meter
 Z    =       -7508049
82                 Z    =        -2261310
67
 XDOT =     -13570
578525                 XDOT =       -4148
795595
 YDOT =      11475
393538  feet/sec       YDOT =        3451
374616  meter/sec
 ZDOT =     -17777
551231                 ZDOT =       -5438
721648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20527775
07                 X    =        -6256865
84
 Y    =       -4481238
55  feet           Y    =        -1365881
51  meter
 Z    =       -7388201
17                 Z    =        -2251923
72
 XDOT =       9328
657085                 XDOT =        2843
374680
 YDOT =     -13316
074659  feet/sec       YDOT =       -4058
739556  meter/sec
 ZDOT =     -17867
140023                 ZDOT =       -5445
904279


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   17281
52771167  
00016717  00000-0  10270-3 0  9024
2 25544  51
6413 193
3183 0004820 356
2564   3
8552 15
54111919 39377


Satellite: ISS
Catalog Number: 25544
Epoch time:      17281
52771167   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:       193
3183  deg
Eccentricity:     
0004820     
Arg of perigee:   356
2564  deg
Mean anomaly:       3
8552  deg
Mean motion:   15
54111919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3937
Checksum:              305


Coasting Arc #4 (Orbit 3952)
---------------------------------------

Vector Time (GMT): 2017/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4465600
27                 A    =         6783674
67  meter
 Y    =       -3520864
59  meter          E    =           
0012421
 Z    =        3685040
63                 I    =           51
58798
 XDOT =       5723
462822                 Wp   =           72
23510
 YDOT =      -2722
262295  meter/sec      RA   =          187
33430  deg
 ZDOT =       4326
521642                 TA   =          331
71493
                                          MA   =          331
78232
                                          Ha   =            221
796  n
mi
                                          Hp   =            214
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14650919
52                 X    =        -4443797
66
 Y    =      -11551393
03  feet           Y    =        -3570679
84  meter
 Z    =       12090028
32                 Z    =         3663400
82
 XDOT =      18777
765163                 XDOT =        5732
461895
 YDOT =      -8931
306742  feet/sec       YDOT =       -2658
208028  meter/sec
 ZDOT =      14194
624809                 ZDOT =        4354
347126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17513306
04                 X    =         5338055
68
 Y    =        6608066
76  feet           Y    =         2014138
75  meter
 Z    =       11994601
84                 Z    =         3655954
64
 XDOT =     -14669
701065                 XDOT =       -4471
324885
 YDOT =      12839
487963  feet/sec       YDOT =        3913
475931  meter/sec
 ZDOT =      14318
248917                 ZDOT =        4364
202270


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   17282
55654943  
00016717  00000-0  10270-3 0  9031
2 25544  51
6406 188
1898 0004814    
0121    
1031 15
54121448 39538


Satellite: ISS
Catalog Number: 25544
Epoch time:      17282
55654943   =   yrday
fracday
Element set:     903
Inclination:       51
6406  deg
RA of node:       188
1898  deg
Eccentricity:     
0004814     
Arg of perigee:      
0121  deg
Mean anomaly:        
1031  deg
Mean motion:   15
54121448  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3953
Checksum:              283


Coasting Arc #5 (Orbit 3967)
---------------------------------------

Vector Time (GMT): 2017/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2969303
14                 A    =         6779868
67  meter
 Y    =        3867377
99  meter          E    =           
0013371
 Z    =       -4723755
76                 I    =           51
60915
 XDOT =      -6882
728118                 Wp   =           51
30859
 YDOT =       1908
137576  meter/sec      RA   =          182
34264  deg
 ZDOT =      -2761
319101                 TA   =          191
28460
                                          MA   =          191
31461
                                          Ha   =            221
728  n
mi
                                          Hp   =            214
392

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9741808
21                 X    =         2948782
55
 Y    =       12688248
01  feet           Y    =         3900467
80  meter
 Z    =      -15497886
37                 Z    =        -4709381
56
 XDOT =     -22581
128997                 XDOT =       -6890
140478
 YDOT =       6260
293884  feet/sec       YDOT =        1831
128633  meter/sec
 ZDOT =      -9059
445869                 ZDOT =       -2794
772023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13347002
07                 X    =        -4068166
23
 Y    =       -8927875
49  feet           Y    =        -2721216
45  meter
 Z    =      -15434685
67                 Z    =        -4704492
19
 XDOT =      18739
593532                 XDOT =        5711
828109
 YDOT =     -12080
077105  feet/sec       YDOT =       -3682
007502  meter/sec
 ZDOT =      -9207
920948                 ZDOT =       -2806
574305


