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

 
Date: October 12th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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


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 9
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 3
000/00:00:00 000 0 0 0 0 213 7

294/08:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 3

299/12:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 212 8

Coasting Arc #1 (Orbit 3983)
---------------------------------------

Vector Time (GMT): 2017/284/12:49:20
768
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -145126
61                 A    =         6777289
49  meter
 Y    =        4219552
43  meter          E    =           
0015954
 Z    =       -5314600
23                 I    =           51
63382
 XDOT =      -7649
846277                 Wp   =           74
41325
 YDOT =        128
664628  meter/sec      RA   =          177
16258  deg
 ZDOT =        316
027114                 TA   =          198
57486
                                          MA   =          198
63316
                                          Ha   =            221
835  n
mi
                                          Hp   =            214
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -476137
18                 X    =         -166483
86
 Y    =       13843675
96  feet           Y    =         4217809
89  meter
 Z    =      -17436352
48                 Z    =        -5315357
28
 XDOT =     -25097
920857                 XDOT =       -7652
251613
 YDOT =        422
128046  feet/sec       YDOT =          43
105392  meter/sec
 ZDOT =       1036
834365                 ZDOT =         278
860107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6980728
53                 X    =        -2127726
06
 Y    =      -11958583
32  feet           Y    =        -3644976
19  meter
 Z    =      -17440245
77                 Z    =        -5315786
91
 XDOT =      20248
268102                 XDOT =        6171
672117
 YDOT =     -13067
817699  feet/sec       YDOT =       -3983
070835  meter/sec
 ZDOT =        872
102178                 ZDOT =         265
816744


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
54990610  
00016717  00000-0  10270-3 0  9003
2 25544  51
6408 178
2528 0004971   5
8276 354
2934 15
54159728 39849


Satellite: ISS
Catalog Number: 25544
Epoch time:      17284
54990610   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       178
2528  deg
Eccentricity:     
0004971     
Arg of perigee:     5
8276  deg
Mean anomaly:     354
2934  deg
Mean motion:   15
54159728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3984
Checksum:              336


Coasting Arc #2 (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    =       -3354725
41                 A    =         6779500
88  meter
 Y    =       -3406000
26  meter          E    =           
0007402
 Z    =        4800144
34                 I    =           51
66756
 XDOT =       6625
376551                 Wp   =           81
07977
 YDOT =      -2884
142769  meter/sec      RA   =          172
88406  deg
 ZDOT =       2581
591873                 TA   =          343
51033
                                          MA   =          343
53440
                                          Ha   =            221
929  n
mi
                                          Hp   =            214
125

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11006316
96                 X    =        -3339706
30
 Y    =      -11174541
54  feet           Y    =        -3443430
89  meter
 Z    =       15748505
06                 Z    =         4783884
57
 XDOT =      21736
799708                 XDOT =        6644
595133
 YDOT =      -9462
410660  feet/sec       YDOT =       -2809
945712  meter/sec
 ZDOT =       8469
789611                 ZDOT =        2613
823096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7429454
84                 X    =         2264497
84
 Y    =       13894737
58  feet           Y    =         4235116
02  meter
 Z    =       15676870
59                 Z    =         4778310
15
 XDOT =     -22472
145649                 XDOT =       -6849
509994
 YDOT =       2289
582049  feet/sec       YDOT =         697
864609  meter/sec
 ZDOT =       8613
017956                 ZDOT =        2625
247873


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
45012676  
00016717  00000-0  10270-3 0  9012
2 25544  51
6390 173
7645 0004843   9
0034 351
1205 15
54171463 39987


Satellite: ISS
Catalog Number: 25544
Epoch time:      17285
45012676   =   yrday
fracday
Element set:     901
Inclination:       51
6390  deg
RA of node:       173
7645  deg
Eccentricity:     
0004843     
Arg of perigee:     9
0034  deg
Mean anomaly:     351
1205  deg
Mean motion:   15
54171463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3998
Checksum:              303


Coasting Arc #3 (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    =        4771094
44                 A    =         6784134
65  meter
 Y    =       -3390250
71  meter          E    =           
0014118
 Z    =        3424131
35                 I    =           51
68948
 XDOT =       5393
955283                 Wp   =           69
03858
 YDOT =       2923
871172  meter/sec      RA   =          172
13226  deg
 ZDOT =      -4600
603511                 TA   =           70
90525
                                          MA   =           70
75242
                                          Ha   =            221
859  n
mi
                                          Hp   =            214
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15653197
00                 X    =         4792017
59
 Y    =      -11122869
77  feet           Y    =        -3336779
92  meter
 Z    =       11234026
75                 Z    =         3447359
10
 XDOT =      17696
703683                 XDOT =        5383
206618
 YDOT =       9592
753189  feet/sec       YDOT =        2984
129745  meter/sec
 ZDOT =     -15093
843541                 ZDOT =       -4574
427294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6517455
22                 X    =        -1986520
35
 Y    =       17998054
27  feet           Y    =         5485806
94  meter
 Z    =       11337415
28                 Z    =         3455644
18
 XDOT =     -18783
182323                 XDOT =       -5725
113972
 YDOT =       2674
835395  feet/sec       YDOT =         815
289828  meter/sec
 ZDOT =     -14978
191727                 ZDOT =       -4565
352838


