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

 
Date: September 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) : 76 1 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


255/21:17:02 000 0 0 0 0 0 0
N/A 0 0 0 0 219 2
000/00:00:00 000 0 0 0 0 216 1

256/02:57:42 000 0 0 0 0 0 0
N/A 0 0 0 0 219 4
000/00:00:00 000 0 0 0 0 216 2

256/23:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 3
000/00:00:00 000 0 0 0 0 216 0

260/08:47:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 0

261/05:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 215 9

Coasting Arc #1 (Orbit 3516)
---------------------------------------

Vector Time (GMT): 2017/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4759764
28                 A    =         6779997
29  meter
 Y    =       -1353195
68  meter          E    =           
0006449
 Z    =       -4641237
99                 I    =           51
43160
 XDOT =       4407
893770                 Wp   =           64
22052
 YDOT =      -5556
083335  meter/sec      RA   =          327
46217  deg
 ZDOT =      -2900
934604                 TA   =          176
82094
                                          MA   =          176
81684
                                          Ha   =            219
454  n
mi
                                          Hp   =            216
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15616024
53                 X    =        -4721733
69
 Y    =       -4439618
36  feet           Y    =        -1406210
33  meter
 Z    =      -15227158
76                 Z    =        -4664267
15
 XDOT =      14461
593734                 XDOT =        4483
787194
 YDOT =     -18228
619867  feet/sec       YDOT =       -5506
367147  meter/sec
 ZDOT =      -9517
501982                 ZDOT =       -2879
337482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14488216
56                 X    =         4416008
41
 Y    =        7110199
57  feet           Y    =         2167188
83  meter
 Z    =      -15328843
41                 Z    =        -4672231
47
 XDOT =     -16995
185212                 XDOT =       -5180
132453
 YDOT =      14322
698825  feet/sec       YDOT =        4365
558602  meter/sec
 ZDOT =      -9420
978443                 ZDOT =       -2871
514229


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   17254
52119098  
00016717  00000-0  10270-3 0  9001
2 25544  51
6413 327
9490 0004237 259
4311 100
6365 15
54157674 35179


Satellite: ISS
Catalog Number: 25544
Epoch time:      17254
52119098   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:       327
9490  deg
Eccentricity:     
0004237     
Arg of perigee:   259
4311  deg
Mean anomaly:     100
6365  deg
Mean motion:   15
54157674  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3517
Checksum:              304


Coasting Arc #2 (Orbit 3532)
---------------------------------------

Vector Time (GMT): 2017/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3490867
80                 A    =         6777490
92  meter
 Y    =        2566227
98  meter          E    =           
0002676
 Z    =        5213118
55                 I    =           51
39657
 XDOT =      -5465
692780                 Wp   =          204
23178
 YDOT =       5271
762903  meter/sec      RA   =          322
44974  deg
 ZDOT =       1062
702949                 TA   =          235
54031
                                          MA   =          235
56560
                                          Ha   =            219
242  n
mi
                                          Hp   =            216
094

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11452978
33                 X    =         3436589
17
 Y    =        8419383
13  feet           Y    =         2604962
07  meter
 Z    =       17103407
32                 Z    =         5229944
22
 XDOT =     -17932
062926                 XDOT =       -5529
398933
 YDOT =      17295
810048  feet/sec       YDOT =        5210
285663  meter/sec
 ZDOT =       3486
558230                 ZDOT =        1035
997090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9851521
21                 X    =        -3002743
67
 Y    =      -10122581
21  feet           Y    =        -3085362
75  meter
 Z    =       17177431
30                 Z    =         5235681
06
 XDOT =      19746
343984                 XDOT =        6018
685646
 YDOT =     -13490
963737  feet/sec       YDOT =       -4112
045747  meter/sec
 ZDOT =       3367
482492                 ZDOT =        1026
408664


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   17255
54999143  
00016717  00000-0  10270-3 0  9012
2 25544  51
6413 322
8203 0004231 263
8940  96
1730 15
54199624 35330


Satellite: ISS
Catalog Number: 25544
Epoch time:      17255
54999143   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:       322
8203  deg
Eccentricity:     
0004231     
Arg of perigee:   263
8940  deg
Mean anomaly:      96
1730  deg
Mean motion:   15
54199624  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3533
Checksum:              306


