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

 
Date: June 16th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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


167/16:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 216 4

Coasting Arc #1 (Orbit 2164)
---------------------------------------

Vector Time (GMT): 2017/167/12:54:23
898
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2877030
12                 A    =         6777620
83  meter
 Y    =        3043560
48  meter          E    =           
0002892
 Z    =        5330788
38                 I    =           51
87065
 XDOT =      -5708
941585                 Wp   =          306
68796
 YDOT =      -5115
291245  meter/sec      RA   =           40
92806  deg
 ZDOT =       -158
970346                 TA   =          144
83201
                                          MA   =          144
81291
                                          Ha   =            219
706  n
mi
                                          Hp   =            216
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9439075
21                 X    =        -2936744
53
 Y    =        9985434
64  feet           Y    =         3011053
20  meter
 Z    =       17489463
20                 Z    =         5316667
91
 XDOT =     -18730
123311                 XDOT =       -5650
544556
 YDOT =     -16782
451592  feet/sec       YDOT =       -5178
805967  meter/sec
 ZDOT =       -521
556253                 ZDOT =        -186
561236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11179863
08                 X    =         3407622
27
 Y    =        8124868
85  feet           Y    =         2476460
02  meter
 Z    =       17426518
20                 Z    =         5311602
75
 XDOT =     -13522
135642                 XDOT =       -4121
546944
 YDOT =      19995
932784  feet/sec       YDOT =        6094
760312  meter/sec
 ZDOT =       -642
439070                 ZDOT =        -195
815429


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   17167
58568477  
00016717  00000-0  10270-3 0  9009
2 25544  51
6419  41
3343 0004929 286
0454  74
0156 15
54039366 21658


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
58568477   =   yrday
fracday
Element set:     900
Inclination:       51
6419  deg
RA of node:        41
3343  deg
Eccentricity:     
0004929     
Arg of perigee:   286
0454  deg
Mean anomaly:      74
0156  deg
Mean motion:   15
54039366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2165
Checksum:              321


Coasting Arc #2 (Orbit 2166)
---------------------------------------

Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3161559
63                 A    =         6786505
60  meter
 Y    =       -5389202
36  meter          E    =           
0001765
 Z    =       -2646131
84                 I    =           51
89430
 XDOT =       5553
273591                 Wp   =          194
44427
 YDOT =       -685
983303  meter/sec      RA   =           40
20332  deg
 ZDOT =      -5238
786337                 TA   =           15
26527
                                          MA   =           15
25995
                                          Ha   =            219
581  n
mi
                                          Hp   =            216
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10372570
97                 X    =        -3088207
58
 Y    =      -17681110
09  feet           Y    =        -5424146
68  meter
 Z    =       -8681534
89                 Z    =        -2661312
04
 XDOT =      18219
401545                 XDOT =        5585
979152
 YDOT =      -2250
601388  feet/sec       YDOT =        -623
699489  meter/sec
 ZDOT =     -17187
619216                 ZDOT =       -5211
730885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         724410
80                 X    =          220800
41
 Y    =       20458164
84  feet           Y    =         6235648
64  meter
 Z    =       -8747551
14                 Z    =        -2666253
59
 XDOT =     -15724
216624                 XDOT =       -4792
741227
 YDOT =      -6739
918329  feet/sec       YDOT =       -2054
327107  meter/sec
 ZDOT =     -17067
995552                 ZDOT =       -5202
325044


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   17167
71429694  
00016717  00000-0  10270-3 0  9012
2 25544  51
6392  40
6887 0004635 284
4755  75
5883 15
54062677 21679


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
71429694   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:        40
6887  deg
Eccentricity:     
0004635     
Arg of perigee:   284
4755  deg
Mean anomaly:      75
5883  deg
Mean motion:   15
54062677  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2167
Checksum:              345