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
57872925  
00016717  00000-0  10270-3 0  9027
2 25544  51
6405 173
1243 0005056   9
4479 350
6768 15
54174393 40004


Satellite: ISS
Catalog Number: 25544
Epoch time:      17285
57872925   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:       173
1243  deg
Eccentricity:     
0005056     
Arg of perigee:     9
4479  deg
Mean anomaly:     350
6768  deg
Mean motion:   15
54174393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4000
Checksum:              315


Coasting Arc #4 (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    =       -5801735
04                 A    =         6787567
93  meter
 Y    =        2912339
21  meter          E    =           
0011408
 Z    =       -1965059
57                 I    =           51
73324
 XDOT =      -3734
468112                 Wp   =           28
23249
 YDOT =      -3677
843491  meter/sec      RA   =          167
15873  deg
 ZDOT =       5598
106811                 TA   =          310
11303
                                          MA   =          310
21295
                                          Ha   =            221
928  n
mi
                                          Hp   =            214
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19034563
78                 X    =        -5824325
02
 Y    =        9554918
66  feet           Y    =         2847333
82  meter
 Z    =       -6447045
82                 Z    =        -1993297
88
 XDOT =     -12252
191968                 XDOT =       -3720
257027
 YDOT =     -12066
415652  feet/sec       YDOT =       -3719
525061  meter/sec
 ZDOT =      18366
492163                 ZDOT =        5580
000508

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9894824
34                 X    =         3015942
46
 Y    =      -18816717
72  feet           Y    =        -5735335
56  meter
 Z    =       -6572600
27                 Z    =        -2003328
56
 XDOT =      15709
174886                 XDOT =        4788
156505
 YDOT =       1899
188848  feet/sec       YDOT =         578
872761  meter/sec
 ZDOT =      18286
694418                 ZDOT =        5573
784459


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
54324749  
00016717  00000-0  10270-3 0  9032
2 25544  51
6409 168
3158 0005044  11
1531 348
9732 15
54147579 40158


Satellite: ISS
Catalog Number: 25544
Epoch time:      17286
54324749   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:       168
3158  deg
Eccentricity:     
0005044     
Arg of perigee:    11
1531  deg
Mean anomaly:     348
9732  deg
Mean motion:   15
54147579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4015
Checksum:              314


Coasting Arc #5 (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    =         259380
52                 A    =         6777717
17  meter
 Y    =       -4315216
20  meter          E    =           
0007870
 Z    =        5217232
91                 I    =           51
70835
 XDOT =       7521
649218                 Wp   =           35
26237
 YDOT =       -961
045984  meter/sec      RA   =          165
77160  deg
 ZDOT =      -1161
681595                 TA   =           65
90324
                                          MA   =           65
82094
                                          Ha   =            221
932  n
mi
                                          Hp   =            214
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         850985
97                 X    =          282272
17
 Y    =      -14157533
47  feet           Y    =        -4312187
29  meter
 Z    =       17116905
86                 Z    =         5218548
79
 XDOT =      24677
326830                 XDOT =        7537
479791
 YDOT =      -3153
038004  feet/sec       YDOT =        -876
845330  meter/sec
 ZDOT =      -3811
291322                 ZDOT =       -1125
104942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10312441
24                 X    =         3143232
09
 Y    =       -9725990
61  feet           Y    =        -2964481
94  meter
 Z    =       17123289
97                 Z    =         5219178
78
 XDOT =      19330
670802                 XDOT =        5891
988460
 YDOT =      14030
599286  feet/sec       YDOT =        4276
526662  meter/sec
 ZDOT =      -3649
015161                 ZDOT =       -1112
219821


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
86475436  
00016717  00000-0  10270-3 0  9048
2 25544  51
6401 166
7074 0004532  16
5738 343
5562 15
54142597 40201


Satellite: ISS
Catalog Number: 25544
Epoch time:      17286
86475436   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       166
7074  deg
Eccentricity:     
0004532     
Arg of perigee:    16
5738  deg
Mean anomaly:     343
5562  deg
Mean motion:   15
54142597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4020
Checksum:              313


