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

 
Date: June 25th 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) : 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


182/20:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 214 8

183/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 215 0

Coasting Arc #1 (Orbit 2272)
---------------------------------------

Vector Time (GMT): 2017/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6610367
84                 A    =         6789178
13  meter
 Y    =       -1334559
02  meter          E    =           
0005204
 Z    =        -760466
78                 I    =           51
70366
 XDOT =       1601
705322                 Wp   =          147
95838
 YDOT =      -4553
643381  meter/sec      RA   =            6
30524  deg
 ZDOT =      -5954
554644                 TA   =           40
25037
                                          MA   =           40
21185
                                          Ha   =            220
445  n
mi
                                          Hp   =            216
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21687558
52                 X    =        -6591259
17
 Y    =       -4378474
46  feet           Y    =        -1408373
66  meter
 Z    =       -2494969
76                 Z    =         -792531
79
 XDOT =       5254
938722                 XDOT =        1681
430680
 YDOT =     -14939
774873  feet/sec       YDOT =       -4535
285249  meter/sec
 ZDOT =     -19535
940433                 ZDOT =       -5946
581167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4006232
67                 X    =        -1221099
72
 Y    =       21742727
76  feet           Y    =         6627183
42  meter
 Z    =       -2636284
64                 Z    =         -803539
56
 XDOT =     -13446
177051                 XDOT =       -4098
394765
 YDOT =      -4833
221028  feet/sec       YDOT =       -1473
165769  meter/sec
 ZDOT =     -19499
832019                 ZDOT =       -5943
548800


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
53062184  
00016717  00000-0  10270-3 0  9006
2 25544  51
6393   6
7155 0005170 312
4359  47
6356 15
54085089 22733


Satellite: ISS
Catalog Number: 25544
Epoch time:      17174
53062184   =   yrday
fracday
Element set:     900
Inclination:       51
6393  deg
RA of node:         6
7155  deg
Eccentricity:     
0005170     
Arg of perigee:   312
4359  deg
Mean anomaly:      47
6356  deg
Mean motion:   15
54085089  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2273
Checksum:              303


Coasting Arc #2 (Orbit 2288)
---------------------------------------

Vector Time (GMT): 2017/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6021652
91                 A    =         6786968
23  meter
 Y    =        2017516
46  meter          E    =           
0012118
 Z    =        2373176
25                 I    =           51
66286
 XDOT =      -3525
673392                 Wp   =           52
51979
 YDOT =       4176
513870  meter/sec      RA   =            1
33458  deg
 ZDOT =       5383
747728                 TA   =          333
98525
                                          MA   =          334
04610
                                          Ha   =            220
428  n
mi
                                          Hp   =            215
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19756079
09                 X    =         5987117
29
 Y    =        6619148
48  feet           Y    =         2084661
15  meter
 Z    =        7786011
33                 Z    =         2402343
93
 XDOT =     -11567
169922                 XDOT =       -3598
265733
 YDOT =      13702
473326  feet/sec       YDOT =        4136
680593  meter/sec
 ZDOT =      17663
214330                 ZDOT =        5366
445561

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5939003
20                 X    =         1810208
18
 Y    =      -19920550
04  feet           Y    =        -6071783
65  meter
 Z    =        7914397
47                 Z    =         2412308
35
 XDOT =      12644
677363                 XDOT =        3854
097660
 YDOT =      10771
616790  feet/sec       YDOT =        3283
188798  meter/sec
 ZDOT =      17585
990724                 ZDOT =        5360
209973


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
55948959  
00016717  00000-0  10270-3 0  9013
2 25544  51
6383   1
5856 0005006 314
8881  45
1864 15
54092457 22898


Satellite: ISS
Catalog Number: 25544
Epoch time:      17175
55948959   =   yrday
fracday
Element set:     901
Inclination:       51
6383  deg
RA of node:         1
5856  deg
Eccentricity:     
0005006     
Arg of perigee:   314
8881  deg
Mean anomaly:      45
1864  deg
Mean motion:   15
54092457  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2289
Checksum:              335