Coasting Arc #3 (Orbit 2182)
---------------------------------------

Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1920617
60                 A    =         6782836
98  meter
 Y    =        5160405
13  meter          E    =           
0006371
 Z    =        3955930
66                 I    =           51
85635
 XDOT =      -6480
675182                 Wp   =           96
28823
 YDOT =       -691
444752  meter/sec      RA   =           35
23752  deg
 ZDOT =       4042
101637                 TA   =          311
60478
                                          MA   =          311
65935
                                          Ha   =            219
603  n
mi
                                          Hp   =            216
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6301238
84                 X    =         1843553
83
 Y    =       16930463
02  feet           Y    =         5181451
55  meter
 Z    =       12978775
13                 Z    =         3965073
72
 XDOT =     -21262
057684                 XDOT =       -6492
096206
 YDOT =      -2268
519529  feet/sec       YDOT =        -763
980261  meter/sec
 ZDOT =      13261
488312                 ZDOT =        4010
592640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2224823
81                 X    =          678126
30
 Y    =      -17898948
08  feet           Y    =        -5455599
37  meter
 Z    =       13018164
60                 Z    =         3967936
57
 XDOT =      16636
480468                 XDOT =        5070
799247
 YDOT =      11626
949819  feet/sec       YDOT =        3543
894305  meter/sec
 ZDOT =      13122
465690                 ZDOT =        3999
727542


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   17168
74318651  
00016717  00000-0  10270-3 0  9027
2 25544  51
6390  35
5595 0004641 285
9157  74
1484 15
54064415 21837


Satellite: ISS
Catalog Number: 25544
Epoch time:      17168
74318651   =   yrday
fracday
Element set:     902
Inclination:       51
6390  deg
RA of node:        35
5595  deg
Eccentricity:     
0004641     
Arg of perigee:   285
9157  deg
Mean anomaly:      74
1484  deg
Mean motion:   15
54064415  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2183
Checksum:              318


Coasting Arc #4 (Orbit 2197)
---------------------------------------

Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -433419
65                 A    =         6779437
47  meter
 Y    =       -4695276
71  meter          E    =           
0008802
 Z    =       -4879182
95                 I    =           51
81832
 XDOT =       7017
514618                 Wp   =           54
02689
 YDOT =       1880
834182  meter/sec      RA   =           30
26229  deg
 ZDOT =      -2431
334578                 TA   =          192
15077
                                          MA   =          192
17201
                                          Ha   =            219
776  n
mi
                                          Hp   =            216
339

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1421980
49                 X    =         -357182
81
 Y    =      -15404451
15  feet           Y    =        -4699696
81  meter
 Z    =      -16007818
06                 Z    =        -4881103
62
 XDOT =      23023
341921                 XDOT =        7007
771378
 YDOT =       6170
715820  feet/sec       YDOT =        1959
254524  meter/sec
 ZDOT =      -7976
819482                 ZDOT =       -2397
268962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5634900
72                 X    =        -1717517
74
 Y    =       14398764
31  feet           Y    =         4388743
36  meter
 Z    =      -16015394
57                 Z    =        -4881492
26
 XDOT =     -16913
637005                 XDOT =       -5155
276559
 YDOT =     -15331
789712  feet/sec       YDOT =       -4673
129504  meter/sec
 ZDOT =      -7826
744579                 ZDOT =       -2385
591748


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   17169
70776940  
00016717  00000-0  10270-3 0  9034
2 25544  51
6395  30
7533 0004513 290
7798  69
2871 15
54060972 21989


Satellite: ISS
Catalog Number: 25544
Epoch time:      17169
70776940   =   yrday
fracday
Element set:     903
Inclination:       51
6395  deg
RA of node:        30
7533  deg
Eccentricity:     
0004513     
Arg of perigee:   290
7798  deg
Mean anomaly:      69
2871  deg
Mean motion:   15
54060972  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2198
Checksum:              337