Coasting Arc #3 (Orbit 3538)
---------------------------------------

Vector Time (GMT): 2017/255/21:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3087825
19                 A    =         6777156
57  meter
 Y    =        2920505
63  meter          E    =           
0001864
 Z    =        5280306
13                 I    =           51
38470
 XDOT =      -5664
020573                 Wp   =          242
86505
 YDOT =       5147
652422  meter/sec      RA   =          320
51207  deg
 ZDOT =        464
370876                 TA   =          202
68549
                                          MA   =          202
69373
                                          Ha   =            219
213  n
mi
                                          Hp   =            216
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10130660
07                 X    =         3029288
56
 Y    =        9581711
39  feet           Y    =         2954708
79  meter
 Z    =       17323839
00                 Z    =         5295163
56
 XDOT =     -18582
744663                 XDOT =       -5723
417726
 YDOT =      16888
623433  feet/sec       YDOT =        5083
981400  meter/sec
 ZDOT =       1523
526497                 ZDOT =         436
712130

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -791961
42                 X    =         -241389
84
 Y    =       13840053
95  feet           Y    =         4218448
44  meter
 Z    =       17389093
36                 Z    =         5300195
66
 XDOT =     -23905
453974                 XDOT =       -7286
382371
 YDOT =      -3130
164064  feet/sec       YDOT =        -954
074007  meter/sec
 ZDOT =       1400
257941                 ZDOT =         426
798620


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   17255
93579164  
00016717  00000-0  10270-3 0  9023
2 25544  51
6404 320
8989 0004191 270
3858  89
6815 15
54215159 35394


Satellite: ISS
Catalog Number: 25544
Epoch time:      17255
93579164   =   yrday
fracday
Element set:     902
Inclination:       51
6404  deg
RA of node:       320
8989  deg
Eccentricity:     
0004191     
Arg of perigee:   270
3858  deg
Mean anomaly:      89
6815  deg
Mean motion:   15
54215159  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3539
Checksum:              341


Coasting Arc #4 (Orbit 3541)
---------------------------------------

Vector Time (GMT): 2017/256/02:57:42
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3080019
19                 A    =         6786240
25  meter
 Y    =       -5434893
74  meter          E    =           
0003026
 Z    =       -2646363
79                 I    =           51
40746
 XDOT =       5602
250895                 Wp   =          355
20691
 YDOT =        647
659285  meter/sec      RA   =          319
30094  deg
 ZDOT =       5192
697268                 TA   =          334
85518
                                          MA   =          334
86991
                                          Ha   =            219
361  n
mi
                                          Hp   =            216
161

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10105049
83                 X    =         3153419
49
 Y    =      -17831016
22  feet           Y    =        -5400040
60  meter
 Z    =       -8682295
89                 Z    =        -2631223
38
 XDOT =      18380
088237                 XDOT =        5569
368540
 YDOT =       2124
866420  feet/sec       YDOT =         710
123889  meter/sec
 ZDOT =      17036
408361                 ZDOT =        5219
831480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2209336
09                 X    =         -673405
64
 Y    =      -20404675
08  feet           Y    =        -6219344
97  meter
 Z    =       -8614377
64                 Z    =        -2625662
31
 XDOT =      14563
414759                 XDOT =        4438
928818
 YDOT =      -8816
362492  feet/sec       YDOT =       -2687
227288  meter/sec
 ZDOT =      17156
374927                 ZDOT =        5229
263078


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   17256
12869025  
00016717  00000-0  10270-3 0  9034
2 25544  51
6392 319
9354 0004267 270
1469  89
9195 15
54184668 35423


Satellite: ISS
Catalog Number: 25544
Epoch time:      17256
12869025   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:       319
9354  deg
Eccentricity:     
0004267     
Arg of perigee:   270
1469  deg
Mean anomaly:      89
9195  deg
Mean motion:   15
54184668  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3542
Checksum:              341


Coasting Arc #5 (Orbit 3555)
---------------------------------------

Vector Time (GMT): 2017/256/23:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5078230
58                 A    =         6780489
49  meter
 Y    =           4839
30  meter          E    =           
0005103
 Z    =        4490982
12                 I    =           51
37133
 XDOT =      -2816
741732                 Wp   =          125
90159
 YDOT =       6388
184656  meter/sec      RA   =          315
08759  deg
 ZDOT =       3172
707286                 TA   =          292
09344
                                          MA   =          292
14762
                                          Ha   =            219
301  n
mi
                                          Hp   =            216
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16660861
49                 X    =         5055984
03
 Y    =          15876
98  feet           Y    =           61503
37  meter
 Z    =       14734193
31                 Z    =         4515596
58
 XDOT =      -9241
278647                 XDOT =       -2903
378234
 YDOT =      20958
611075  feet/sec       YDOT =        6356
201668  meter/sec
 ZDOT =      10409
144640                 ZDOT =        3158
813684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15857978
62                 X    =         4833511
88
 Y    =        4784078
19  feet           Y    =         1458187
03  meter
 Z    =       14843116
92                 Z    =         4524182
04
 XDOT =     -14599
396830                 XDOT =       -4449
896154
 YDOT =      16236
506448  feet/sec       YDOT =        4948
887165  meter/sec
 ZDOT =      10346
590440                 ZDOT =        3153
640766