Coasting Arc #3 (Orbit 2303)
---------------------------------------

Vector Time (GMT): 2017/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4983554
67                 A    =         6783346
79  meter
 Y    =       -2665451
30  meter          E    =           
0005887
 Z    =       -3758315
50                 I    =           51
61777
 XDOT =       5187
978825                 Wp   =           27
11929
 YDOT =      -3703
745254  meter/sec      RA   =          356
35475  deg
 ZDOT =      -4250
055130                 TA   =          197
82377
                                          MA   =          197
84442
                                          Ha   =            220
697  n
mi
                                          Hp   =            215
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16350244
99                 X    =        -4935122
63
 Y    =       -8744918
95  feet           Y    =        -2720909
38  meter
 Z    =      -12330431
43                 Z    =        -3782406
64
 XDOT =      17020
927902                 XDOT =        5249
653988
 YDOT =     -12151
395191  feet/sec       YDOT =       -3645
384234  meter/sec
 ZDOT =     -13943
750426                 ZDOT =       -4224
704556

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7895880
45                 X    =        -2406664
36
 Y    =       16698437
02  feet           Y    =         5089683
60  meter
 Z    =      -12436274
80                 Z    =        -3790576
56
 XDOT =     -11800
764001                 XDOT =       -3596
872867
 YDOT =     -15886
847969  feet/sec       YDOT =       -4842
311261  meter/sec
 ZDOT =     -13831
086452                 ZDOT =       -4215
715151


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
52405320  
00016717  00000-0  10270-3 0  9022
2 25544  51
6378 356
7775 0004947 320
8204  39
2590 15
54093443 23040


Satellite: ISS
Catalog Number: 25544
Epoch time:      17176
52405320   =   yrday
fracday
Element set:     902
Inclination:       51
6378  deg
RA of node:       356
7775  deg
Eccentricity:     
0004947     
Arg of perigee:   320
8204  deg
Mean anomaly:      39
2590  deg
Mean motion:   15
54093443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2304
Checksum:              306


Coasting Arc #4 (Orbit 2319)
---------------------------------------

Vector Time (GMT): 2017/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3570483
46                 A    =         6779832
82  meter
 Y    =        3265708
86  meter          E    =           
0003602
 Z    =        4745699
35                 I    =           51
57376
 XDOT =      -6457
245920                 Wp   =           82
55227
 YDOT =       3142
869764  meter/sec      RA   =          351
36174  deg
 ZDOT =       2694
152497                 TA   =          340
80247
                                          MA   =          340
81603
                                          Ha   =            220
723  n
mi
                                          Hp   =            215
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11714184
56                 X    =         3510648
08
 Y    =       10714267
91  feet           Y    =         3305301
20  meter
 Z    =       15569879
77                 Z    =         4762898
57
 XDOT =     -21185
190027                 XDOT =       -6504
997110
 YDOT =      10311
252506  feet/sec       YDOT =        3070
393095  meter/sec
 ZDOT =       8839
082995                 ZDOT =        2662
670039

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9892455
13                 X    =         3015220
32
 Y    =      -12320982
79  feet           Y    =        -3755435
55  meter
 Z    =       15645175
85                 Z    =         4768649
60
 XDOT =      10848
805223                 XDOT =        3306
715832
 YDOT =      19762
398002  feet/sec       YDOT =        6023
578911  meter/sec
 ZDOT =       8699
461317                 ZDOT =        2651
595809


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
55291819  
00016717  00000-0  10270-3 0  9033
2 25544  51
6382 351
6481 0005052 322
8428  37
2374 15
54074156 23207


Satellite: ISS
Catalog Number: 25544
Epoch time:      17177
55291819   =   yrday
fracday
Element set:     903
Inclination:       51
6382  deg
RA of node:       351
6481  deg
Eccentricity:     
0005052     
Arg of perigee:   322
8428  deg
Mean anomaly:      37
2374  deg
Mean motion:   15
54074156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2320
Checksum:              304