Coasting Arc #5 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1191638
30                 A    =         6777705
69  meter
 Y    =        4053257
77  meter          E    =           
0001826
 Z    =        5301176
48                 I    =           51
78396
 XDOT =      -7096
579978                 Wp   =          297
43372
 YDOT =      -2844
919743  meter/sec      RA   =           25
27524  deg
 ZDOT =        580
965749                 TA   =          147
03797
                                          MA   =          147
02658
                                          Ha   =            219
975  n
mi
                                          Hp   =            216
378

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3909574
47                 X    =        -1262625
06
 Y    =       13298089
79  feet           Y    =         4039534
63  meter
 Z    =       17392311
29                 Z    =         5295215
81
 XDOT =     -23282
742711                 XDOT =       -7067
061976
 YDOT =      -9333
726192  feet/sec       YDOT =       -2924
113523  meter/sec
 ZDOT =       1906
055608                 ZDOT =         546
563875

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9316379
40                 X    =         2839632
44
 Y    =      -10308794
76  feet           Y    =        -3142120
64  meter
 Z    =       17365203
21                 Z    =         5292913
94
 XDOT =      16328
014294                 XDOT =        4976
778757
 YDOT =      17706
530579  feet/sec       YDOT =        5396
950520  meter/sec
 ZDOT =       1754
693754                 ZDOT =         534
830656


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   17170
73665493  
00016717  00000-0  10270-3 0  9040
2 25544  51
6399  25
6239 0004625 294
6694  65
3977 15
54038250 22148


Satellite: ISS
Catalog Number: 25544
Epoch time:      17170
73665493   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:        25
6239  deg
Eccentricity:     
0004625     
Arg of perigee:   294
6694  deg
Mean anomaly:      65
3977  deg
Mean motion:   15
54038250  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2214
Checksum:              332


Coasting Arc #6 (Orbit 2228)
---------------------------------------

Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2822058
70                 A    =         6778142
36  meter
 Y    =       -3324271
14  meter          E    =           
0009662
 Z    =       -5197650
85                 I    =           51
75668
 XDOT =       6646
801247                 Wp   =           91
62572
 YDOT =       3571
532433  meter/sec      RA   =           20
28638  deg
 ZDOT =       1326
483474                 TA   =          191
09923
                                          MA   =          191
12056
                                          Ha   =            220
005  n
mi
                                          Hp   =            216
342

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9258722
76                 X    =         2884269
72
 Y    =      -10906401
36  feet           Y    =        -3292364
51  meter
 Z    =      -17052660
26                 Z    =        -5183791
31
 XDOT =      21807
090706                 XDOT =        6599
925958
 YDOT =      11717
626091  feet/sec       YDOT =        3645
599218  meter/sec
 ZDOT =       4351
979901                 ZDOT =        1358
658470

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13027406
63                 X    =        -3970753
54
 Y    =        6088164
41  feet           Y    =         1855672
51  meter
 Z    =      -16990811
94                 Z    =        -5178799
48
 XDOT =     -14586
424146                 XDOT =       -4445
942080
 YDOT =     -18688
996067  feet/sec       YDOT =       -5696
406001  meter/sec
 ZDOT =       4493
355527                 ZDOT =        1369
574765


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   17171
70123032  
00016717  00000-0  10270-3 0  9057
2 25544  51
6408  20
8171 0004566 298
4049  61
6643 15
54070411 22291


Satellite: ISS
Catalog Number: 25544
Epoch time:      17171
70123032   =   yrday
fracday
Element set:     905
Inclination:       51
6408  deg
RA of node:        20
8171  deg
Eccentricity:     
0004566     
Arg of perigee:   298
4049  deg
Mean anomaly:      61
6643  deg
Mean motion:   15
54070411  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2229
Checksum:              282