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   17257
02888614  
00016717  00000-0  10270-3 0  9040
2 25544  51
6428 315
4495 0004064 275
3902  84
6787 15
54181985 35567


Satellite: ISS
Catalog Number: 25544
Epoch time:      17257
02888614   =   yrday
fracday
Element set:     904
Inclination:       51
6428  deg
RA of node:       315
4495  deg
Eccentricity:     
0004064     
Arg of perigee:   275
3902  deg
Mean anomaly:      84
6787  deg
Mean motion:   15
54181985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3556
Checksum:              341


Coasting Arc #6 (Orbit 3570)
---------------------------------------

Vector Time (GMT): 2017/257/23:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4150096
85                 A    =         6777668
48  meter
 Y    =       -1478670
00  meter          E    =           
0010189
 Z    =       -5159481
27                 I    =           51
33936
 XDOT =       3972
136389                 Wp   =           71
35858
 YDOT =      -6408
697109  meter/sec      RA   =          310
07161  deg
 ZDOT =      -1357
365488                 TA   =          185
52114
                                          MA   =          185
53238
                                          Ha   =            219
409  n
mi
                                          Hp   =            215
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13615803
32                 X    =        -4108191
38
 Y    =       -4851279
54  feet           Y    =        -1524845
18  meter
 Z    =      -16927432
00                 Z    =        -5179539
23
 XDOT =      13031
943533                 XDOT =        4050
098322
 YDOT =     -21025
909150  feet/sec       YDOT =       -6363
842133  meter/sec
 ZDOT =      -4453
298846                 ZDOT =       -1337
880444

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11681312
87                 X    =        -3560464
16
 Y    =       -8334713
39  feet           Y    =        -2540420
64  meter
 Z    =      -17015946
92                 Z    =        -5186460
62
 XDOT =      17668
022722                 XDOT =        5385
213326
 YDOT =     -15842
057999  feet/sec       YDOT =       -4828
659278  meter/sec
 ZDOT =      -4366
009409                 ZDOT =       -1330
759668


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   17257
99337396  
00016717  00000-0  10270-3 0  9053
2 25544  51
6423 310
6413 0004133 280
4002  79
6685 15
54221990 35713


Satellite: ISS
Catalog Number: 25544
Epoch time:      17257
99337396   =   yrday
fracday
Element set:     905
Inclination:       51
6423  deg
RA of node:       310
6413  deg
Eccentricity:     
0004133     
Arg of perigee:   280
4002  deg
Mean anomaly:      79
6685  deg
Mean motion:   15
54221990  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3571
Checksum:              310


Coasting Arc #7 (Orbit 3586)
---------------------------------------

Vector Time (GMT): 2017/258/23:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3059084
06                 A    =         6777187
47  meter
 Y    =        2978809
81  meter          E    =           
0002596
 Z    =        5264407
32                 I    =           51
31699
 XDOT =      -4775
163404                 Wp   =          326
72509
 YDOT =       5969
302860  meter/sec      RA   =          305
04975  deg
 ZDOT =       -600
886870                 TA   =          129
04798
                                          MA   =          129
02487
                                          Ha   =            219
318  n
mi
                                          Hp   =            216
014

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10036365
04                 X    =         2999975
11
 Y    =        9772998
08  feet           Y    =         3012688
44  meter
 Z    =       17271677
55                 Z    =         5279123
54
 XDOT =     -15666
546600                 XDOT =       -4838
640040
 YDOT =      19584
326967  feet/sec       YDOT =        5915
548767  meter/sec
 ZDOT =      -1971
413617                 ZDOT =        -624
237572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7105785
27                 X    =         2165843
35
 Y    =       11979611
42  feet           Y    =         3651385
56  meter
 Z    =       17336311
20                 Z    =         5284107
65
 XDOT =     -19251
933513                 XDOT =       -5867
989335
 YDOT =      14432
711425  feet/sec       YDOT =        4399
090442  meter/sec
 ZDOT =      -2075
723010                 ZDOT =        -632
680374