Coasting Arc #5 (Orbit 2334)
---------------------------------------

Vector Time (GMT): 2017/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1932672
99                 A    =         6777675
96  meter
 Y    =       -3829652
48  meter          E    =           
0013227
 Z    =       -5258441
61                 I    =           51
53563
 XDOT =       7205
367095                 Wp   =           63
97109
 YDOT =      -2450
972402  meter/sec      RA   =          346
35941  deg
 ZDOT =       -859
235479                 TA   =          197
76834
                                          MA   =          197
81463
                                          Ha   =            220
907  n
mi
                                          Hp   =            215
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6340790
64                 X    =        -1864162
58
 Y    =      -12564476
65  feet           Y    =        -3850881
27  meter
 Z    =      -17252105
02                 Z    =        -5267663
86
 XDOT =      23639
655823                 XDOT =        7236
412687
 YDOT =      -8041
248038  feet/sec       YDOT =       -2370
223417  meter/sec
 ZDOT =      -2819
014038                 ZDOT =        -824
159374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11984878
65                 X    =        -3652991
01
 Y    =        7283798
45  feet           Y    =         2220101
77  meter
 Z    =      -17292073
06                 Z    =        -5270623
87
 XDOT =      -9511
933712                 XDOT =       -2899
237395
 YDOT =     -22005
806488  feet/sec       YDOT =       -6707
369818  meter/sec
 ZDOT =      -2663
670156                 ZDOT =        -811
886663


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
51747640  
00016717  00000-0  10270-3 0  9049
2 25544  51
6392 346
8403 0004822 328
6769  31
4095 15
54094296 23353


Satellite: ISS
Catalog Number: 25544
Epoch time:      17178
51747640   =   yrday
fracday
Element set:     904
Inclination:       51
6392  deg
RA of node:       346
8403  deg
Eccentricity:     
0004822     
Arg of perigee:   328
6769  deg
Mean anomaly:      31
4095  deg
Mean motion:   15
54094296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2335
Checksum:              326


Coasting Arc #6 (Orbit 2350)
---------------------------------------

Vector Time (GMT): 2017/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         180366
63                 A    =         6777997
17  meter
 Y    =        4320481
85  meter          E    =           
0006428
 Z    =        5219577
14                 I    =           51
50351
 XDOT =      -7421
519818                 Wp   =            8
47121
 YDOT =       1608
018206  meter/sec      RA   =          341
35122  deg
 ZDOT =      -1068
175340                 TA   =           91
81763
                                          MA   =           91
74401
                                          Ha   =            221
111  n
mi
                                          Hp   =            215
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         591754
05                 X    =          106686
62
 Y    =       14174809
22  feet           Y    =         4322086
36  meter
 Z    =       17124596
91                 Z    =         5220274
75
 XDOT =     -24348
818302                 XDOT =       -7433
760912
 YDOT =       5275
650281  feet/sec       YDOT =        1524
957397  meter/sec
 ZDOT =      -3504
512271                 ZDOT =       -1104
255933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14051544
80                 X    =         4282910
85
 Y    =       -1937198
05  feet           Y    =         -590457
96  meter
 Z    =       17126837
45                 Z    =         5220260
05
 XDOT =       7611
211782                 XDOT =        2319
897351
 YDOT =      22628
092082  feet/sec       YDOT =        6897
042467  meter/sec
 ZDOT =      -3664
116232                 ZDOT =       -1116
822628


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
54633770  
00016717  00000-0  10270-3 0  9052
2 25544  51
6380 341
7112 0004777 332
4442  27
6457 15
54048640 23510


