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

 
Date: June 21st 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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


187/04:14:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 213 5

Coasting Arc #1 (Orbit 549)
---------------------------------------

Vector Time (GMT): 2016/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3288706
00                 A    =         6775993
17  meter
 Y    =        2651606
28  meter          E    =           
0003174
 Z    =        5296084
83                 I    =           51
87015
 XDOT =      -5421
996068                 Wp   =           46
96064
 YDOT =      -5385
662759  meter/sec      RA   =           40
87273  deg
 ZDOT =       -668
072955                 TA   =           49
40947
                                          MA   =           49
38185
                                          Ha   =            220
178  n
mi
                                          Hp   =            213
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10789717
83                 X    =        -3343838
60
 Y    =        8699495
67  feet           Y    =         2614520
72  meter
 Z    =       17375606
40                 Z    =         5279975
60
 XDOT =     -17788
701010                 XDOT =       -5358
124050
 YDOT =     -17669
497242  feet/sec       YDOT =       -5445
937900  meter/sec
 ZDOT =      -2191
840404                 ZDOT =        -694
257334

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8369578
10                 X    =         2551047
41
 Y    =       11158119
32  feet           Y    =         3400994
77  meter
 Z    =       17304839
47                 Z    =         5274515
07
 XDOT =     -17382
240814                 XDOT =       -5298
107000
 YDOT =      16624
818640  feet/sec       YDOT =        5067
244721  meter/sec
 ZDOT =      -2304
840477                 ZDOT =        -702
515377


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   16172
54703394  
00016717  00000-0  10270-3 0  9009
2 25544  51
6442  41
2776 0000862 332
9699  27
1409 15
54648981  5502


Satellite: ISS
Catalog Number: 25544
Epoch time:      16172
54703394   =   yrday
fracday
Element set:     900
Inclination:       51
6442  deg
RA of node:        41
2776  deg
Eccentricity:     
0000862     
Arg of perigee:   332
9699  deg
Mean anomaly:      27
1409  deg
Mean motion:   15
54648981  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             550
Checksum:              315


Coasting Arc #2 (Orbit 564)
---------------------------------------

Vector Time (GMT): 2016/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4663034
61                 A    =         6778311
79  meter
 Y    =       -1249024
49  meter          E    =           
0010434
 Z    =       -4768173
99                 I    =           51
85147
 XDOT =       4299
916501                 Wp   =          104
97086
 YDOT =       5733
810988  meter/sec      RA   =           35
88524  deg
 ZDOT =       2705
438105                 TA   =          191
70162
                                          MA   =          191
72589
                                          Ha   =            220
095  n
mi
                                          Hp   =            214
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15298669
97                 X    =         4699816
60
 Y    =       -4097849
37  feet           Y    =        -1196672
96  meter
 Z    =      -15643615
44                 Z    =        -4745433
05
 XDOT =      14107
337602                 XDOT =        4222
338202
 YDOT =      18811
715840  feet/sec       YDOT =        5781
461351  meter/sec
 ZDOT =       8876
109269                 ZDOT =        2726
138378

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3901022
91                 X    =        -1189031
78
 Y    =      -15450667
95  feet           Y    =        -4709363
59  meter
 Z    =      -15544235
48                 Z    =        -4737882
97
 XDOT =      17864
940638                 XDOT =        5445
233906
 YDOT =     -13522
333728  feet/sec       YDOT =       -4121
607320  meter/sec
 ZDOT =       8965
128045                 ZDOT =        2732
571028


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   16173
51125244  
00016717  00000-0  10270-3 0  9010
2 25544  51
6428  36
4673 0000887 336
9857  23
1256 15
54648193  5652


Satellite: ISS
Catalog Number: 25544
Epoch time:      16173
51125244   =   yrday
fracday
Element set:     901
Inclination:       51
6428  deg
RA of node:        36
4673  deg
Eccentricity:     
0000887     
Arg of perigee:   336
9857  deg
Mean anomaly:      23
1256  deg
Mean motion:   15
54648193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             565
Checksum:              316


Coasting Arc #3 (Orbit 580)
---------------------------------------

Vector Time (GMT): 2016/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5728499
32                 A    =         6782263
23  meter
 Y    =        -113160
91  meter          E    =           
0011688
 Z    =        3620775
06                 I    =           51
83928
 XDOT =      -2691
841104                 Wp   =           81
44547
 YDOT =      -5661
224758  meter/sec      RA   =           30
90611  deg
 ZDOT =      -4421
880804                 TA   =           55
75655
                                          MA   =           55
64589
                                          Ha   =            220
096  n
mi
                                          Hp   =            213
982