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   17283
52107481  
00016717  00000-0  10270-3 0  9040
2 25544  51
6415 183
3820 0004887   2
3394 357
7780 15
54163465 39680


Satellite: ISS
Catalog Number: 25544
Epoch time:      17283
52107481   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:       183
3820  deg
Eccentricity:     
0004887     
Arg of perigee:     2
3394  deg
Mean anomaly:     357
7780  deg
Mean motion:   15
54163465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3968
Checksum:              324


Coasting Arc #6 (Orbit 3970)
---------------------------------------

Vector Time (GMT): 2017/283/16:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         973648
71                 A    =         6777635
36  meter
 Y    =        4187195
22  meter          E    =           
0015916
 Z    =       -5253283
80                 I    =           51
60385
 XDOT =      -7577
035824                 Wp   =           65
77370
 YDOT =        570
902019  meter/sec      RA   =          181
34828  deg
 ZDOT =       -945
171083                 TA   =          195
14067
                                          MA   =          195
18837
                                          Ha   =            221
730  n
mi
                                          Hp   =            214
358

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3194385
54                 X    =          952272
38
 Y    =       13737517
14  feet           Y    =         4197963
46  meter
 Z    =      -17235183
07                 Z    =        -5248606
14
 XDOT =     -24859
041416                 XDOT =       -7578
265392
 YDOT =       1873
038121  feet/sec       YDOT =         486
163515  meter/sec
 ZDOT =      -3100
954997                 ZDOT =        -981
981692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13779124
41                 X    =        -4199877
12
 Y    =        3123283
82  feet           Y    =          951976
91  meter
 Z    =      -17214988
82                 Z    =        -5247128
59
 XDOT =      -1312
462566                 XDOT =        -400
038590
 YDOT =     -23856
208742  feet/sec       YDOT =       -7271
372425  meter/sec
 ZDOT =      -3264
142912                 ZDOT =        -994
910760


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   17283
71397817  
00016717  00000-0  10270-3 0  9056
2 25544  51
6373 182
4170 0004740   2
8769 357
2410 15
54147056 39717


Satellite: ISS
Catalog Number: 25544
Epoch time:      17283
71397817   =   yrday
fracday
Element set:     905
Inclination:       51
6373  deg
RA of node:       182
4170  deg
Eccentricity:     
0004740     
Arg of perigee:     2
8769  deg
Mean anomaly:     357
2410  deg
Mean motion:   15
54147056  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3971
Checksum:              317


Coasting Arc #7 (Orbit 3986)
---------------------------------------

Vector Time (GMT): 2017/284/16:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         873554
16                 A    =         6777667
09  meter
 Y    =       -4209805
36  meter          E    =           
0007435
 Z    =        5237224
14                 I    =           51
63620
 XDOT =       7597
741029                 Wp   =           29
05447
 YDOT =        314
213169  meter/sec      RA   =          176
34668  deg
 ZDOT =      -1007
750138                 TA   =           70
63131
                                          MA   =           70
55095
                                          Ha   =            221
797  n
mi
                                          Hp   =            214
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2865991
33                 X    =          895124
15
 Y    =      -13811697
38  feet           Y    =        -4199915
86  meter
 Z    =       17182493
90                 Z    =         5241520
23
 XDOT =      24926
971879                 XDOT =        7598
557960
 YDOT =       1030
883101  feet/sec       YDOT =         399
180819  meter/sec
 ZDOT =      -3306
266856                 ZDOT =        -970
840148

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13820690
85                 X    =         4212546
57
 Y    =        2700417
20  feet           Y    =          823087
16  meter
 Z    =       17202070
77                 Z    =         5243191
17
 XDOT =       -738
402505                 XDOT =        -225
065083
 YDOT =      23944
062938  feet/sec       YDOT =        7298
150384  meter/sec
 ZDOT =      -3142
726099                 ZDOT =        -957
902915