Satellite: ISS
Catalog Number: 25544
Epoch time:      17179
54633770   =   yrday
fracday
Element set:     905
Inclination:       51
6380  deg
RA of node:       341
7112  deg
Eccentricity:     
0004777     
Arg of perigee:   332
4442  deg
Mean anomaly:      27
6457  deg
Mean motion:   15
54048640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2351
Checksum:              306


Coasting Arc #7 (Orbit 2365)
---------------------------------------

Vector Time (GMT): 2017/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1487307
63                 A    =         6780270
00  meter
 Y    =       -4701050
09  meter          E    =           
0007862
 Z    =       -4660392
04                 I    =           51
48263
 XDOT =       7077
753303                 Wp   =           83
51322
 YDOT =       -603
810211  meter/sec      RA   =          336
34574  deg
 ZDOT =       2872
902685                 TA   =          215
09390
                                          MA   =          215
14573
                                          Ha   =            221
118  n
mi
                                          Hp   =            215
346

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4879618
21                 X    =         1562403
15
 Y    =      -15423392
67  feet           Y    =        -4683997
74  meter
 Z    =      -15290000
13                 Z    =        -4652985
22
 XDOT =      23220
975404                 XDOT =        7070
024219
 YDOT =      -1981
004629  feet/sec       YDOT =        -524
705425  meter/sec
 ZDOT =       9425
533744                 ZDOT =        2907
265070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15911082
15                 X    =        -4849697
84
 Y    =       -3091230
83  feet           Y    =         -942207
16  meter
 Z    =      -15256394
60                 Z    =        -4650149
07
 XDOT =      -4972
195575                 XDOT =       -1515
525211
 YDOT =     -21593
234685  feet/sec       YDOT =       -6581
617932  meter/sec
 ZDOT =       9577
347345                 ZDOT =        2919
175471


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
51089122  
00016717  00000-0  10270-3 0  9068
2 25544  51
6397 336
9038 0004809 335
0162  25
0757 15
54093538 23662


Satellite: ISS
Catalog Number: 25544
Epoch time:      17180
51089122   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:       336
9038  deg
Eccentricity:     
0004809     
Arg of perigee:   335
0162  deg
Mean anomaly:      25
0757  deg
Mean motion:   15
54093538  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2366
Checksum:              314


Coasting Arc #8 (Orbit 2381)
---------------------------------------

Vector Time (GMT): 2017/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2995740
95                 A    =         6784030
27  meter
 Y    =        4904742
26  meter          E    =           
0011497
 Z    =        3600447
98                 I    =           51
46522
 XDOT =      -6252
638157                 Wp   =           63
03494
 YDOT =       -577
009081  meter/sec      RA   =          331
34537  deg
 ZDOT =      -4400
476445                 TA   =           74
22381
                                          MA   =           74
09706
                                          Ha   =            221
279  n
mi
                                          Hp   =            215
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9828546
42                 X    =        -3067853
51
 Y    =       16091674
09  feet           Y    =         4870838
37  meter
 Z    =       11812493
39                 Z    =         3585720
93
 XDOT =     -20513
904714                 XDOT =       -6224
345967
 YDOT =      -1893
074413  feet/sec       YDOT =        -646
771790  meter/sec
 ZDOT =     -14437
258678                 ZDOT =       -4430
780956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17299125
84                 X    =         5272773
56
 Y    =        7605017
46  feet           Y    =         2318009
32  meter
 Z    =       11746542
23                 Z    =         3580346
07
 XDOT =       1478
383943                 XDOT =         450
611426
 YDOT =      19224
455220  feet/sec       YDOT =        5859
613951  meter/sec
 ZDOT =     -14570
922956                 ZDOT =       -4441
217317


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
53974685  
00016717  00000-0  10270-3 0  9079
2 25544  51
6393 331
7744 0004826 339
0051  21
0903 15
54082507 23826


Satellite: ISS
Catalog Number: 25544
Epoch time:      17181
53974685   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       331
7744  deg
Eccentricity:     
0004826     
Arg of perigee:   339
0051  deg
Mean anomaly:      21
0903  deg
Mean motion:   15
54082507  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2382
Checksum:              309