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18794289
09                 X    =        -5744396
22
 Y    =        -371262
82  feet           Y    =         -177310
19  meter
 Z    =       11879183
25                 Z    =         3592908
99
 XDOT =      -8831
499686                 XDOT =       -2606
856356
 YDOT =     -18573
572042  feet/sec       YDOT =       -5690
850922  meter/sec
 ZDOT =     -14507
482954                 ZDOT =       -4434
751387

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -288122
91                 X    =          -87819
86
 Y    =       18871947
16  feet           Y    =         5752169
49  meter
 Z    =       11757751
87                 Z    =         3583762
77
 XDOT =     -17160
628540                 XDOT =       -5230
559579
 YDOT =       8839
413583  feet/sec       YDOT =        2694
253260  meter/sec
 ZDOT =     -14562
386738                 ZDOT =       -4438
615478


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   16174
53974520  
00016717  00000-0  10270-3 0  9023
2 25544  51
6437  31
3365 0001094 336
1420  23
9683 15
54684159  5815


Satellite: ISS
Catalog Number: 25544
Epoch time:      16174
53974520   =   yrday
fracday
Element set:     902
Inclination:       51
6437  deg
RA of node:        31
3365  deg
Eccentricity:     
0001094     
Arg of perigee:   336
1420  deg
Mean anomaly:      23
9683  deg
Mean motion:   15
54684159  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             581
Checksum:              302


Coasting Arc #4 (Orbit 595)
---------------------------------------

Vector Time (GMT): 2016/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6337139
87                 A    =         6786106
03  meter
 Y    =        1295538
07  meter          E    =           
0007280
 Z    =       -2043298
98                 I    =           51
82258
 XDOT =        723
301128                 Wp   =           32
54908
 YDOT =       5220
621965  meter/sec      RA   =           25
93614  deg
 ZDOT =       5568
546658                 TA   =          304
91949
                                          MA   =          304
98787
                                          Ha   =            220
124  n
mi
                                          Hp   =            214
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20791141
30                 X    =         6332107
23
 Y    =        4250452
98  feet           Y    =         1366376
31  meter
 Z    =       -6703736
81                 Z    =        -2012527
07
 XDOT =       2373
035198                 XDOT =         637
819708
 YDOT =      17128
024819  feet/sec       YDOT =        5228
231740  meter/sec
 ZDOT =      18269
510033                 ZDOT =        5571
853283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3799931
90                 X    =         1158219
24
 Y    =      -20920684
33  feet           Y    =        -6376624
58  meter
 Z    =       -6569891
89                 Z    =        -2002503
05
 XDOT =      15551
620941                 XDOT =        4740
134063
 YDOT =      -2900
815059  feet/sec       YDOT =        -884
168430  meter/sec
 ZDOT =      18282
819806                 ZDOT =        5572
603477


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   16175
50395285  
00016717  00000-0  10270-3 0  9037
2 25544  51
6425  26
5252 0001029 338
4530  21
6579 15
54650732  5963


Satellite: ISS
Catalog Number: 25544
Epoch time:      16175
50395285   =   yrday
fracday
Element set:     903
Inclination:       51
6425  deg
RA of node:        26
5252  deg
Eccentricity:     
0001029     
Arg of perigee:   338
4530  deg
Mean anomaly:      21
6579  deg
Mean motion:   15
54650732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             596
Checksum:              304


Coasting Arc #5 (Orbit 611)
---------------------------------------

Vector Time (GMT): 2016/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6379000
37                 A    =         6787801
44  meter
 Y    =       -2297881
26  meter          E    =           
0011584
 Z    =         175103
11                 I    =           51
79843
 XDOT =       1455
358819                 Wp   =          130
27311
 YDOT =      -4518
534564  meter/sec      RA   =           20
97488  deg
 ZDOT =      -6023
232556                 TA   =           47
84424
                                          MA   =           47
74589
                                          Ha   =            220
112  n
mi
                                          Hp   =            213
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20928478
89                 X    =        -6353681
35
 Y    =       -7538980
51  feet           Y    =        -2369073
94  meter
 Z    =         574485
28                 Z    =          144177
07
 XDOT =       4774
799274                 XDOT =        1535
036021
 YDOT =     -14824
588463  feet/sec       YDOT =       -4501
813606  meter/sec
 ZDOT =     -19761
261666                 ZDOT =       -6015
969829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6722354
09                 X    =        -2048973
53
 Y    =       21208104
17  feet           Y    =         6464230
15  meter
 Z    =         440184
31                 Z    =          134168
18
 XDOT =     -13458
714015                 XDOT =       -4102
216032
 YDOT =      -3833
890704  feet/sec       YDOT =       -1168
569887  meter/sec
 ZDOT =     -19728
654001                 ZDOT =       -6013
293740