Coasting Arc #7 (Orbit 2244)
---------------------------------------

Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4330093
46                 A    =         6780913
30  meter
 Y    =        2541897
09  meter          E    =           
0007205
 Z    =        4556727
28                 I    =           51
73402
 XDOT =      -5686
052031                 Wp   =           36
35307
 YDOT =      -4097
882820  meter/sec      RA   =           15
29828  deg
 ZDOT =      -3109
126559                 TA   =           84
78303
                                          MA   =           84
70081
                                          Ha   =            220
246  n
mi
                                          Hp   =            216
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14206343
36                 X    =        -4380330
35
 Y    =        8339557
37  feet           Y    =         2493193
52  meter
 Z    =       14949892
65                 Z    =         4535571
16
 XDOT =     -18655
026350                 XDOT =       -5624
703075
 YDOT =     -13444
497442  feet/sec       YDOT =       -4161
124653  meter/sec
 ZDOT =     -10200
546453                 ZDOT =       -3136
599466

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16436540
56                 X    =         5009857
56
 Y    =       -2001936
21  feet           Y    =         -610190
16  meter
 Z    =       14855978
07                 Z    =         4528102
12
 XDOT =      11606
658953                 XDOT =        3537
709649
 YDOT =      18503
384051  feet/sec       YDOT =        5639
831459  meter/sec
 ZDOT =     -10321
047036                 ZDOT =       -3145
855137


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   17172
73010971  
00016717  00000-0  10270-3 0  9069
2 25544  51
6402  15
6882 0004508 302
0442  58
0272 15
54032641 22450


Satellite: ISS
Catalog Number: 25544
Epoch time:      17172
73010971   =   yrday
fracday
Element set:     906
Inclination:       51
6402  deg
RA of node:        15
6882  deg
Eccentricity:     
0004508     
Arg of perigee:   302
0442  deg
Mean anomaly:      58
0272  deg
Mean motion:   15
54032641  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2245
Checksum:              273


Coasting Arc #8 (Orbit 2259)
---------------------------------------

Vector Time (GMT): 2017/173/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5554385
50                 A    =         6784556
49  meter
 Y    =       -1771383
18  meter          E    =           
0002889
 Z    =       -3468253
34                 I    =           51
71520
 XDOT =       4265
357468                 Wp   =           21
51441
 YDOT =       4440
465669  meter/sec      RA   =           10
31774  deg
 ZDOT =       4566
840100                 TA   =          297
84249
                                          MA   =          297
87177
                                          Ha   =            220
336  n
mi
                                          Hp   =            216
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18223049
53                 X    =         5590627
93
 Y    =       -5811624
59  feet           Y    =        -1709067
08  meter
 Z    =      -11378783
93                 Z    =        -3441183
93
 XDOT =      13993
954949                 XDOT =        4193
202397
 YDOT =      14568
456918  feet/sec       YDOT =        4487
759617  meter/sec
 ZDOT =      14983
071194                 ZDOT =        4587
385471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19133749
88                 X    =        -5831966
96
 Y    =       -1570914
15  feet           Y    =         -478814
63  meter
 Z    =      -11258911
26                 Z    =        -3431716
15
 XDOT =      -7436
627028                 XDOT =       -2266
683918
 YDOT =     -17359
951105  feet/sec       YDOT =       -5291
313097  meter/sec
 ZDOT =      15072
909663                 ZDOT =        4594
222865


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   17173
69467980  
00016717  00000-0  10270-3 0  9072
2 25544  51
6406  10
8807 0004719 305
7545  54
3169 15
54051976 22609


Satellite: ISS
Catalog Number: 25544
Epoch time:      17173
69467980   =   yrday
fracday
Element set:     907
Inclination:       51
6406  deg
RA of node:        10
8807  deg
Eccentricity:     
0004719     
Arg of perigee:   305
7545  deg
Mean anomaly:      54
3169  deg
Mean motion:   15
54051976  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2260
Checksum:              325