Coasting Arc #6 (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    =       -1970647
54                 A    =         6780086
20  meter
 Y    =        4553128
26  meter          E    =           
0011372
 Z    =       -4630656
48                 I    =           51
74813
 XDOT =      -7056
220756                 Wp   =           86
82053
 YDOT =        -29
261666  meter/sec      RA   =          160
78249  deg
 ZDOT =       2981
044121                 TA   =          212
85091
                                          MA   =          212
92165
                                          Ha   =            221
957  n
mi
                                          Hp   =            213
829

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6465379
07                 X    =        -1998921
73
 Y    =       14938084
85  feet           Y    =         4530932
66  meter
 Z    =      -15192442
51                 Z    =        -4640298
41
 XDOT =     -23150
330564                 XDOT =       -7069
849678
 YDOT =        -96
002840  feet/sec       YDOT =        -108
245097  meter/sec
 ZDOT =       9780
328482                 ZDOT =        2946
733816

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14808132
52                 X    =        -4513518
79
 Y    =        6659446
25  feet           Y    =         2029799
22  meter
 Z    =      -15235773
76                 Z    =        -4643863
84
 XDOT =     -16509
074734                 XDOT =       -5031
965979
 YDOT =     -14734
092263  feet/sec       YDOT =       -4490
951322  meter/sec
 ZDOT =       9628
207105                 ZDOT =        2934
677526


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
82926719  
00016717  00000-0  10270-3 0  9051
2 25544  51
6402 161
9004 0004516  20
0275 340
1054 15
54167240 40357


Satellite: ISS
Catalog Number: 25544
Epoch time:      17287
82926719   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       161
9004  deg
Eccentricity:     
0004516     
Arg of perigee:    20
0275  deg
Mean anomaly:     340
1054  deg
Mean motion:   15
54167240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4035
Checksum:              282


Coasting Arc #7 (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    =        3499569
26                 A    =         6783948
13  meter
 Y    =       -4614615
08  meter          E    =           
0014689
 Z    =        3525007
33                 I    =           51
79106
 XDOT =       6092
310981                 Wp   =           72
32948
 YDOT =       1157
404613  meter/sec      RA   =          155
80303  deg
 ZDOT =      -4513
357376                 TA   =           66
24272
                                          MA   =           66
08873
                                          Ha   =            222
025  n
mi
                                          Hp   =            213
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11481526
44                 X    =         3533788
09
 Y    =      -15139813
24  feet           Y    =        -4575288
82  meter
 Z    =       11564984
69                 Z    =         3542090
90
 XDOT =      19987
896918                 XDOT =        6100
839673
 YDOT =       3797
259228  feet/sec       YDOT =        1225
580229  meter/sec
 ZDOT =     -14807
602941                 ZDOT =       -4483
741932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18587703
69                 X    =         5665532
08
 Y    =       -3710125
03  feet           Y    =        -1130846
11  meter
 Z    =       11641327
63                 Z    =         3548276
66
 XDOT =      12195
009911                 XDOT =        3717
039021
 YDOT =      14843
719860  feet/sec       YDOT =        4524
365813  meter/sec
 ZDOT =     -14676
427759                 ZDOT =       -4473
375181


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
85807970  
00016717  00000-0  10270-3 0  9063
2 25544  51
6399 156
7714 0004451  24
7996 335
3370 15
54143415 40514


Satellite: ISS
Catalog Number: 25544
Epoch time:      17288
85807970   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       156
7714  deg
Eccentricity:     
0004451     
Arg of perigee:    24
7996  deg
Mean anomaly:     335
3370  deg
Mean motion:   15
54143415  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4051
Checksum:              331


Coasting Arc #8 (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    =       -4655389
62                 A    =         6787388
02  meter
 Y    =        4472645
97  meter          E    =           
0010945
 Z    =       -2082822
08                 I    =           51
83318
 XDOT =      -4735
668410                 Wp   =           35
16561
 YDOT =      -2354
526498  meter/sec      RA   =          150
83645  deg
 ZDOT =       5551
961982                 TA   =          301
84663
                                          MA   =          301
95312
                                          Ha   =            222
105  n
mi
                                          Hp   =            213
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15273588
00                 X    =        -4694940
48
 Y    =       14674035
33  feet           Y    =         4420364
85  meter
 Z    =       -6833405
77                 Z    =        -2105533
37
 XDOT =     -15536
969850                 XDOT =       -4735
956564
 YDOT =      -7724
824470  feet/sec       YDOT =       -2407
484973  meter/sec
 ZDOT =      18215
098365                 ZDOT =        5528
956837

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21114404
03                 X    =        -6435670
35
 Y    =        1182012
58  feet           Y    =          360277
43  meter
 Z    =       -6934697
28                 Z    =        -2113695
73
 XDOT =      -6737
765811                 XDOT =       -2053
671019
 YDOT =     -14528
891279  feet/sec       YDOT =       -4428
406062  meter/sec
 ZDOT =      18113
379950                 ZDOT =        5520
958209