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   17259
02215785  
00016717  00000-0  10270-3 0  9067
2 25544  51
6418 305
5127 0004185 282
9342  77
1344 15
54229326 35876


Satellite: ISS
Catalog Number: 25544
Epoch time:      17259
02215785   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:       305
5127  deg
Eccentricity:     
0004185     
Arg of perigee:   282
9342  deg
Mean anomaly:      77
1344  deg
Mean motion:   15
54229326  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3587
Checksum:              317


Coasting Arc #8 (Orbit 3601)
---------------------------------------

Vector Time (GMT): 2017/259/23:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1923244
42                 A    =         6779177
31  meter
 Y    =       -4376910
10  meter          E    =           
0007295
 Z    =       -4813280
40                 I    =           51
30542
 XDOT =       5214
097330                 Wp   =          108
07700
 YDOT =      -5031
194718  meter/sec      RA   =          300
02803  deg
 ZDOT =       2492
568699                 TA   =          186
55013
                                          MA   =          186
55967
                                          Ha   =            219
466  n
mi
                                          Hp   =            215
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6309857
03                 X    =        -1850777
33
 Y    =      -14359941
26  feet           Y    =        -4398012
36  meter
 Z    =      -15791602
35                 Z    =        -4822446
45
 XDOT =      17106
618537                 XDOT =        5257
862377
 YDOT =     -16506
544351  feet/sec       YDOT =       -4972
642200  meter/sec
 ZDOT =       8177
718829                 ZDOT =        2518
003722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2609016
27                 X    =         -795228
16
 Y    =      -15425787
70  feet           Y    =        -4701780
09  meter
 Z    =      -15831456
71                 Z    =        -4825428
00
 XDOT =      19366
798498                 XDOT =        5903
000182
 YDOT =     -11781
676637  feet/sec       YDOT =       -3591
055039  meter/sec
 ZDOT =       8291
084413                 ZDOT =        2527
122529


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   17259
98663973  
00016717  00000-0  10270-3 0  9079
2 25544  51
6416 300
7041 0004268 287
3983  72
6703 15
54227592 36028


Satellite: ISS
Catalog Number: 25544
Epoch time:      17259
98663973   =   yrday
fracday
Element set:     907
Inclination:       51
6416  deg
RA of node:       300
7041  deg
Eccentricity:     
0004268     
Arg of perigee:   287
3983  deg
Mean anomaly:      72
6703  deg
Mean motion:   15
54227592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3602
Checksum:              331


Coasting Arc #9 (Orbit 3607)
---------------------------------------

Vector Time (GMT): 2017/260/08:47:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         351771
76                 A    =         6784931
02  meter
 Y    =       -6003373
74  meter          E    =           
0002050
 Z    =       -3139696
95                 I    =           51
31808
 XDOT =       5542
659867                 Wp   =            8
61926
 YDOT =      -2194
531840  meter/sec      RA   =          298
06216  deg
 ZDOT =       4819
535564                 TA   =          315
01962
                                          MA   =          315
03622
                                          Ha   =            219
454  n
mi
                                          Hp   =            216
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1154106
83                 X    =          434127
94
 Y    =      -19696108
07  feet           Y    =        -5998979
81  meter
 Z    =      -10300843
00                 Z    =        -3137787
55
 XDOT =      18184
579616                 XDOT =        5543
376992
 YDOT =      -7199
907612  feet/sec       YDOT =       -2132
545562  meter/sec
 ZDOT =      15812
124554                 ZDOT =        4846
461843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16396500
56                 X    =        -4997653
37
 Y    =       10982587
57  feet           Y    =         3347492
69  meter
 Z    =      -10291430
51                 Z    =        -3136828
02
 XDOT =     -15893
130256                 XDOT =       -4844
226102
 YDOT =      -8806
083358  feet/sec       YDOT =       -2684
094208  meter/sec
 ZDOT =      15931
628152                 ZDOT =        4855
960261


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   17260
37243091  
00016717  00000-0  10270-3 0  9080
2 25544  51
6416 298
7779 0004199 283
3312  76
7372 15
54205557 36087


Satellite: ISS
Catalog Number: 25544
Epoch time:      17260
37243091   =   yrday
fracday
Element set:     908
Inclination:       51
6416  deg
RA of node:       298
7779  deg
Eccentricity:     
0004199     
Arg of perigee:   283
3312  deg
Mean anomaly:      76
7372  deg
Mean motion:   15
54205557  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3608
Checksum:              331