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   17284
74279763  
00016717  00000-0  10270-3 0  9060
2 25544  51
6369 177
2878 0004711   6
8617 353
2600 15
54123828 39878


Satellite: ISS
Catalog Number: 25544
Epoch time:      17284
74279763   =   yrday
fracday
Element set:     906
Inclination:       51
6369  deg
RA of node:       177
2878  deg
Eccentricity:     
0004711     
Arg of perigee:     6
8617  deg
Mean anomaly:     353
2600  deg
Mean motion:   15
54123828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3987
Checksum:              342


Coasting Arc #8 (Orbit 3997)
---------------------------------------

Vector Time (GMT): 2017/285/09:32:03
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3343360
21                 A    =         6779435
22  meter
 Y    =       -3410923
11  meter          E    =           
0007336
 Z    =        4804546
84                 I    =           51
66774
 XDOT =       6632
723246                 Wp   =           81
26679
 YDOT =      -2876
611570  meter/sec      RA   =          172
88447  deg
 ZDOT =       2571
067982                 TA   =          343
43423
                                          MA   =          343
45818
                                          Ha   =            221
886  n
mi
                                          Hp   =            214
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10969029
57                 X    =        -3328308
29
 Y    =      -11190692
61  feet           Y    =        -3448226
46  meter
 Z    =       15762948
95                 Z    =         4788342
35
 XDOT =      21760
903037                 XDOT =        6651
908186
 YDOT =      -9437
702001  feet/sec       YDOT =       -2802
332545  meter/sec
 ZDOT =       8435
262408                 ZDOT =        2603
334810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7389190
63                 X    =         2252225
31
 Y    =       13899516
96  feet           Y    =         4236572
77  meter
 Z    =       15691560
17                 Z    =         4782787
54
 XDOT =     -22487
999447                 XDOT =       -6854
342232
 YDOT =       2261
862324  feet/sec       YDOT =         689
415636  meter/sec
 ZDOT =       8578
647610                 ZDOT =        2614
771792


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   17285
45010634  
00016717  00000-0  10270-3 0  9070
2 25544  51
6393 173
7648 0004804   8
7002 351
4234 15
54187753 39985


Satellite: ISS
Catalog Number: 25544
Epoch time:      17285
45010634   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       173
7648  deg
Eccentricity:     
0004804     
Arg of perigee:     8
7002  deg
Mean anomaly:     351
4234  deg
Mean motion:   15
54187753  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3998
Checksum:              319


Coasting Arc #9 (Orbit 3999)
---------------------------------------

Vector Time (GMT): 2017/285/12:56:35
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4780966
83                 A    =         6784110
91  meter
 Y    =       -3384797
64  meter          E    =           
0014082
 Z    =        3415677
29                 I    =           51
68980
 XDOT =       5382
737502                 Wp   =           69
27633
 YDOT =       2931
868100  meter/sec      RA   =          172
13273  deg
 ZDOT =      -4608
688225                 TA   =           70
78630
                                          MA   =           70
63397
                                          Ha   =            221
815  n
mi
                                          Hp   =            214
026

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15685586
71                 X    =         4801869
33
 Y    =      -11104979
14  feet           Y    =        -3331216
58  meter
 Z    =       11206290
31                 Z    =         3438952
94
 XDOT =      17659
899942                 XDOT =        5371
939520
 YDOT =       9618
989830  feet/sec       YDOT =        2992
000952  meter/sec
 ZDOT =     -15120
368191                 ZDOT =       -4582
566620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6554425
32                 X    =        -1997788
84
 Y    =       18001806
03  feet           Y    =         5486950
48  meter
 Z    =       11309890
49                 Z    =         3447254
62
 XDOT =     -18767
633516                 XDOT =       -5720
374696
 YDOT =       2635
145105  feet/sec       YDOT =         803
192228  meter/sec
 ZDOT =     -15004
959468                 ZDOT =       -4573
511646


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   17285
57870746  
00016717  00000-0  10270-3 0  9082
2 25544  51
6408 173
1247 0005016   9
1695 350
9548 15
54190975 40007


Satellite: ISS
Catalog Number: 25544
Epoch time:      17285
57870746   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:       173
1247  deg
Eccentricity:     
0005016     
Arg of perigee:     9
1695  deg
Mean anomaly:     350
9548  deg
Mean motion:   15
54190975  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4000
Checksum:              323