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
82258682  
00016717  00000-0  10270-3 0  9072
2 25544  51
6411 151
9636 0004653  25
5193 334
6189 15
54142979 40661


Satellite: ISS
Catalog Number: 25544
Epoch time:      17289
82258682   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       151
9636  deg
Eccentricity:     
0004653     
Arg of perigee:    25
5193  deg
Mean anomaly:     334
6189  deg
Mean motion:   15
54142979  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4066
Checksum:              337


Coasting Arc #9 (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    =        2224043
51                 A    =         6777299
64  meter
 Y    =        3561133
58  meter          E    =           
0017828
 Z    =       -5335053
75                 I    =           51
80523
 XDOT =      -6550
595549                 Wp   =           75
22694
 YDOT =       3961
550444  meter/sec      RA   =          149
32038  deg
 ZDOT =        -82
248266                 TA   =          193
96511
                                          MA   =          194
01448
                                          Ha   =            222
288  n
mi
                                          Hp   =            213
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7296730
69                 X    =         2209972
12
 Y    =       11683509
13  feet           Y    =         3585925
08  meter
 Z    =      -17503457
19                 Z    =        -5324284
47
 XDOT =     -21491
455213                 XDOT =       -6594
008280
 YDOT =      12997
212742  feet/sec       YDOT =        3888
054466  meter/sec
 ZDOT =       -269
843394                 ZDOT =        -114
175368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13461488
70                 X    =         4103061
75
 Y    =       -3191963
44  feet           Y    =         -972910
46  meter
 Z    =      -17456155
64                 Z    =        -5320636
24
 XDOT =       5037
525500                 XDOT =        1535
437772
 YDOT =      23573
155941  feet/sec       YDOT =        7185
097931  meter/sec
 ZDOT =       -411
943201                 ZDOT =        -125
560288


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
14408833  
00016717  00000-0  10270-3 0  9085
2 25544  51
6382 150
3638 0004996  28
0091 332
1330 15
54151246 40712


Satellite: ISS
Catalog Number: 25544
Epoch time:      17290
14408833   =   yrday
fracday
Element set:     908
Inclination:       51
6382  deg
RA of node:       150
3638  deg
Eccentricity:     
0004996     
Arg of perigee:    28
0091  deg
Mean anomaly:     332
1330  deg
Mean motion:   15
54151246  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4071
Checksum:              291


Coasting Arc #10 (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    =        -615426
80                 A    =         6778314
90  meter
 Y    =       -4457973
79  meter          E    =           
0010259
 Z    =        5064834
31                 I    =           51
83531
 XDOT =       6781
840959                 Wp   =           43
59977
 YDOT =      -3064
424876  meter/sec      RA   =          144
33290  deg
 ZDOT =      -1863
696052                 TA   =           64
45058
                                          MA   =           64
34456
                                          Ha   =            222
309  n
mi
                                          Hp   =            213
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2019116
81                 X    =         -590133
74
 Y    =      -14625898
26  feet           Y    =        -4464713
91  meter
 Z    =       16616910
46                 Z    =         5061906
64
 XDOT =      22250
134381                 XDOT =        6824
657220
 YDOT =     -10053
887387  feet/sec       YDOT =       -2988
346511  meter/sec
 ZDOT =      -6114
488359                 ZDOT =       -1830
647031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14563452
35                 X    =        -4438940
28
 Y    =       -2512317
69  feet           Y    =         -765754
43  meter
 Z    =       16604504
25                 Z    =         5061052
89
 XDOT =      -2829
102041                 XDOT =        -862
310302
 YDOT =     -23246
946593  feet/sec       YDOT =       -7085
669322  meter/sec
 ZDOT =      -5967
513296                 ZDOT =       -1818
898053


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
17289156  
00016717  00000-0  10270-3 0  9095
2 25544  51
6369 145
2345 0005053  30
0644 330
0798 15
54174294 40877


Satellite: ISS
Catalog Number: 25544
Epoch time:      17291
17289156   =   yrday
fracday
Element set:     909
Inclination:       51
6369  deg
RA of node:       145
2345  deg
Eccentricity:     
0005053     
Arg of perigee:    30
0644  deg
Mean anomaly:     330
0798  deg
Mean motion:   15
54174294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4087
Checksum:              316