Coasting Arc #9 (Orbit 2396)
---------------------------------------

Vector Time (GMT): 2017/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4171029
74                 A    =         6787419
54  meter
 Y    =       -4877104
34  meter          E    =           
0009678
 Z    =       -2194976
60                 I    =           51
44928
 XDOT =       5049
546386                 Wp   =           16
36514
 YDOT =       1867
260578  meter/sec      RA   =          326
35459  deg
 ZDOT =       5461
497583                 TA   =          319
19020
                                          MA   =          319
26264
                                          Ha   =            221
379  n
mi
                                          Hp   =            215
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13684480
77                 X    =         4235918
88
 Y    =      -16000998
48  feet           Y    =        -4830098
06  meter
 Z    =       -7201366
79                 Z    =        -2174557
88
 XDOT =      16566
753235                 XDOT =        5001
761716
 YDOT =       6126
182998  feet/sec       YDOT =        1923
460413  meter/sec
 ZDOT =      17918
299156                 ZDOT =        5485
910717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17927151
64                 X    =        -5464195
82
 Y    =      -11100334
55  feet           Y    =        -3383381
97  meter
 Z    =       -7110306
39                 Z    =        -2167221
39
 XDOT =       2709
280626                 XDOT =         825
788735
 YDOT =     -15889
980349  feet/sec       YDOT =       -4843
266011  meter/sec
 ZDOT =      18025
705166                 ZDOT =        5494
234935


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   17182
50429648  
00016717  00000-0  10270-3 0  9082
2 25544  51
6399 326
9672 0004855 343
2924  16
8068 15
54099077 23976


Satellite: ISS
Catalog Number: 25544
Epoch time:      17182
50429648   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:       326
9672  deg
Eccentricity:     
0004855     
Arg of perigee:   343
2924  deg
Mean anomaly:      16
8068  deg
Mean motion:   15
54099077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2397
Checksum:              352


Coasting Arc #10 (Orbit 2402)
---------------------------------------

Vector Time (GMT): 2017/182/20:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922738
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3753479
80                 A    =         6778173
64  meter
 Y    =       -2361177
58  meter          E    =           
0014440
 Z    =       -5138693
17                 I    =           51
40823
 XDOT =       5354
358186                 Wp   =           57
66628
 YDOT =      -5269
772968  meter/sec      RA   =          324
53302  deg
 ZDOT =      -1485
095821                 TA   =          197
94237
                                          MA   =          197
99339
                                          Ha   =            221
481  n
mi
                                          Hp   =            214
837

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12314566
28                 X    =        -3701836
35
 Y    =       -7746645
61  feet           Y    =        -2402862
36  meter
 Z    =      -16859229
56                 Z    =        -5156801
13
 XDOT =      17566
791950                 XDOT =        5420
102075
 YDOT =     -17289
281391  feet/sec       YDOT =       -5209
529184  meter/sec
 ZDOT =      -4872
361616                 ZDOT =       -1458
926828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13533930
96                 X    =         4125142
16
 Y    =       -5079914
10  feet           Y    =        -1548357
82  meter
 Z    =      -16938709
16                 Z    =        -5162918
55
 XDOT =       2840
096706                 XDOT =         865
661476
 YDOT =      23473
788114  feet/sec       YDOT =        7154
810617  meter/sec
 ZDOT =      -4755
848199                 ZDOT =       -1449
582531


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   17182
89011485  
00016717  00000-0  10270-3 0  9091
2 25544  51
6398 325
0483 0005159 345
8322  14
2685 15
54088336 24034


Satellite: ISS
Catalog Number: 25544
Epoch time:      17182
89011485   =   yrday
fracday
Element set:     909
Inclination:       51
6398  deg
RA of node:       325
0483  deg
Eccentricity:     
0005159     
Arg of perigee:   345
8322  deg
Mean anomaly:      14
2685  deg
Mean motion:   15
54088336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2403
Checksum:              319