Coasting Arc #10 (Orbit 4014)
---------------------------------------

Vector Time (GMT): 2017/286/12:56:35
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5812520
69                 A    =         6787533
55  meter
 Y    =        2901577
87  meter          E    =           
0011411
 Z    =       -1948806
56                 I    =           51
73357
 XDOT =      -3712
938467                 Wp   =           28
11596
 YDOT =      -3688
625559  meter/sec      RA   =          167
15919  deg
 ZDOT =       5605
406272                 TA   =          310
41747
                                          MA   =          310
51697
                                          Ha   =            221
875  n
mi
                                          Hp   =            214
015

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19069949
77                 X    =        -5835068
48
 Y    =        9519612
45  feet           Y    =         2836452
11  meter
 Z    =       -6393722
32                 Z    =        -1977097
17
 XDOT =     -12181
556650                 XDOT =       -3698
643871
 YDOT =     -12101
789891  feet/sec       YDOT =       -3730
065903  meter/sec
 ZDOT =      18390
440526                 ZDOT =        5587
404757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9944424
57                 X    =         3031060
61
 Y    =      -18808778
17  feet           Y    =        -5732915
59  meter
 Z    =       -6519507
20                 Z    =        -1987145
80
 XDOT =      15672
986978                 XDOT =        4777
126431
 YDOT =       1965
331168  feet/sec       YDOT =         599
032940  meter/sec
 ZDOT =      18311
108693                 ZDOT =        5581
225930


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   17286
54321389  
00016717  00000-0  10270-3 0  9095
2 25544  51
6411 168
3161 0005001  10
8263 349
2996 15
54168832 40157


Satellite: ISS
Catalog Number: 25544
Epoch time:      17286
54321389   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:       168
3161  deg
Eccentricity:     
0005001     
Arg of perigee:    10
8263  deg
Mean anomaly:     349
2996  deg
Mean motion:   15
54168832  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4015
Checksum:              306


Coasting Arc #11 (Orbit 4019)
---------------------------------------

Vector Time (GMT): 2017/286/19:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         283633
27                 A    =         6777669
77  meter
 Y    =       -4318230
71  meter          E    =           
0007864
 Z    =        5213442
24                 I    =           51
70864
 XDOT =       7520
550166                 Wp   =           35
23014
 YDOT =       -943
208706  meter/sec      RA   =          165
77173  deg
 ZDOT =      -1183
229713                 TA   =           66
14452
                                          MA   =           66
06212
                                          Ha   =            221
878  n
mi
                                          Hp   =            213
995

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         930555
34                 X    =          306575
24
 Y    =      -14167423
59  feet           Y    =        -4314930
31  meter
 Z    =       17104469
29                 Z    =         5214876
06
 XDOT =      24673
721017                 XDOT =        7536
286031
 YDOT =      -3094
516753  feet/sec       YDOT =        -859
020875  meter/sec
 ZDOT =      -3881
987249                 ZDOT =       -1146
658631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10376867
44                 X    =         3162869
20
 Y    =       -9678125
13  feet           Y    =        -2949892
54  meter
 Z    =       17111376
62                 Z    =         5215547
60
 XDOT =      19291
469888                 XDOT =        5880
040022
 YDOT =      14066
043201  feet/sec       YDOT =        4287
329968  meter/sec
 ZDOT =      -3719
738057                 ZDOT =       -1133
776160


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   17286
86471628  
00016717  00000-0  10270-3 0  9104
2 25544  51
6403 166
7077 0004486  16
2494 343
8801 15
54164390 40204


Satellite: ISS
Catalog Number: 25544
Epoch time:      17286
86471628   =   yrday
fracday
Element set:     910
Inclination:       51
6403  deg
RA of node:       166
7077  deg
Eccentricity:     
0004486     
Arg of perigee:    16
2494  deg
Mean anomaly:     343
8801  deg
Mean motion:   15
54164390  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4020
Checksum:              312