Coasting Arc #11 (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    =        -876644
68                 A    =         6781449
54  meter
 Y    =        5187631
75  meter          E    =           
0010797
 Z    =       -4287209
98                 I    =           51
87115
 XDOT =      -6503
037319                 Wp   =           83
18251
 YDOT =       1864
285688  meter/sec      RA   =          139
35419  deg
 ZDOT =       3594
570506                 TA   =          223
39479
                                          MA   =          223
47985
                                          Ha   =            222
405  n
mi
                                          Hp   =            213
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2876130
85                 X    =         -913763
39
 Y    =       17019789
19  feet           Y    =         5177620
50  meter
 Z    =      -14065649
53                 Z    =        -4291559
26
 XDOT =     -21335
424275                 XDOT =       -6540
861981
 YDOT =       6116
422861  feet/sec       YDOT =        1791
353182  meter/sec
 ZDOT =      11793
210322                 ZDOT =        3562
888006

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15450227
56                 X    =         4709229
36
 Y    =        7659867
82  feet           Y    =         2334727
71  meter
 Z    =      -14085621
84                 Z    =        -4293297
54
 XDOT =        116
620735                 XDOT =          35
546000
 YDOT =      21138
035257  feet/sec       YDOT =        6442
873146  meter/sec
 ZDOT =      11652
438103                 ZDOT =        3551
663134


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
13739294  
00016717  00000-0  10270-3 0  9107
2 25544  51
6364 140
4266 0005123  33
6420 326
5057 15
54153528 41023


Satellite: ISS
Catalog Number: 25544
Epoch time:      17292
13739294   =   yrday
fracday
Element set:     910
Inclination:       51
6364  deg
RA of node:       140
4266  deg
Eccentricity:     
0005123     
Arg of perigee:    33
6420  deg
Mean anomaly:     326
5057  deg
Mean motion:   15
54153528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4102
Checksum:              284


Coasting Arc #12 (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    =        2222213
22                 A    =         6785232
67  meter
 Y    =       -5651160
03  meter          E    =           
0016253
 Z    =        3016877
11                 I    =           51
90852
 XDOT =       5825
950574                 Wp   =           80
81595
 YDOT =       -378
042225  meter/sec      RA   =          134
38577  deg
 ZDOT =      -4974
177333                 TA   =           64
75853
                                          MA   =           64
59016
                                          Ha   =            222
358  n
mi
                                          Hp   =            213
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7290725
80                 X    =         2270585
97
 Y    =      -18540551
28  feet           Y    =        -5626038
97  meter
 Z    =        9897890
77                 Z    =         3027790
23
 XDOT =      19114
011068                 XDOT =        5853
907659
 YDOT =      -1240
296014  feet/sec       YDOT =        -312
736625  meter/sec
 ZDOT =     -16319
479440                 ZDOT =       -4945
808031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15809692
61                 X    =        -4818794
31
 Y    =      -12082414
29  feet           Y    =        -3682719
88  meter
 Z    =        9947052
35                 Z    =         3031861
56
 XDOT =       3254
824562                 XDOT =         992
070526
 YDOT =     -17658
606567  feet/sec       YDOT =       -5382
343282  meter/sec
 ZDOT =     -16193
587629                 ZDOT =       -4935
805509


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
16618991  
00016717  00000-0  10270-3 0  9112
2 25544  51
6366 135
2966 0005129  36
1139 324
0359 15
54197845 41180


Satellite: ISS
Catalog Number: 25544
Epoch time:      17293
16618991   =   yrday
fracday
Element set:     911
Inclination:       51
6366  deg
RA of node:       135
2966  deg
Eccentricity:     
0005129     
Arg of perigee:    36
1139  deg
Mean anomaly:     324
0359  deg
Mean motion:   15
54197845  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4118
Checksum:              326


Coasting Arc #13 (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    =       -3254919
02                 A    =         6788180
63  meter
 Y    =        5767226
14  meter          E    =           
0013498
 Z    =       -1467286
38                 I    =           51
94061
 XDOT =      -4845
217058                 Wp   =           39
25872
 YDOT =      -1266
965014  meter/sec      RA   =          129
42962  deg
 ZDOT =       5807
680152                 TA   =          304
79496
                                          MA   =          304
92191
                                          Ha   =            222
446  n
mi
                                          Hp   =            213
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10678868
19                 X    =        -3312040
22
 Y    =       18921345
62  feet           Y    =         5730507
92  meter
 Z    =       -4813931
70                 Z    =        -1483237
39
 XDOT =     -15896
381424                 XDOT =       -4858
901024
 YDOT =      -4156
709365  feet/sec       YDOT =       -1321
223596  meter/sec
 ZDOT =      19054
068741                 ZDOT =        5784
109827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15491328
42                 X    =         4721756
90
 Y    =       15211192
25  feet           Y    =         4636371
40  meter
 Z    =       -4885474
22                 Z    =        -1489092
54
 XDOT =      -7078
597132                 XDOT =       -2157
556406
 YDOT =      13254
377078  feet/sec       YDOT =        4039
934133  meter/sec
 ZDOT =      18949
677940                 ZDOT =        5775
861836