Coasting Arc #10 (Orbit 3621)
---------------------------------------

Vector Time (GMT): 2017/261/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1655348
15                 A    =         6781030
36  meter
 Y    =        4919697
90  meter          E    =           
0006727
 Z    =        4361216
46                 I    =           51
29041
 XDOT =      -5027
845700                 Wp   =           51
89729
 YDOT =       4698
374271  meter/sec      RA   =          293
72970  deg
 ZDOT =      -3384
006563                 TA   =           72
57774
                                          MA   =           72
50421
                                          Ha   =            219
588  n
mi
                                          Hp   =            215
913

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5430932
26                 X    =         1579027
23
 Y    =       16140741
15  feet           Y    =         4937782
89  meter
 Z    =       14308452
96                 Z    =         4369071
65
 XDOT =     -16495
556759                 XDOT =       -5063
572744
 YDOT =      15414
613750  feet/sec       YDOT =        4641
949324  meter/sec
 ZDOT =     -11102
383738                 ZDOT =       -3408
517440

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16845581
36                 X    =         5134533
20
 Y    =       -2295941
86  feet           Y    =         -699803
08  meter
 Z    =       14342434
10                 Z    =         4371573
91
 XDOT =      11984
120980                 XDOT =        3652
760075
 YDOT =      17735
168782  feet/sec       YDOT =        5405
679445  meter/sec
 ZDOT =     -11211
588197                 ZDOT =       -3417
292082


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   17261
27260958  
00016717  00000-0  10270-3 0  9092
2 25544  51
6397 294
2876 0003828 285
7620  74
3110 15
54194495 36228


Satellite: ISS
Catalog Number: 25544
Epoch time:      17261
27260958   =   yrday
fracday
Element set:     909
Inclination:       51
6397  deg
RA of node:       294
2876  deg
Eccentricity:     
0003828     
Arg of perigee:   285
7620  deg
Mean anomaly:      74
3110  deg
Mean motion:   15
54194495  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3622
Checksum:              334


Coasting Arc #11 (Orbit 3636)
---------------------------------------

Vector Time (GMT): 2017/262/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -652548
10                 A    =         6784846
52  meter
 Y    =       -5966955
75  meter          E    =           
0002460
 Z    =       -3160721
55                 I    =           51
29078
 XDOT =       5111
360538                 Wp   =           16
43110
 YDOT =      -3099
474969  meter/sec      RA   =          288
71965  deg
 ZDOT =       4799
298949                 TA   =          306
90788
                                          MA   =          306
93042
                                          Ha   =            219
633  n
mi
                                          Hp   =            215
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2140905
84                 X    =         -570422
32
 Y    =      -19576626
48  feet           Y    =        -5973794
21  meter
 Z    =      -10369821
35                 Z    =        -3163691
17
 XDOT =      16769
555572                 XDOT =        5122
327231
 YDOT =     -10168
881132  feet/sec       YDOT =       -3042
254307  meter/sec
 ZDOT =      15745
731461                 ZDOT =        4824
155316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19650091
93                 X    =        -5989348
02
 Y    =       -1203436
55  feet           Y    =         -366807
46  meter
 Z    =      -10382032
78                 Z    =        -3164443
59
 XDOT =      -7349
872171                 XDOT =       -2240
241038
 YDOT =     -16688
757970  feet/sec       YDOT =       -5086
733429  meter/sec
 ZDOT =      15856
201057                 ZDOT =        4832
970082


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   17262
23708015  
00016717  00000-0  10270-3 0  9102
2 25544  51
6394 289
4795 0003992 290
6266  69
4458 15
54209162 36378


Satellite: ISS
Catalog Number: 25544
Epoch time:      17262
23708015   =   yrday
fracday
Element set:     910
Inclination:       51
6394  deg
RA of node:       289
4795  deg
Eccentricity:     
0003992     
Arg of perigee:   290
6266  deg
Mean anomaly:      69
4458  deg
Mean motion:   15
54209162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3637
Checksum:              334


Coasting Arc #12 (Orbit 3652)
---------------------------------------

Vector Time (GMT): 2017/263/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -290102
22                 A    =         6787967
36  meter
 Y    =        6585941
71  meter          E    =           
0009983
 Z    =        1597291
17                 I    =           51
29203
 XDOT =      -4990
557333                 Wp   =          118
59355
 YDOT =       1168
992016  meter/sec      RA   =          283
71845  deg
 ZDOT =      -5703
869401                 TA   =           43
84269
                                          MA   =           43
76349
                                          Ha   =            219
685  n
mi
                                          Hp   =            215
849