Coasting Arc #12 (Orbit 4034)
---------------------------------------

Vector Time (GMT): 2017/287/19:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2002896
93                 A    =         6780064
58  meter
 Y    =        4552841
69  meter          E    =           
0011242
 Z    =       -4616918
19                 I    =           51
74855
 XDOT =      -7044
720157                 Wp   =           86
89979
 YDOT =        -55
769853  meter/sec      RA   =          160
78250  deg
 ZDOT =       3008
035690                 TA   =          213
06759
                                          MA   =          213
13793
                                          Ha   =            221
895  n
mi
                                          Hp   =            213
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6571184
16                 X    =        -2031232
26
 Y    =       14937144
64  feet           Y    =         4530285
10  meter
 Z    =      -15147369
39                 Z    =        -4626716
93
 XDOT =     -23112
598941                 XDOT =       -7058
184625
 YDOT =       -182
971958  feet/sec       YDOT =        -134
623754  meter/sec
 ZDOT =       9868
883496                 ZDOT =        2973
781653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14885465
92                 X    =        -4537090
01
 Y    =        6586800
98  feet           Y    =         2007656
94  meter
 Z    =      -15191395
85                 Z    =        -4630337
45
 XDOT =     -16428
093679                 XDOT =       -5007
282953
 YDOT =     -14767
163310  feet/sec       YDOT =       -4501
031377  meter/sec
 ZDOT =       9717
014983                 ZDOT =        2961
746167


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   17287
82921411  
00016717  00000-0  10270-3 0  9112
2 25544  51
6404 161
9006 0004467  19
6238 340
5086 15
54192763 40356


Satellite: ISS
Catalog Number: 25544
Epoch time:      17287
82921411   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:       161
9006  deg
Eccentricity:     
0004467     
Arg of perigee:    19
6238  deg
Mean anomaly:     340
5086  deg
Mean motion:   15
54192763  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4035
Checksum:              302


Coasting Arc #13 (Orbit 4050)
---------------------------------------

Vector Time (GMT): 2017/288/19:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3536580
99                 A    =         6783944
24  meter
 Y    =       -4607369
23  meter          E    =           
0014660
 Z    =        3497404
76                 I    =           51
79157
 XDOT =       6064
914332                 Wp   =           72
85978
 YDOT =       1193
360226  meter/sec      RA   =          155
80304  deg
 ZDOT =      -4540
837929                 TA   =           66
10738
                                          MA   =           65
95385
                                          Ha   =            221
955  n
mi
                                          Hp   =            213
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11602956
00                 X    =         3570850
13
 Y    =      -15116040
77  feet           Y    =        -4567628
80  meter
 Z    =       11474425
08                 Z    =         3514668
24
 XDOT =      19898
012899                 XDOT =        6073
176483
 YDOT =       3915
223840  feet/sec       YDOT =        1261
227982  meter/sec
 ZDOT =     -14897
762233                 ZDOT =       -4511
356221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18662968
66                 X    =         5688472
85
 Y    =       -3611184
93  feet           Y    =        -1100689
17  meter
 Z    =       11551564
88                 Z    =         3520916
98
 XDOT =      12057
079310                 XDOT =        3674
997774
 YDOT =      14866
857879  feet/sec       YDOT =        4531
418282  meter/sec
 ZDOT =     -14767
184670                 ZDOT =       -4501
037887


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   17288
85800822  
00016717  00000-0  10270-3 0  9129
2 25544  51
6402 156
7715 0004397  24
3720 335
7640 15
54172946 40515


Satellite: ISS
Catalog Number: 25544
Epoch time:      17288
85800822   =   yrday
fracday
Element set:     912
Inclination:       51
6402  deg
RA of node:       156
7715  deg
Eccentricity:     
0004397     
Arg of perigee:    24
3720  deg
Mean anomaly:     335
7640  deg
Mean motion:   15
54172946  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4051
Checksum:              308