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
13068389  
00016717  00000-0  10270-3 0  9121
2 25544  51
6367 130
4884 0005184  41
0789 319
0753 15
54198866 41337


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
13068389   =   yrday
fracday
Element set:     912
Inclination:       51
6367  deg
RA of node:       130
4884  deg
Eccentricity:     
0005184     
Arg of perigee:    41
0789  deg
Mean anomaly:     319
0753  deg
Mean motion:   15
54198866  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4133
Checksum:              332


Coasting Arc #14 (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    =        3373448
75                 A    =         6777127
45  meter
 Y    =        2484426
70  meter          E    =           
0018613
 Z    =       -5342686
03                 I    =           51
91226
 XDOT =      -4663
746739                 Wp   =           76
84145
 YDOT =       6069
367433  meter/sec      RA   =          128
23498  deg
 ZDOT =       -118
638661                 TA   =          192
00806
                                          MA   =          192
05249
                                          Ha   =            222
415  n
mi
                                          Hp   =            213
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11067745
25                 X    =         3371369
35
 Y    =        8151006
24  feet           Y    =         2522138
89  meter
 Z    =      -17528497
48                 Z    =        -5326303
66
 XDOT =     -15301
006362                 XDOT =       -4730
693100
 YDOT =      19912
622811  feet/sec       YDOT =        6016
839903  meter/sec
 ZDOT =       -389
234451                 ZDOT =        -141
457361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8288028
24                 X    =        -2526191
01
 Y    =      -11080307
91  feet           Y    =        -3377277
85  meter
 Z    =      -17456158
69                 Z    =        -5320637
17
 XDOT =      19674
024604                 XDOT =        5996
642699
 YDOT =     -13922
519991  feet/sec       YDOT =       -4243
584093  meter/sec
 ZDOT =       -491
289680                 ZDOT =        -149
745094


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
38788128  
00016717  00000-0  10270-3 0  9139
2 25544  51
6402 129
2071 0005169  38
8895 321
2628 15
54211159 41377


Satellite: ISS
Catalog Number: 25544
Epoch time:      17294
38788128   =   yrday
fracday
Element set:     913
Inclination:       51
6402  deg
RA of node:       129
2071  deg
Eccentricity:     
0005169     
Arg of perigee:    38
8895  deg
Mean anomaly:     321
2628  deg
Mean motion:   15
54211159  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4137
Checksum:              320


Coasting Arc #15 (Orbit 4152)
---------------------------------------

Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2193024
91                 A    =         6778109
65  meter
 Y    =       -3909480
90  meter          E    =           
0010420
 Z    =        5079342
10                 I    =           51
93504
 XDOT =       5211
480977                 Wp   =           48
96022
 YDOT =      -5322
939785  meter/sec      RA   =          123
25445  deg
 ZDOT =      -1837
781134                 TA   =           58
80247
                                          MA   =           58
70037
                                          Ha   =            222
437  n
mi
                                          Hp   =            213
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7194963
63                 X    =        -2173818
69
 Y    =      -12826380
92  feet           Y    =        -3933897
13  meter
 Z    =       16664508
20                 Z    =         5068735
65
 XDOT =      17098
034701                 XDOT =        5279
543461
 YDOT =     -17463
713204  feet/sec       YDOT =       -5264
280989  meter/sec
 ZDOT =      -6029
465663                 ZDOT =       -1812
299074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3452527
67                 X    =         1052330
43
 Y    =       14349626
33  feet           Y    =         4373766
11  meter
 Z    =       16617992
04                 Z    =         5065163
97
 XDOT =     -20269
003987                 XDOT =       -6177
992415
 YDOT =      11762
281518  feet/sec       YDOT =        3585
143407  meter/sec
 ZDOT =      -5915
674246                 ZDOT =       -1803
097510


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   17295
41666980  
00016717  00000-0  10270-3 0  9146
2 25544  51
6399 124
0781 0005071  41
6639 318
4899 15
54237512 41530


Satellite: ISS
Catalog Number: 25544
Epoch time:      17295
41666980   =   yrday
fracday
Element set:     914
Inclination:       51
6399  deg
RA of node:       124
0781  deg
Eccentricity:     
0005071     
Arg of perigee:    41
6639  deg
Mean anomaly:     318
4899  deg
Mean motion:   15
54237512  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4153
Checksum:              330