Coasting Arc #11 (Orbit 2412)
---------------------------------------

Vector Time (GMT): 2017/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5009439
40                 A    =         6789265
52  meter
 Y    =        4547127
63  meter          E    =           
0009434
 Z    =         532575
61                 I    =           51
42837
 XDOT =      -3574
571181                 Wp   =          111
31009
 YDOT =      -3230
059352  meter/sec      RA   =          321
36887  deg
 ZDOT =      -5962
390214                 TA   =           62
92904
                                          MA   =           62
83281
                                          Ha   =            221
406  n
mi
                                          Hp   =            214
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16435168
64                 X    =        -5062501
26
 Y    =       14918397
74  feet           Y    =         4490811
95  meter
 Z    =        1747295
32                 Z    =          508112
86
 XDOT =     -11727
595738                 XDOT =       -3509
223812
 YDOT =     -10597
307584  feet/sec       YDOT =       -3269
666725  meter/sec
 ZDOT =     -19561
647683                 ZDOT =       -5979
595918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17512948
74                 X    =         5337946
77
 Y    =       13650585
55  feet           Y    =         4160698
48  meter
 Z    =        1638456
93                 Z    =          499401
67
 XDOT =      -7462
243566                 XDOT =       -2274
491839
 YDOT =      11965
085430  feet/sec       YDOT =        3646
958039  meter/sec
 ZDOT =     -19636
979038                 ZDOT =       -5985
351211


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   17183
53314757  
00016717  00000-0  10270-3 0  9103
2 25544  51
6392 321
8383 0004924 345
8751  14
2263 15
54113211 24130


Satellite: ISS
Catalog Number: 25544
Epoch time:      17183
53314757   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:       321
8383  deg
Eccentricity:     
0004924     
Arg of perigee:   345
8751  deg
Mean anomaly:      14
2263  deg
Mean motion:   15
54113211  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2413
Checksum:              287


Coasting Arc #12 (Orbit 2428)
---------------------------------------

Vector Time (GMT): 2017/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5425761
06                 A    =         6788751
65  meter
 Y    =       -3896606
18  meter          E    =           
0016220
 Z    =        1154916
40                 I    =           51
40374
 XDOT =       2007
009601                 Wp   =           41
45325
 YDOT =       4539
550796  meter/sec      RA   =          316
38323  deg
 ZDOT =       5852
039944                 TA   =          331
13712
                                          MA   =          331
22674
                                          Ha   =            221
458  n
mi
                                          Hp   =            214
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17801053
34                 X    =         5463320
66
 Y    =      -12784141
00  feet           Y    =        -3835721
74  meter
 Z    =        3789095
80                 Z    =         1181363
90
 XDOT =       6584
677167                 XDOT =        1927
671651
 YDOT =      14893
539358  feet/sec       YDOT =        4561
550347  meter/sec
 ZDOT =      19199
606116                 ZDOT =        5861
597130

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15898549
88                 X    =        -4845878
00
 Y    =      -15054696
44  feet           Y    =        -4588671
47  meter
 Z    =        3906563
07                 Z    =         1190720
42
 XDOT =      12317
051976                 XDOT =        3754
237442
 YDOT =      -7985
519926  feet/sec       YDOT =       -2433
986473  meter/sec
 ZDOT =      19240
932423                 ZDOT =        5864
636203


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   17184
56199558  
00016717  00000-0  10270-3 0  9118
2 25544  51
6410 316
7095 0004904 350
5842   9
5218 15
54122497 24296


Satellite: ISS
Catalog Number: 25544
Epoch time:      17184
56199558   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:       316
7095  deg
Eccentricity:     
0004904     
Arg of perigee:   350
5842  deg
Mean anomaly:       9
5218  deg
Mean motion:   15
54122497  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2429
Checksum:              318