Coasting Arc #14 (Orbit 4065)
---------------------------------------

Vector Time (GMT): 2017/289/19:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4692355
06                 A    =         6787368
18  meter
 Y    =        4453894
22  meter          E    =           
0011026
 Z    =       -2039116
41                 I    =           51
83368
 XDOT =      -4688
799690                 Wp   =           34
78388
 YDOT =      -2399
303856  meter/sec      RA   =          150
83651  deg
 ZDOT =       5572
746988                 TA   =          302
73709
                                          MA   =          302
84332
                                          Ha   =            222
029  n
mi
                                          Hp   =            213
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15394865
69                 X    =        -4731905
79
 Y    =       14612513
85  feet           Y    =         4401199
73  meter
 Z    =       -6690014
47                 Z    =        -2062007
27
 XDOT =     -15383
201082                 XDOT =       -4688
691579
 YDOT =      -7871
731811  feet/sec       YDOT =       -2451
735994  meter/sec
 ZDOT =      18283
290643                 ZDOT =        5549
970487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21166877
90                 X    =        -6451664
38
 Y    =        1055653
11  feet           Y    =          321763
07  meter
 Z    =       -6792099
88                 Z    =        -2070232
04
 XDOT =      -6534
943705                 XDOT =       -1991
850841
 YDOT =     -14536
336913  feet/sec       YDOT =       -4430
675491  meter/sec
 ZDOT =      18182
591938                 ZDOT =        5542
054023


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   17289
82249585  
00016717  00000-0  10270-3 0  9131
2 25544  51
6414 151
9636 0004602  25
0886 335
0489 15
54176334 40662


Satellite: ISS
Catalog Number: 25544
Epoch time:      17289
82249585   =   yrday
fracday
Element set:     913
Inclination:       51
6414  deg
RA of node:       151
9636  deg
Eccentricity:     
0004602     
Arg of perigee:    25
0886  deg
Mean anomaly:     335
0489  deg
Mean motion:   15
54176334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4066
Checksum:              327


Coasting Arc #15 (Orbit 4070)
---------------------------------------

Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2168674
15                 A    =         6777196
55  meter
 Y    =        3594270
74  meter          E    =           
0017740
 Z    =       -5335413
39                 I    =           51
80546
 XDOT =      -6574
194724                 Wp   =           75
63537
 YDOT =       3923
300993  meter/sec      RA   =          149
31959  deg
 ZDOT =        -24
998259                 TA   =          194
10178
                                          MA   =          194
15137
                                          Ha   =            222
210  n
mi
                                          Hp   =            213
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7115072
68                 X    =         2154238
07
 Y    =       11792226
82  feet           Y    =         3618441
01  meter
 Z    =      -17504637
11                 Z    =        -5324913
97
 XDOT =     -21568
880328                 XDOT =       -6617
456082
 YDOT =      12871
722419  feet/sec       YDOT =        3849
541966  meter/sec
 ZDOT =        -82
015284                 ZDOT =         -57
039627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13504954
31                 X    =         4116310
07
 Y    =       -2984778
42  feet           Y    =         -909760
46  meter
 Z    =      -17458536
59                 Z    =        -5321361
95
 XDOT =       4908
356116                 XDOT =        1496
066944
 YDOT =      23603
373833  feet/sec       YDOT =        7194
308344  meter/sec
 ZDOT =       -224
616925                 ZDOT =         -68
463239


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   17290
14399038  
00016717  00000-0  10270-3 0  9148
2 25544  51
6384 150
3638 0004942  27
5629 332
5785 15
54185287 40716


Satellite: ISS
Catalog Number: 25544
Epoch time:      17290
14399038   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:       150
3638  deg
Eccentricity:     
0004942     
Arg of perigee:    27
5629  deg
Mean anomaly:     332
5785  deg
Mean motion:   15
54185287  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4071
Checksum:              328


Coasting Arc #16 (Orbit 4086)
---------------------------------------

Vector Time (GMT): 2017/291/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -544689
86                 A    =         6778287
39  meter
 Y    =       -4489532
74  meter          E    =           
0010349
 Z    =        5045020
73                 I    =           51
83582
 XDOT =       6789
587703                 Wp   =           43
79009
 YDOT =      -3004
812822  meter/sec      RA   =          144
33187  deg
 ZDOT =      -1931
266887                 TA   =           64
93702
                                          MA   =           64
82964
                                          Ha   =            222
221  n
mi
                                          Hp   =            213
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1787040
21                 X    =         -518952
90
 Y    =      -14729438
12  feet           Y    =        -4495479
35  meter
 Z    =       16551905
27                 Z    =         5042437
77
 XDOT =      22275
550207                 XDOT =        6832
065022
 YDOT =      -9858
309784  feet/sec       YDOT =       -2928
649731  meter/sec
 ZDOT =      -6336
177451                 ZDOT =       -1898
181065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14589787
31                 X    =        -4446967
17
 Y    =       -2765464
82  feet           Y    =         -842913
68  meter
 Z    =       16541031
98                 Z    =         5041706
55
 XDOT =      -2653
311428                 XDOT =        -808
729323
 YDOT =     -23209
922588  feet/sec       YDOT =       -7074
384405  meter/sec
 ZDOT =      -6189
046897                 ZDOT =       -1886
421494