Coasting Arc #16 (Orbit 4167)
---------------------------------------

Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1058996
89                 A    =         6781265
38  meter
 Y    =        5139574
21  meter          E    =           
0011477
 Z    =       -4304674
02                 I    =           51
96275
 XDOT =      -5387
870602                 Wp   =           86
79611
 YDOT =       4101
823793  meter/sec      RA   =          118
28084  deg
 ZDOT =       3580
743460                 TA   =          219
56885
                                          MA   =          219
65269
                                          Ha   =            222
463  n
mi
                                          Hp   =            213
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3474399
25                 X    =         1022356
63
 Y    =       16862120
12  feet           Y    =         5151211
59  meter
 Z    =      -14122946
25                 Z    =        -4299618
81
 XDOT =     -17676
740821                 XDOT =       -5450
731800
 YDOT =      13457
427143  feet/sec       YDOT =        4041
221614  meter/sec
 ZDOT =      11747
845999                 ZDOT =        3554
417321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         963145
82                 X    =          293566
85
 Y    =      -17207194
65  feet           Y    =        -5244752
93  meter
 Z    =      -14101239
60                 Z    =        -4298057
83
 XDOT =      19398
804380                 XDOT =        5912
755575
 YDOT =      -8421
506713  feet/sec       YDOT =       -2566
875246  meter/sec
 ZDOT =      11630
458527                 ZDOT =        3544
963759


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   17296
38115804  
00016717  00000-0  10270-3 0  9158
2 25544  51
6402 119
2693 0005072  44
5683 315
5877 15
54211361 41689


Satellite: ISS
Catalog Number: 25544
Epoch time:      17296
38115804   =   yrday
fracday
Element set:     915
Inclination:       51
6402  deg
RA of node:       119
2693  deg
Eccentricity:     
0005072     
Arg of perigee:    44
5683  deg
Mean anomaly:     315
5877  deg
Mean motion:   15
54211361  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4168
Checksum:              311


Coasting Arc #17 (Orbit 4183)
---------------------------------------

Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          35140
38                 A    =         6785111
20  meter
 Y    =       -6064704
25  meter          E    =           
0016986
 Z    =        3030366
21                 I    =           51
99093
 XDOT =       5294
696094                 Wp   =           83
08131
 YDOT =      -2466
612813  meter/sec      RA   =          113
31808  deg
 ZDOT =      -4972
053427                 TA   =           62
35742
                                          MA   =           62
18509
                                          Ha   =            222
499  n
mi
                                          Hp   =            212
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         115289
96                 X    =           88234
52
 Y    =      -19897323
65  feet           Y    =        -6064014
33  meter
 Z    =        9942146
35                 Z    =         3030666
06
 XDOT =      17371
050177                 XDOT =        5346
037286
 YDOT =      -8092
561723  feet/sec       YDOT =       -2407
116990  meter/sec
 ZDOT =     -16312
511243                 ZDOT =       -4946
208034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4916867
43                 X    =        -1498661
19
 Y    =       19279457
33  feet           Y    =         5876378
59  meter
 Z    =        9944344
82                 Z    =         3031036
30
 XDOT =     -17521
040642                 XDOT =       -5340
413188
 YDOT =       3929
895769  feet/sec       YDOT =        1197
832230  meter/sec
 ZDOT =     -16197
471187                 ZDOT =       -4936
989218


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   17297
40993964  
00016717  00000-0  10270-3 0  9164
2 25544  51
6407 114
1395 0005240  47
2417 312
9171 15
54240173 41848


Satellite: ISS
Catalog Number: 25544
Epoch time:      17297
40993964   =   yrday
fracday
Element set:     916
Inclination:       51
6407  deg
RA of node:       114
1395  deg
Eccentricity:     
0005240     
Arg of perigee:    47
2417  deg
Mean anomaly:     312
9171  deg
Mean motion:   15
54240173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4184
Checksum:              306


Coasting Arc #18 (Orbit 4198)
---------------------------------------

Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -960545
89                 A    =         6788193
10  meter
 Y    =        6550940
15  meter          E    =           
0013429
 Z    =       -1475801
48                 I    =           52
01139
 XDOT =      -4971
077684                 Wp   =           42
83087
 YDOT =        571
016072  meter/sec      RA   =          108
36653  deg
 ZDOT =       5810
663110                 TA   =          301
14496
                                          MA   =          301
27660
                                          Ha   =            222
582  n
mi
                                          Hp   =            213
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3151397
27                 X    =        -1026559
98
 Y    =       21492585
80  feet           Y    =         6539829
53  meter
 Z    =       -4841868
36                 Z    =        -1480628
11
 XDOT =     -16309
309988                 XDOT =       -5005
319450
 YDOT =       1873
412310  feet/sec       YDOT =         515
234765  meter/sec
 ZDOT =      19063
855349                 ZDOT =        5786
431441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7936965
44                 X    =         2419187
07
 Y    =      -20215093
04  feet           Y    =        -6161560
36  meter
 Z    =       -4864240
03                 Z    =        -1482620
36
 XDOT =      14954
685726                 XDOT =        4558
188209
 YDOT =       1342
077681  feet/sec       YDOT =         409
065277  meter/sec
 ZDOT =      18956
237020                 ZDOT =        5777
861044