Coasting Arc #9 (Orbit 2275)
---------------------------------------

Vector Time (GMT): 2017/174/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6403388
58                 A    =         6787878
91  meter
 Y    =         994059
81  meter          E    =           
0009589
 Z    =        2008029
67                 I    =           51
69472
 XDOT =      -2475
181225                 Wp   =          103
51662
 YDOT =      -4650
916608  meter/sec      RA   =            5
34424  deg
 ZDOT =      -5570
516705                 TA   =           54
32339
                                          MA   =           54
23417
                                          Ha   =            220
358  n
mi
                                          Hp   =            216
123

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21008492
73                 X    =        -6423782
54
 Y    =        3261351
09  feet           Y    =          922338
41  meter
 Z    =        6588023
85                 Z    =         1976874
59
 XDOT =      -8120
673310                 XDOT =       -2395
930632
 YDOT =     -15258
912756  feet/sec       YDOT =       -4678
151695  meter/sec
 ZDOT =     -18275
973440                 ZDOT =       -5582
348688

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20795451
58                 X    =         6338453
64
 Y    =        4619362
20  feet           Y    =         1407981
60  meter
 Z    =        6450265
27                 Z    =         1966040
86
 XDOT =       2238
348162                 XDOT =         682
248520
 YDOT =      15609
153475  feet/sec       YDOT =        4757
669979  meter/sec
 ZDOT =     -18327
294131                 ZDOT =       -5586
159251


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   17174
72355232  
00016717  00000-0  10270-3 0  9084
2 25544  51
6411   5
7518 0004657 309
3300  50
7439 15
54064083 22767


Satellite: ISS
Catalog Number: 25544
Epoch time:      17174
72355232   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:         5
7518  deg
Eccentricity:     
0004657     
Arg of perigee:   309
3300  deg
Mean anomaly:      50
7439  deg
Mean motion:   15
54064083  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2276
Checksum:              295


Coasting Arc #10 (Orbit 2290)
---------------------------------------

Vector Time (GMT): 2017/175/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6767583
59                 A    =         6789458
32  meter
 Y    =        -242917
22  meter          E    =           
0012569
 Z    =        -363385
36                 I    =           51
66813
 XDOT =        488
869961                 Wp   =           20
47159
 YDOT =       4750
001590  meter/sec      RA   =             
37591  deg
 ZDOT =       6003
485624                 TA   =          335
61157
                                          MA   =          335
67099
                                          Ha   =            220
566  n
mi
                                          Hp   =            215
909

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22203358
25                 X    =         6771562
12
 Y    =        -796972
50  feet           Y    =         -167215
21  meter
 Z    =       -1192209
20                 Z    =         -330501
07
 XDOT =       1603
904073                 XDOT =         406
556024
 YDOT =      15583
994719  feet/sec       YDOT =        4755
007202  meter/sec
 ZDOT =      19696
475144                 ZDOT =        6005
661270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21102032
91                 X    =        -6431899
63
 Y    =       -6975221
64  feet           Y    =        -2126047
56  meter
 Z    =       -1046964
85                 Z    =         -319114
89
 XDOT =       3527
387563                 XDOT =        1075
147729
 YDOT =     -13587
433444  feet/sec       YDOT =       -4141
449714  meter/sec
 ZDOT =      19705
139791                 ZDOT =        6006
126608


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   17175
68811711  
00016717  00000-0  10270-3 0  9090
2 25544  51
6416    
9440 0004699 315
4590  44
6184 15
54069562 22911


Satellite: ISS
Catalog Number: 25544
Epoch time:      17175
68811711   =   yrday
fracday
Element set:     909
Inclination:       51
6416  deg
RA of node:          
9440  deg
Eccentricity:     
0004699     
Arg of perigee:   315
4590  deg
Mean anomaly:      44
6184  deg
Mean motion:   15
54069562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2291
Checksum:              315