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   17291
17276962  
00016717  00000-0  10270-3 0  9153
2 25544  51
6371 145
2344 0004996  29
5802 330
5632 15
54212307 40873


Satellite: ISS
Catalog Number: 25544
Epoch time:      17291
17276962   =   yrday
fracday
Element set:     915
Inclination:       51
6371  deg
RA of node:       145
2344  deg
Eccentricity:     
0004996     
Arg of perigee:    29
5802  deg
Mean anomaly:     330
5632  deg
Mean motion:   15
54212307  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4087
Checksum:              310


Coasting Arc #17 (Orbit 4101)
---------------------------------------

Vector Time (GMT): 2017/292/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -958839
91                 A    =         6781491
08  meter
 Y    =        5210570
88  meter          E    =           
0010527
 Z    =       -4241198
37                 I    =           51
87193
 XDOT =      -6488
323688                 Wp   =           82
50216
 YDOT =       1780
574278  meter/sec      RA   =          139
35316  deg
 ZDOT =       3663
523498                 TA   =          224
89428
                                          MA   =          224
97946
                                          Ha   =            222
312  n
mi
                                          Hp   =            213
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3145800
22                 X    =         -996432
53
 Y    =       17095048
81  feet           Y    =         5199637
82  meter
 Z    =      -13914692
81                 Z    =        -4245948
09
 XDOT =     -21287
151207                 XDOT =       -6525
548307
 YDOT =       5841
779128  feet/sec       YDOT =        1707
809673  meter/sec
 ZDOT =      12019
434048                 ZDOT =        3631
913940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15442679
47                 X    =         4706928
70
 Y    =        7940692
68  feet           Y    =         2420323
13  meter
 Z    =      -13936444
29                 Z    =        -4247828
22
 XDOT =       -111
669113                 XDOT =         -34
036746
 YDOT =      21013
196175  feet/sec       YDOT =        6404
822194  meter/sec
 ZDOT =      11878
996350                 ZDOT =        3620
718088


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   17292
13724618  
00016717  00000-0  10270-3 0  9167
2 25544  51
6367 140
4264 0005067  33
1416 327
0054 15
54195453 41027


Satellite: ISS
Catalog Number: 25544
Epoch time:      17292
13724618   =   yrday
fracday
Element set:     916
Inclination:       51
6367  deg
RA of node:       140
4264  deg
Eccentricity:     
0005067     
Arg of perigee:    33
1416  deg
Mean anomaly:     327
0054  deg
Mean motion:   15
54195453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4102
Checksum:              288


Coasting Arc #18 (Orbit 4117)
---------------------------------------

Vector Time (GMT): 2017/293/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2309569
54                 A    =         6785289
49  meter
 Y    =       -5655940
30  meter          E    =           
0016206
 Z    =        2941491
44                 I    =           51
90940
 XDOT =       5782
320471                 Wp   =           81
87758
 YDOT =       -269
171554  meter/sec      RA   =          134
38496  deg
 ZDOT =      -5031
788851                 TA   =           64
67327
                                          MA   =           64
50551
                                          Ha   =            222
259  n
mi
                                          Hp   =            213
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7577327
90                 X    =         2358355
45
 Y    =      -18556234
57  feet           Y    =        -5629840
05  meter
 Z    =        9650562
48                 Z    =         2952829
93
 XDOT =      18970
867688                 XDOT =        5809
343234
 YDOT =       -883
108772  feet/sec       YDOT =        -204
359085  meter/sec
 ZDOT =     -16508
493607                 ZDOT =       -5003
633775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15744873
20                 X    =        -4799037
35
 Y    =      -12363688
65  feet           Y    =        -3768452
30  meter
 Z    =        9701611
55                 Z    =         2957051
20
 XDOT =       3538
142824                 XDOT =        1078
425933
 YDOT =     -17427
971888  feet/sec       YDOT =       -5312
045832  meter/sec
 ZDOT =     -16383
566568                 ZDOT =       -4993
711090