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   17298
37442099  
00016717  00000-0  10270-3 0  9170
2 25544  51
6392 109
3310 0005173  50
8310 309
3302 15
54197227 41994


Satellite: ISS
Catalog Number: 25544
Epoch time:      17298
37442099   =   yrday
fracday
Element set:     917
Inclination:       51
6392  deg
RA of node:       109
3310  deg
Eccentricity:     
0005173     
Arg of perigee:    50
8310  deg
Mean anomaly:     309
3302  deg
Mean motion:   15
54197227  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4199
Checksum:              308


Coasting Arc #19 (Orbit 4214)
---------------------------------------

Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1792930
86                 A    =         6789108
05  meter
 Y    =       -6538162
06  meter          E    =           
0013268
 Z    =        -289928
04                 I    =           52
02445
 XDOT =       4487
637835                 Wp   =          115
01556
 YDOT =       1488
431210  meter/sec      RA   =          103
42196  deg
 ZDOT =      -6034
550685                 TA   =           68
09151
                                          MA   =           67
95050
                                          Ha   =            222
583  n
mi
                                          Hp   =            213
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5882319
11                 X    =         1867317
44
 Y    =      -21450662
91  feet           Y    =        -6517696
36  meter
 Z    =        -951207
47                 Z    =         -281037
55
 XDOT =      14723
221245                 XDOT =        4499
973732
 YDOT =       4883
304494  feet/sec       YDOT =        1538
683887  meter/sec
 ZDOT =     -19798
394637                 ZDOT =       -6012
720773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10285750
13                 X    =        -3135096
64
 Y    =       19723367
49  feet           Y    =         6011682
41  meter
 Z    =        -910786
51                 Z    =         -277607
73
 XDOT =     -12048
670447                 XDOT =       -3672
434752
 YDOT =      -7158
246965  feet/sec       YDOT =       -2181
833675  meter/sec
 ZDOT =     -19701
729737                 ZDOT =       -6005
087224


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   17299
40319812  
00016717  00000-0  10270-3 0  9182
2 25544  51
6399 104
2021 0005005  55
7627 304
3999 15
54192270 42152


Satellite: ISS
Catalog Number: 25544
Epoch time:      17299
40319812   =   yrday
fracday
Element set:     918
Inclination:       51
6399  deg
RA of node:       104
2021  deg
Eccentricity:     
0005005     
Arg of perigee:    55
7627  deg
Mean anomaly:     304
3999  deg
Mean motion:   15
54192270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4215
Checksum:              308


Coasting Arc #20 (Orbit 4216)
---------------------------------------

Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920119
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2907881
27                 A    =         6787334
80  meter
 Y    =       -5802210
61  meter          E    =           
0009174
 Z    =       -1988508
70                 I    =           52
01776
 XDOT =       3642
655501                 Wp   =          106
55704
 YDOT =       3739
740744  meter/sec      RA   =          102
77769  deg
 ZDOT =      -5609
165706                 TA   =           95
26146
                                          MA   =           95
15677
                                          Ha   =            222
585  n
mi
                                          Hp   =            212
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9540292
87                 X    =         2982206
40
 Y    =      -19036124
06  feet           Y    =        -5769277
16  meter
 Z    =       -6523978
68                 Z    =        -1974202
19
 XDOT =      11950
969493                 XDOT =        3627
813094
 YDOT =      12269
490631  feet/sec       YDOT =        3780
392297  meter/sec
 ZDOT =     -18402
774625                 ZDOT =       -5591
506602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3230293
34                 X    =          984593
41
 Y    =       21066369
61  feet           Y    =         6421029
46  meter
 Z    =       -6459627
04                 Z    =        -1968894
32
 XDOT =     -15412
236666                 XDOT =       -4697
649736
 YDOT =      -3231
444324  feet/sec       YDOT =        -984
944230  meter/sec
 ZDOT =     -18324
952464                 ZDOT =       -5585
445511


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   17299
53179500  
00016717  00000-0  10270-3 0  9195
2 25544  51
6376 103
5564 0005160  59
0881 301
0778 15
54247254 42176


Satellite: ISS
Catalog Number: 25544
Epoch time:      17299
53179500   =   yrday
fracday
Element set:     919
Inclination:       51
6376  deg
RA of node:       103
5564  deg
Eccentricity:     
0005160     
Arg of perigee:    59
0881  deg
Mean anomaly:     301
0778  deg
Mean motion:   15
54247254  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4217
Checksum:              315
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