Coasting Arc #13 (Orbit 2443)
---------------------------------------

Vector Time (GMT): 2017/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5486945
49                 A    =         6786063
73  meter
 Y    =        2900134
00  meter          E    =           
0004427
 Z    =       -2751510
16                 I    =           51
37154
 XDOT =       -440
267195                 Wp   =           54
41255
 YDOT =      -5684
521718  meter/sec      RA   =          311
39196  deg
 ZDOT =      -5116
903696                 TA   =          156
83991
                                          MA   =          156
81995
                                          Ha   =            221
641  n
mi
                                          Hp   =            214
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18001789
65                 X    =        -5505602
26
 Y    =        9514875
32  feet           Y    =         2838671
25  meter
 Z    =       -9027264
31                 Z    =        -2778209
03
 XDOT =      -1444
446178                 XDOT =        -351
813253
 YDOT =     -18650
005636  feet/sec       YDOT =       -5688
949928  meter/sec
 ZDOT =     -16787
741786                 ZDOT =       -5118
828182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12988928
83                 X    =         3959025
51
 Y    =       15611971
25  feet           Y    =         4758528
84  meter
 Z    =       -9145647
34                 Z    =        -2787593
31
 XDOT =     -16843
751526                 XDOT =       -5133
975465
 YDOT =       4181
221772  feet/sec       YDOT =        1274
436396  meter/sec
 ZDOT =     -16795
169368                 ZDOT =       -5119
167624


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   17185
52653844  
00016717  00000-0  10270-3 0  9129
2 25544  51
6407 311
9017 0004985 354
7271   5
3828 15
54118573 24442


Satellite: ISS
Catalog Number: 25544
Epoch time:      17185
52653844   =   yrday
fracday
Element set:     912
Inclination:       51
6407  deg
RA of node:       311
9017  deg
Eccentricity:     
0004985     
Arg of perigee:   354
7271  deg
Mean anomaly:       5
3828  deg
Mean motion:   15
54118573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2444
Checksum:              315


Coasting Arc #14 (Orbit 2459)
---------------------------------------

Vector Time (GMT): 2017/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5198290
10                 A    =         6782236
06  meter
 Y    =       -1608673
16  meter          E    =           
0010462
 Z    =        4037556
19                 I    =           51
33858
 XDOT =       -982
783060                 Wp   =           75
27952
 YDOT =       6552
667003  meter/sec      RA   =          306
38983  deg
 ZDOT =       3870
277113                 TA   =          334
45969
                                          MA   =          334
51134
                                          Ha   =            221
506  n
mi
                                          Hp   =            214
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17054757
56                 X    =         5196279
92
 Y    =       -5277799
08  feet           Y    =        -1550554
10  meter
 Z    =       13246575
44                 Z    =         4062802
77
 XDOT =      -3224
353870                 XDOT =       -1074
783547
 YDOT =      21498
251323  feet/sec       YDOT =        6541
161964  meter/sec
 ZDOT =      12697
759558                 ZDOT =        3865
280432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8907479
51                 X    =        -2714999
76
 Y    =      -15375441
88  feet           Y    =        -4686434
69  meter
 Z    =       13358303
59                 Z    =         4071610
94
 XDOT =      20576
364114                 XDOT =        6271
675782
 YDOT =       -892
444518  feet/sec       YDOT =        -272
017089  meter/sec
 ZDOT =      12674
484990                 ZDOT =        3863
183025


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   17186
55538042  
00016717  00000-0  10270-3 0  9136
2 25544  51
6410 306
7733 0004941 357
3787   2
7339 15
54146191 24609


Satellite: ISS
Catalog Number: 25544
Epoch time:      17186
55538042   =   yrday
fracday
Element set:     913
Inclination:       51
6410  deg
RA of node:       306
7733  deg
Eccentricity:     
0004941     
Arg of perigee:   357
3787  deg
Mean anomaly:       2
7339  deg
Mean motion:   15
54146191  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2460
Checksum:              309