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   17293
16601418  
00016717  00000-0  10270-3 0  9174
2 25544  51
6369 135
2962 0005073  35
5434 324
6056 15
54243656 41180


Satellite: ISS
Catalog Number: 25544
Epoch time:      17293
16601418   =   yrday
fracday
Element set:     917
Inclination:       51
6369  deg
RA of node:       135
2962  deg
Eccentricity:     
0005073     
Arg of perigee:    35
5434  deg
Mean anomaly:     324
6056  deg
Mean motion:   15
54243656  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4118
Checksum:              308


Coasting Arc #19 (Orbit 4132)
---------------------------------------

Vector Time (GMT): 2017/294/03:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3340015
72                 A    =         6788159
37  meter
 Y    =        5743510
85  meter          E    =           
0013744
 Z    =       -1364045
80                 I    =           51
94125
 XDOT =      -4770
562643                 Wp   =           39
01679
 YDOT =      -1397
312870  meter/sec      RA   =          129
42904  deg
 ZDOT =       5839
927749                 TA   =          306
18504
                                          MA   =          306
31208
                                          Ha   =            222
337  n
mi
                                          Hp   =            213
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10958056
82                 X    =        -3397366
91
 Y    =       18843539
54  feet           Y    =         5705839
74  meter
 Z    =       -4475215
89                 Z    =        -1380410
75
 XDOT =     -15651
452241                 XDOT =       -4782
951220
 YDOT =      -4584
359810  feet/sec       YDOT =       -1450
729369  meter/sec
 ZDOT =      19159
867942                 ZDOT =        5816
723238

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15342883
30                 X    =         4676510
83
 Y    =       15462593
46  feet           Y    =         4712998
49  meter
 Z    =       -4548591
52                 Z    =        -1386410
70
 XDOT =      -7409
455899                 XDOT =       -2258
402158
 YDOT =      12917
939892  feet/sec       YDOT =        3937
388079  meter/sec
 ZDOT =      19057
117608                 ZDOT =        5808
609447


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   17294
13047869  
00016717  00000-0  10270-3 0  9187
2 25544  51
6369 130
4878 0005118  40
5248 319
6285 15
54249367 41332


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
13047869   =   yrday
fracday
Element set:     918
Inclination:       51
6369  deg
RA of node:       130
4878  deg
Eccentricity:     
0005118     
Arg of perigee:    40
5248  deg
Mean anomaly:     319
6285  deg
Mean motion:   15
54249367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4133
Checksum:              333


Coasting Arc #20 (Orbit 4136)
---------------------------------------

Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3286900
96                 A    =         6776974
77  meter
 Y    =        2595347
58  meter          E    =           
0018489
 Z    =       -5343576
15                 I    =           51
91247
 XDOT =      -4741
524531                 Wp   =           77
58222
 YDOT =       6010
227314  meter/sec      RA   =          128
23240  deg
 ZDOT =          6
451060                 TA   =          192
45624
                                          MA   =          192
50200
                                          Ha   =            222
308  n
mi
                                          Hp   =            213
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10783795
78                 X    =         3283591
97
 Y    =        8514919
88  feet           Y    =         2632085
05  meter
 Z    =      -17531417
83                 Z    =        -5327617
21
 XDOT =     -15556
182843                 XDOT =       -4808
411431
 YDOT =      19718
593550  feet/sec       YDOT =        5956
830362  meter/sec
 ZDOT =         21
164894                 ZDOT =         -16
745322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7909558
06                 X    =        -2410833
30
 Y    =      -11344516
37  feet           Y    =        -3457808
59  meter
 Z    =      -17460972
56                 Z    =        -5322104
44
 XDOT =      19844
089457                 XDOT =        6048
478466
 YDOT =     -13688
810331  feet/sec       YDOT =       -4172
349389  meter/sec
 ZDOT =        -82
557799                 ZDOT =         -25
163617


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   17294
38766783  
00016717  00000-0  10270-3 0  9198
2 25544  51
6405 129
2065 0005110  38
2495 321
9019 15
54260956 41379


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
38766783   =   yrday
fracday
Element set:     919
Inclination:       51
6405  deg
RA of node:       129
2065  deg
Eccentricity:     
0005110     
Arg of perigee:    38
2495  deg
Mean anomaly:     321
9019  deg
Mean motion:   15
54260956  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4137
Checksum:              321
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