Coasting Arc #11 (Orbit 2306)
---------------------------------------

Vector Time (GMT): 2017/176/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6631997
47                 A    =         6788641
52  meter
 Y    =        -531292
89  meter          E    =           
0003994
 Z    =       -1339790
29                 I    =           51
63274
 XDOT =       1552
762743                 Wp   =          147
24843
 YDOT =      -4744
135929  meter/sec      RA   =          355
40699  deg
 ZDOT =      -5816
332593                 TA   =           47
33469
                                          MA   =           47
30105
                                          Ha   =            220
585  n
mi
                                          Hp   =            215
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21758521
87                 X    =        -6619055
53
 Y    =       -1743086
90  feet           Y    =         -605383
81  meter
 Z    =       -4395637
44                 Z    =        -1371974
81
 XDOT =       5094
365954                 XDOT =        1633
950119
 YDOT =     -15564
750423  feet/sec       YDOT =       -4726
317028  meter/sec
 ZDOT =     -19082
456013                 ZDOT =       -5808
593379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19922520
16                 X    =         6072384
14
 Y    =        8848519
08  feet           Y    =         2697028
62  meter
 Z    =       -4537637
63                 Z    =        -1383071
95
 XDOT =      -9439
163072                 XDOT =       -2877
056904
 YDOT =      11503
207970  feet/sec       YDOT =        3506
177789  meter/sec
 ZDOT =     -19047
347110                 ZDOT =       -5805
631399


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   17176
71698414  
00016717  00000-0  10270-3 0  9100
2 25544  51
6412 355
8157 0004676 317
9083  42
1710 15
54084816 23078


Satellite: ISS
Catalog Number: 25544
Epoch time:      17176
71698414   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:       355
8157  deg
Eccentricity:     
0004676     
Arg of perigee:   317
9083  deg
Mean anomaly:      42
1710  deg
Mean motion:   15
54084816  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2307
Checksum:              312


Coasting Arc #12 (Orbit 2322)
---------------------------------------

Vector Time (GMT): 2017/177/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5992047
18                 A    =         6785767
78  meter
 Y    =        1310325
17  meter          E    =           
0011648
 Z    =        2886245
77                 I    =           51
59231
 XDOT =      -3449
159788                 Wp   =           60
96207
 YDOT =       4637
890511  meter/sec      RA   =          350
43041  deg
 ZDOT =       5045
282885                 TA   =          331
95003
                                          MA   =          332
01275
                                          Ha   =            220
594  n
mi
                                          Hp   =            215
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19658947
44                 X    =         5962929
65
 Y    =        4298967
09  feet           Y    =         1377169
11  meter
 Z    =        9469310
27                 Z    =         2915282
37
 XDOT =     -11316
141037                 XDOT =       -3525
272747
 YDOT =      15216
176216  feet/sec       YDOT =        4598
893414  meter/sec
 ZDOT =      16552
765371                 ZDOT =        5028
343907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17241962
00                 X    =        -5255350
02
 Y    =      -10258196
51  feet           Y    =        -3126698
30  meter
 Z    =        9597255
86                 Z    =         2925243
58
 XDOT =      14890
785576                 XDOT =        4538
711444
 YDOT =      -9583
112517  feet/sec       YDOT =       -2920
932695  meter/sec
 ZDOT =      16477
063876                 ZDOT =        5022
209069


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   17177
74584715  
00016717  00000-0  10270-3 0  9113
2 25544  51
6426 350
6872 0004693 322
2896  37
7927 15
54105281 23238


Satellite: ISS
Catalog Number: 25544
Epoch time:      17177
74584715   =   yrday
fracday
Element set:     911
Inclination:       51
6426  deg
RA of node:       350
6872  deg
Eccentricity:     
0004693     
Arg of perigee:   322
2896  deg
Mean anomaly:      37
7927  deg
Mean motion:   15
54105281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2323
Checksum:              325