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   16176
53243574  
00016717  00000-0  10270-3 0  9045
2 25544  51
6419  21
3949 0000939 345
8185  14
2942 15
54651520  6126


Satellite: ISS
Catalog Number: 25544
Epoch time:      16176
53243574   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:        21
3949  deg
Eccentricity:     
0000939     
Arg of perigee:   345
8185  deg
Mean anomaly:      14
2942  deg
Mean motion:   15
54651520  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             612
Checksum:              305


Coasting Arc #6 (Orbit 627)
---------------------------------------

Vector Time (GMT): 2016/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5816645
42                 A    =         6786443
45  meter
 Y    =        3048636
46  meter          E    =           
0014036
 Z    =        1682923
67                 I    =           51
76358
 XDOT =      -3579
279459                 Wp   =           60
47580
 YDOT =       3658
067253  meter/sec      RA   =           16
01060  deg
 ZDOT =       5715
312964                 TA   =          317
94813
                                          MA   =          318
05578
                                          Ha   =            219
995  n
mi
                                          Hp   =            213
870

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19083482
35                 X    =         5773947
65
 Y    =       10002088
13  feet           Y    =         3113443
17  meter
 Z    =        5521403
11                 Z    =         1711075
80
 XDOT =     -11743
042846                 XDOT =       -3647
681144
 YDOT =      12001
532981  feet/sec       YDOT =        3617
658374  meter/sec
 ZDOT =      18751
026785                 ZDOT =        5697
760078

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8921752
77                 X    =         2719350
24
 Y    =      -19577046
53  feet           Y    =        -5967083
78  meter
 Z    =        5643450
61                 Z    =         1720123
74
 XDOT =      11220
393195                 XDOT =        3419
975846
 YDOT =      10523
332947  feet/sec       YDOT =        3207
511882  meter/sec
 ZDOT =      18673
756407                 ZDOT =        5691
760953


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   16177
56091175  
00016717  00000-0  10270-3 0  9058
2 25544  51
6415  16
2630 0000901 338
4928  21
6187 15
54690951  6285


Satellite: ISS
Catalog Number: 25544
Epoch time:      16177
56091175   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:        16
2630  deg
Eccentricity:     
0000901     
Arg of perigee:   338
4928  deg
Mean anomaly:      21
6187  deg
Mean motion:   15
54690951  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             628
Checksum:              307


Coasting Arc #7 (Orbit 642)
---------------------------------------

Vector Time (GMT): 2016/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4660026
85                 A    =         6782836
55  meter
 Y    =       -3610543
08  meter          E    =           
0004787
 Z    =       -3359948
24                 I    =           51
71981
 XDOT =       5448
099362                 Wp   =           78
06663
 YDOT =      -2691
329361  meter/sec      RA   =           11
03691  deg
 ZDOT =      -4668
758042                 TA   =          141
04291
                                          MA   =          141
00841
                                          Ha   =            220
096  n
mi
                                          Hp   =            213
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15288801
99                 X    =        -4602985
43
 Y    =      -11845613
79  feet           Y    =        -3662335
40  meter
 Z    =      -11023452
22                 Z    =        -3382447
08
 XDOT =      17874
341739                 XDOT =        5500
468237
 YDOT =      -8829
820737  feet/sec       YDOT =       -2630
111895  meter/sec
 ZDOT =     -15317
447644                 ZDOT =       -4642
165727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10702731
19                 X    =        -3262192
47
 Y    =       16042545
51  feet           Y    =         4889767
87  meter
 Z    =      -11120737
83                 Z    =        -3389600
89
 XDOT =      -8951
421389                 XDOT =       -2728
393239
 YDOT =     -16498
777443  feet/sec       YDOT =       -5028
827365  meter/sec
 ZDOT =     -15200
993013                 ZDOT =       -4633
262670