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -951778
94                 X    =         -371485
28
 Y    =       21607420
30  feet           Y    =         6582242
77  meter
 Z    =        5240456
60                 Z    =         1595683
36
 XDOT =     -16373
219597                 XDOT =       -4975
551771
 YDOT =       3835
275643  feet/sec       YDOT =        1113
267303  meter/sec
 ZDOT =     -18713
482287                 ZDOT =       -5728
075720

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21220155
03                 X    =         6467903
25
 Y    =        4192445
41  feet           Y    =         1277857
36  meter
 Z    =        5232332
45                 Z    =         1594814
93
 XDOT =       1677
143039                 XDOT =         511
193198
 YDOT =      15092
431026  feet/sec       YDOT =        4600
172977  meter/sec
 ZDOT =     -18820
769302                 ZDOT =       -5736
570483


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   17263
26584526  
00016717  00000-0  10270-3 0  9116
2 25544  51
6396 284
3500 0003949 292
8495  67
2240 15
54226367 36537


Satellite: ISS
Catalog Number: 25544
Epoch time:      17263
26584526   =   yrday
fracday
Element set:     911
Inclination:       51
6396  deg
RA of node:       284
3500  deg
Eccentricity:     
0003949     
Arg of perigee:   292
8495  deg
Mean anomaly:      67
2240  deg
Mean motion:   15
54226367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3653
Checksum:              327


Coasting Arc #13 (Orbit 3668)
---------------------------------------

Vector Time (GMT): 2017/264/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1125322
68                 A    =         6789005
19  meter
 Y    =       -6686688
91  meter          E    =           
0011847
 Z    =         122579
96                 I    =           51
28983
 XDOT =       4712
619375                 Wp   =           28
18328
 YDOT =        906
954210  meter/sec      RA   =          278
72281  deg
 ZDOT =       5983
778345                 TA   =          333
14400
                                          MA   =          333
20528
                                          Ha   =            219
820  n
mi
                                          Hp   =            215
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3692003
53                 X    =         1199415
94
 Y    =      -21937955
75  feet           Y    =        -6673690
49  meter
 Z    =         402165
23                 Z    =          128227
37
 XDOT =      15461
349656                 XDOT =        4673
060902
 YDOT =       2975
571554  feet/sec       YDOT =         959
433599  meter/sec
 ZDOT =      19631
818716                 ZDOT =        6006
574695

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21259871
18                 X    =        -6480008
74
 Y    =       -6549891
73  feet           Y    =        -1996407
00  meter
 Z    =         428164
78                 Z    =          130504
63
 XDOT =       4495
337789                 XDOT =        1370
178958
 YDOT =     -13255
510022  feet/sec       YDOT =       -4040
279455  meter/sec
 ZDOT =      19732
548208                 ZDOT =        6014
480694


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   17264
29460492  
00016717  00000-0  10270-3 0  9126
2 25544  51
6406 279
2205 0003921 300
4068  59
6697 15
54238592 36697


Satellite: ISS
Catalog Number: 25544
Epoch time:      17264
29460492   =   yrday
fracday
Element set:     912
Inclination:       51
6406  deg
RA of node:       279
2205  deg
Eccentricity:     
0003921     
Arg of perigee:   300
4068  deg
Mean anomaly:      59
6697  deg
Mean motion:   15
54238592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3669
Checksum:              327


Coasting Arc #14 (Orbit 3683)
---------------------------------------

Vector Time (GMT): 2017/265/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1894353
55                 A    =         6787499
97  meter
 Y    =        6247227
25  meter          E    =           
0003674
 Z    =       -1851381
24                 I    =           51
28033
 XDOT =      -4308
842412                 Wp   =          160
96472
 YDOT =      -2965
263986  meter/sec      RA   =          273
72683  deg
 ZDOT =      -5603
578195                 TA   =           39
50419
                                          MA   =           39
47741
                                          Ha   =            219
888  n
mi
                                          Hp   =            215
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6215070
69                 X    =        -1955077
73
 Y    =       20496152
39  feet           Y    =         6225703
51  meter
 Z    =       -6074085
44                 Z    =        -1860731
84
 XDOT =     -14136
622088                 XDOT =       -4248
144114
 YDOT =      -9728
556385  feet/sec       YDOT =       -3013
109777  meter/sec
 ZDOT =     -18384
442897                 ZDOT =       -5624
361571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19651302
43                 X    =         5989716
98
 Y    =        8487045
41  feet           Y    =         2586851
44  meter
 Z    =       -6116392
19                 Z    =        -1864276
34
 XDOT =     -10655
777604                 XDOT =       -3247
881014
 YDOT =      11373
157956  feet/sec       YDOT =        3466
538545  meter/sec
 ZDOT =     -18475
958581                 ZDOT =       -5631
472176