Coasting Arc #13 (Orbit 2337)
---------------------------------------

Vector Time (GMT): 2017/178/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4928606
68                 A    =         6782054
97  meter
 Y    =       -2127581
84  meter          E    =           
0008100
 Z    =       -4153305
69                 I    =           51
54768
 XDOT =       5047
645163                 Wp   =           34
82862
 YDOT =      -4381
277924  meter/sec      RA   =          345
44306  deg
 ZDOT =      -3742
637648                 TA   =          196
55876
                                          MA   =          196
58522
                                          Ha   =            220
861  n
mi
                                          Hp   =            215
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16169969
41                 X    =        -4884274
74
 Y    =       -6980255
39  feet           Y    =        -2182448
53  meter
 Z    =      -13626331
02                 Z    =        -4177139
59
 XDOT =      16560
515626                 XDOT =        5114
442273
 YDOT =     -14374
271404  feet/sec       YDOT =       -4324
457831  meter/sec
 ZDOT =     -12278
994909                 ZDOT =       -3717
956321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13259022
79                 X    =         4041350
15
 Y    =       11468338
41  feet           Y    =         3495549
55  meter
 Z    =      -13731143
51                 Z    =        -4185252
54
 XDOT =     -19339
933066                 XDOT =       -5894
811598
 YDOT =       7778
171821  feet/sec       YDOT =        2370
786771  meter/sec
 ZDOT =     -12169
169305                 ZDOT =       -3709
162804


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   17178
71040443  
00016717  00000-0  10270-3 0  9127
2 25544  51
6425 345
8801 0004800 326
0040  34
0804 15
54080395 23386


Satellite: ISS
Catalog Number: 25544
Epoch time:      17178
71040443   =   yrday
fracday
Element set:     912
Inclination:       51
6425  deg
RA of node:       345
8801  deg
Eccentricity:     
0004800     
Arg of perigee:   326
0040  deg
Mean anomaly:      34
0804  deg
Mean motion:   15
54080395  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2338
Checksum:              277


Coasting Arc #14 (Orbit 2353)
---------------------------------------

Vector Time (GMT): 2017/179/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3524455
76                 A    =         6778722
82  meter
 Y    =        2950710
89  meter          E    =           
0002696
 Z    =        4979741
85                 I    =           51
50563
 XDOT =      -6235
572449                 Wp   =           70
06749
 YDOT =       3959
600468  meter/sec      RA   =          340
44316  deg
 ZDOT =       2067
037320                 TA   =          359
79237
                                          MA   =          359
79248
                                          Ha   =            220
840  n
mi
                                          Hp   =            215
438

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11563175
07                 X    =         3467009
33
 Y    =        9680810
01  feet           Y    =         2989802
08  meter
 Z    =       16337735
73                 Z    =         4996723
11
 XDOT =     -20457
914860                 XDOT =       -6289
426841
 YDOT =      12990
815183  feet/sec       YDOT =        3889
568759  meter/sec
 ZDOT =       6781
618503                 ZDOT =        2036
616752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8255418
31                 X    =        -2516251
50
 Y    =      -12523445
07  feet           Y    =        -3817146
06  meter
 Z    =       16412132
73                 Z    =         5002418
06
 XDOT =      22422
936424                 XDOT =        6834
511022
 YDOT =      -6070
704948  feet/sec       YDOT =       -1850
350868  meter/sec
 ZDOT =       6646
548331                 ZDOT =        2025
867931


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   17179
73926151  
00016717  00000-0  10270-3 0  9130
2 25544  51
6425 340
7519 0004848 330
1342  29
9534 15
54121713 23540


Satellite: ISS
Catalog Number: 25544
Epoch time:      17179
73926151   =   yrday
fracday
Element set:     913
Inclination:       51
6425  deg
RA of node:       340
7519  deg
Eccentricity:     
0004848     
Arg of perigee:   330
1342  deg
Mean anomaly:      29
9534  deg
Mean motion:   15
54121713  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2354
Checksum:              304