Coasting Arc #15 (Orbit 2474)
---------------------------------------

Vector Time (GMT): 2017/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4672596
69                 A    =         6778994
33  meter
 Y    =          88150
84  meter          E    =           
0014644
 Z    =       -4923881
27                 I    =           51
30978
 XDOT =       2196
753883                 Wp   =           54
49397
 YDOT =      -6995
671322  meter/sec      RA   =          301
37665  deg
 ZDOT =      -2206
187451                 TA   =          193
82395
                                          MA   =          193
86409
                                          Ha   =            221
803  n
mi
                                          Hp   =            214
274

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15330041
62                 X    =        -4649317
42
 Y    =         289208
79  feet           Y    =           36029
52  meter
 Z    =      -16154466
12                 Z    =        -4946522
68
 XDOT =       7207
197779                 XDOT =        2285
534594
 YDOT =     -22951
677566  feet/sec       YDOT =       -6970
609029  meter/sec
 ZDOT =      -7238
147806                 ZDOT =       -2195
301646

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3909899
95                 X    =         1191737
51
 Y    =       14716226
48  feet           Y    =         4485505
83  meter
 Z    =      -16254413
37                 Z    =        -4954345
20
 XDOT =     -22946
965847                 XDOT =       -6994
235190
 YDOT =      -1856
832927  feet/sec       YDOT =        -565
962676  meter/sec
 ZDOT =      -7188
808144                 ZDOT =       -2191
148722


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   17187
51991932  
00016717  00000-0  10270-3 0  9145
2 25544  51
6419 301
9660 0005029    
8624 359
2536 15
54113909 24758


Satellite: ISS
Catalog Number: 25544
Epoch time:      17187
51991932   =   yrday
fracday
Element set:     914
Inclination:       51
6419  deg
RA of node:       301
9660  deg
Eccentricity:     
0005029     
Arg of perigee:      
8624  deg
Mean anomaly:     359
2536  deg
Mean motion:   15
54113909  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2475
Checksum:              317


Coasting Arc #16 (Orbit 2490)
---------------------------------------

Vector Time (GMT): 2017/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901313
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3949470
65                 A    =         6777271
40  meter
 Y    =        1559586
10  meter          E    =           
0005386
 Z    =        5279412
20                 I    =           51
28866
 XDOT =      -3173
072837                 Wp   =           32
26775
 YDOT =       6977
257005  meter/sec      RA   =          296
35386  deg
 ZDOT =        316
923594                 TA   =           54
72258
                                          MA   =           54
67221
                                          Ha   =            221
735  n
mi
                                          Hp   =            214
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12957580
86                 X    =         3906092
77
 Y    =        5116752
29  feet           Y    =         1603508
48  meter
 Z    =       17320906
18                 Z    =         5298492
26
 XDOT =     -10410
343954                 XDOT =       -3252
397983
 YDOT =      22891
263141  feet/sec       YDOT =        6941
329975  meter/sec
 ZDOT =       1039
775572                 ZDOT =         301
318190

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1671927
49                 X    =          509603
50
 Y    =      -13724803
77  feet           Y    =        -4183320
19  meter
 Z    =       17404834
57                 Z    =         5304993
58
 XDOT =      23790
673439                 XDOT =        7251
397264
 YDOT =       4109
817531  feet/sec       YDOT =        1252
672383  meter/sec
 ZDOT =        969
619267                 ZDOT =         295
539952


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   17188
54875502  
00016717  00000-0  10270-3 0  9154
2 25544  51
6422 296
8369 0005152   4
9903 355
1300 15
54163114 24917


Satellite: ISS
Catalog Number: 25544
Epoch time:      17188
54875502   =   yrday
fracday
Element set:     915
Inclination:       51
6422  deg
RA of node:       296
8369  deg
Eccentricity:     
0005152     
Arg of perigee:     4
9903  deg
Mean anomaly:     355
1300  deg
Mean motion:   15
54163114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2491
Checksum:              305
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