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   17265
25906286  
00016717  00000-0  10270-3 0  9130
2 25544  51
6399 274
4121 0003912 302
5207  57
5567 15
54249843 36841


Satellite: ISS
Catalog Number: 25544
Epoch time:      17265
25906286   =   yrday
fracday
Element set:     913
Inclination:       51
6399  deg
RA of node:       274
4121  deg
Eccentricity:     
0003912     
Arg of perigee:   302
5207  deg
Mean anomaly:      57
5567  deg
Mean motion:   15
54249843  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3684
Checksum:              325


Coasting Arc #15 (Orbit 3699)
---------------------------------------

Vector Time (GMT): 2017/266/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2577589
70                 A    =         6784048
93  meter
 Y    =       -5293175
60  meter          E    =           
0009636
 Z    =        3360044
08                 I    =           51
26884
 XDOT =       3812
214044                 Wp   =           75
46174
 YDOT =       4793
899800  meter/sec      RA   =          268
72310  deg
 ZDOT =       4618
746434                 TA   =          323
98821
                                          MA   =          324
05309
                                          Ha   =            219
848  n
mi
                                          Hp   =            215
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8456659
12                 X    =         2620266
19
 Y    =      -17366061
68  feet           Y    =        -5264112
20  meter
 Z    =       11023766
66                 Z    =         3372669
66
 XDOT =      12507
263923                 XDOT =        3735
888177
 YDOT =      15728
017718  feet/sec       YDOT =        4836
104384  meter/sec
 ZDOT =      15153
367564                 ZDOT =        4637
079226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16463056
00                 X    =        -5017939
47
 Y    =      -10040460
48  feet           Y    =        -3060332
35  meter
 Z    =       11080413
05                 Z    =         3377309
90
 XDOT =      16133
956441                 XDOT =        4917
629923
 YDOT =      -9611
196422  feet/sec       YDOT =       -2929
492669  meter/sec
 ZDOT =      15233
775101                 ZDOT =        4643
254651


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   17266
28781289  
00016717  00000-0  10270-3 0  9149
2 25544  51
6408 269
2827 0003905 306
2381  53
8410 15
54280164 37009


Satellite: ISS
Catalog Number: 25544
Epoch time:      17266
28781289   =   yrday
fracday
Element set:     914
Inclination:       51
6408  deg
RA of node:       269
2827  deg
Eccentricity:     
0003905     
Arg of perigee:   306
2381  deg
Mean anomaly:      53
8410  deg
Mean motion:   15
54280164  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3700
Checksum:              312


Coasting Arc #16 (Orbit 3714)
---------------------------------------

Vector Time (GMT): 2017/267/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3214845
75                 A    =         6780253
98  meter
 Y    =        3912814
19  meter          E    =           
0008554
 Z    =       -4516981
07                 I    =           51
25786
 XDOT =      -3199
607453                 Wp   =           45
46546
 YDOT =      -6225
690230  meter/sec      RA   =          263
70905  deg
 ZDOT =      -3113
500371                 TA   =          193
12012
                                          MA   =          193
14238
                                          Ha   =            220
086  n
mi
                                          Hp   =            215
472

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10547394
19                 X    =        -3236419
37
 Y    =       12837316
89  feet           Y    =         3876742
48  meter
 Z    =      -14819491
70                 Z    =        -4532650
82
 XDOT =     -10497
399781                 XDOT =       -3114
628268
 YDOT =     -20425
492880  feet/sec       YDOT =       -6260
995612  meter/sec
 ZDOT =     -10214
896229                 ZDOT =       -3128
836197

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11952578
63                 X    =         3643145
97
 Y    =       11450031
69  feet           Y    =         3489969
66  meter
 Z    =      -14889398
97                 Z    =        -4538288
81
 XDOT =     -20365
210761                 XDOT =       -6207
316240
 YDOT =       7879
243437  feet/sec       YDOT =        2401
593400  meter/sec
 ZDOT =     -10281
842457                 ZDOT =       -3133
905581