Coasting Arc #15 (Orbit 2368)
---------------------------------------

Vector Time (GMT): 2017/180/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1942959
68                 A    =         6777472
29  meter
 Y    =       -3757654
23  meter          E    =           
0013503
 Z    =       -5306252
10                 I    =           51
47023
 XDOT =       6903
825281                 Wp   =           69
10862
 YDOT =      -3311
822058  meter/sec      RA   =          335
43502  deg
 ZDOT =       -178
300310                 TA   =          199
16068
                                          MA   =          199
21152
                                          Ha   =            221
080  n
mi
                                          Hp   =            215
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6374539
64                 X    =        -1875021
27
 Y    =      -12328261
90  feet           Y    =        -3779001
42  meter
 Z    =      -17408963
58                 Z    =        -5315525
60
 XDOT =      22650
345409                 XDOT =        6941
211929
 YDOT =     -10865
557933  feet/sec       YDOT =       -3234
409746  meter/sec
 ZDOT =       -584
974770                 ZDOT =        -144
673426

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2757181
27                 X    =          840388
85
 Y    =       13550533
23  feet           Y    =         4130202
53  meter
 Z    =      -17449177
93                 Z    =        -5318509
43
 XDOT =     -23739
049137                 XDOT =       -7235
662177
 YDOT =       4250
659234  feet/sec       YDOT =        1295
600934  meter/sec
 ZDOT =       -435
887927                 ZDOT =        -132
858640


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   17180
70381412  
00016717  00000-0  10270-3 0  9145
2 25544  51
6421 335
9449 0004967 333
5955  26
4944 15
54090470 23691


Satellite: ISS
Catalog Number: 25544
Epoch time:      17180
70381412   =   yrday
fracday
Element set:     914
Inclination:       51
6421  deg
RA of node:       335
9449  deg
Eccentricity:     
0004967     
Arg of perigee:   333
5955  deg
Mean anomaly:      26
4944  deg
Mean motion:   15
54090470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2369
Checksum:              320


Coasting Arc #16 (Orbit 2384)
---------------------------------------

Vector Time (GMT): 2017/181/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         281874
19                 A    =         6778372
19  meter
 Y    =        4487990
54  meter          E    =           
0008175
 Z    =        5071876
63                 I    =           51
44505
 XDOT =      -7066
739120                 Wp   =           17
52495
 YDOT =       2417
739720  meter/sec      RA   =          330
42285  deg
 ZDOT =      -1738
286150                 TA   =           89
37184
                                          MA   =           89
27818
                                          Ha   =            221
185  n
mi
                                          Hp   =            215
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         924784
08                 X    =          207030
81
 Y    =       14724378
41  feet           Y    =         4490723
78  meter
 Z    =       16640015
19                 Z    =         5073064
44
 XDOT =     -23184
839632                 XDOT =       -7084
806018
 YDOT =       7932
216928  feet/sec       YDOT =        2338
613766  meter/sec
 ZDOT =      -5703
038551                 ZDOT =       -1772
657672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2880124
26                 X    =          877861
87
 Y    =      -14464491
79  feet           Y    =        -4408777
10  meter
 Z    =       16644398
82                 Z    =         5073212
76
 XDOT =      23338
707081                 XDOT =        7113
637918
 YDOT =      -2122
143221  feet/sec       YDOT =        -646
829254  meter/sec
 ZDOT =      -5855
228274                 ZDOT =       -1784
673578


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   17181
73266457  
00016717  00000-0  10270-3 0  9151
2 25544  51
6427 330
8159 0005088 338
1122  21
9812 15
54140816 23853


Satellite: ISS
Catalog Number: 25544
Epoch time:      17181
73266457   =   yrday
fracday
Element set:     915
Inclination:       51
6427  deg
RA of node:       330
8159  deg
Eccentricity:     
0005088     
Arg of perigee:   338
1122  deg
Mean anomaly:      21
9812  deg
Mean motion:   15
54140816  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2385
Checksum:              308
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