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   17267
25226265  
00016717  00000-0  10270-3 0  9156
2 25544  51
6410 264
4744 0004039 310
2324  49
8475 15
54250732 37158


Satellite: ISS
Catalog Number: 25544
Epoch time:      17267
25226265   =   yrday
fracday
Element set:     915
Inclination:       51
6410  deg
RA of node:       264
4744  deg
Eccentricity:     
0004039     
Arg of perigee:   310
2324  deg
Mean anomaly:      49
8475  deg
Mean motion:   15
54250732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3715
Checksum:              298


Coasting Arc #17 (Orbit 3730)
---------------------------------------

Vector Time (GMT): 2017/268/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3781246
05                 A    =         6777399
78  meter
 Y    =       -2226085
82  meter          E    =           
0000798
 Z    =        5164619
89                 I    =           51
25361
 XDOT =       2471
297132                 Wp   =           51
42778
 YDOT =       7148
160159  meter/sec      RA   =          258
68519  deg
 ZDOT =       1272
053340                 TA   =           26
29600
                                          MA   =           26
29195
                                          Ha   =            220
009  n
mi
                                          Hp   =            215
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12405662
89                 X    =         3780770
18
 Y    =       -7303431
17  feet           Y    =        -2183803
52  meter
 Z    =       16944290
99                 Z    =         5182987
31
 XDOT =       8107
930223                 XDOT =        2385
001736
 YDOT =      23451
969027  feet/sec       YDOT =        7175
313502  meter/sec
 ZDOT =       4173
403348                 ZDOT =        1283
848021

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6507911
17                 X    =        -1983611
33
 Y    =      -12732470
79  feet           Y    =        -3880857
10  meter
 Z    =       17025887
81                 Z    =         5189490
60
 XDOT =      22988
950915                 XDOT =        7007
032239
 YDOT =      -6102
739845  feet/sec       YDOT =       -1860
115105  meter/sec
 ZDOT =       4224
558668                 ZDOT =        1287
645482


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   17268
28100224  
00016717  00000-0  10270-3 0  9167
2 25544  51
6412 259
3451 0004060 315
6118  44
4709 15
54298588 37312


Satellite: ISS
Catalog Number: 25544
Epoch time:      17268
28100224   =   yrday
fracday
Element set:     916
Inclination:       51
6412  deg
RA of node:       259
3451  deg
Eccentricity:     
0004060     
Arg of perigee:   315
6118  deg
Mean anomaly:      44
4709  deg
Mean motion:   15
54298588  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3731
Checksum:              303


Coasting Arc #18 (Orbit 3745)
---------------------------------------

Vector Time (GMT): 2017/269/05:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905019
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4272241
56                 A    =         6777084
28  meter
 Y    =         413739
39  meter          E    =           
0012036
 Z    =       -5254756
70                 I    =           51
25886
 XDOT =      -1592
822479                 Wp   =           81
76468
 YDOT =      -7459
025740  meter/sec      RA   =          253
65783  deg
 ZDOT =        710
802161                 TA   =          195
04981
                                          MA   =          195
08565
                                          Ha   =            220
272  n
mi
                                          Hp   =            215
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14016540
54                 X    =        -4251025
23
 Y    =        1357412
71  feet           Y    =          366082
47  meter
 Z    =      -17240015
41                 Z    =        -5275458
68
 XDOT =      -5225
795535                 XDOT =       -1512
748058
 YDOT =     -24471
869225  feet/sec       YDOT =       -7476
389985  meter/sec
 ZDOT =       2332
028088                 ZDOT =         703
259736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         711907
21                 X    =          216989
32
 Y    =       13950986
00  feet           Y    =         4252260
53  meter
 Z    =      -17331684
48                 Z    =        -5282697
43
 XDOT =     -23670
449720                 XDOT =       -7214
753075
 YDOT =       4052
339980  feet/sec       YDOT =        1235
153226  meter/sec
 ZDOT =       2299
720274                 ZDOT =         700
954740


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   17269
24544338  
00016717  00000-0  10270-3 0  9173
2 25544  51
6403 254
5373 0004102 319
7921  40
2928 15
54277005 37460


Satellite: ISS
Catalog Number: 25544
Epoch time:      17269
24544338   =   yrday
fracday
Element set:     917
Inclination:       51
6403  deg
RA of node:       254
5373  deg
Eccentricity:     
0004102     
Arg of perigee:   319
7921  deg
Mean anomaly:      40
2928  deg
Mean motion:   15
54277005  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3746
Checksum:              307
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