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   16178
52510438  
00016717  00000-0  10270-3 0  9064
2 25544  51
6409  11
4521 0001047 352
9348   7
1790 15
54686008  6437


Satellite: ISS
Catalog Number: 25544
Epoch time:      16178
52510438   =   yrday
fracday
Element set:     906
Inclination:       51
6409  deg
RA of node:        11
4521  deg
Eccentricity:     
0001047     
Arg of perigee:   352
9348  deg
Mean anomaly:       7
1790  deg
Mean motion:   15
54686008  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             643
Checksum:              295


Coasting Arc #8 (Orbit 658)
---------------------------------------

Vector Time (GMT): 2016/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3030544
32                 A    =         6778769
39  meter
 Y    =        3964240
90  meter          E    =           
0007968
 Z    =        4582932
80                 I    =           51
67365
 XDOT =      -6834
620587                 Wp   =          107
55461
 YDOT =       1696
521499  meter/sec      RA   =            6
04912  deg
 ZDOT =       3045
308347                 TA   =          312
01626
                                          MA   =          312
08407
                                          Ha   =            220
083  n
mi
                                          Hp   =            213
851

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9942730
72                 X    =         2963728
10
 Y    =       13006039
71  feet           Y    =         3997756
53  meter
 Z    =       15035868
78                 Z    =         4597492
40
 XDOT =     -22423
295888                 XDOT =       -6867
876305
 YDOT =       5566
015418  feet/sec       YDOT =        1619
906042  meter/sec
 ZDOT =       9991
169119                 ZDOT =        3012
026921

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12065984
75                 X    =         3677712
15
 Y    =      -10979085
38  feet           Y    =        -3346425
22  meter
 Z    =       15098477
05                 Z    =         4602015
80
 XDOT =       6772
755724                 XDOT =        2064
335945
 YDOT =      21013
350463  feet/sec       YDOT =        6404
869221  meter/sec
 ZDOT =       9845
783359                 ZDOT =        3000
994768


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   16179
55357127  
00016717  00000-0  10270-3 0  9073
2 25544  51
6403   6
3208 0001030 353
9604   6
1536 15
54665560  6598


Satellite: ISS
Catalog Number: 25544
Epoch time:      16179
55357127   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:         6
3208  deg
Eccentricity:     
0001030     
Arg of perigee:   353
9604  deg
Mean anomaly:       6
1536  deg
Mean motion:   15
54665560  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             659
Checksum:              295


Coasting Arc #9 (Orbit 673)
---------------------------------------

Vector Time (GMT): 2016/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1076876
72                 A    =         6776020
14  meter
 Y    =       -4171214
69  meter          E    =           
0014591
 Z    =       -5243070
61                 I    =           51
63214
 XDOT =       7560
778199                 Wp   =           78
71262
 YDOT =       -669
348653  meter/sec      RA   =            1
04802  deg
 ZDOT =      -1020
019612                 TA   =          181
50482
                                          MA   =          181
50922
                                          Ha   =            220
154  n
mi
                                          Hp   =            213
704

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3533060
11                 X    =        -1004684
53
 Y    =      -13685087
55  feet           Y    =        -4182852
96  meter
 Z    =      -17201675
24                 Z    =        -5248126
81
 XDOT =      24805
702754                 XDOT =        7572
655909
 YDOT =      -2196
025764  feet/sec       YDOT =        -584
732497  meter/sec
 ZDOT =      -3346
521037                 ZDOT =        -983
262429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13240247
17                 X    =        -4035627
34
 Y    =        4871540
31  feet           Y    =         1484845
49  meter
 Z    =      -17222825
44                 Z    =        -5249517
19
 XDOT =      -4493
611477                 XDOT =       -1369
652778
 YDOT =     -23482
027308  feet/sec       YDOT =       -7157
321924  meter/sec
 ZDOT =      -3186
216466                 ZDOT =        -971
158779


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   16180
51775339  
00016717  00000-0  10270-3 0  9081
2 25544  51
6399   1
5103 0000866   4
2878 355
8282 15
54695378  6747


Satellite: ISS
Catalog Number: 25544
Epoch time:      16180
51775339   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:         1
5103  deg
Eccentricity:     
0000866     
Arg of perigee:     4
2878  deg
Mean anomaly:     355
8282  deg
Mean motion:   15
54695378  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             674
Checksum:              332


Coasting Arc #10 (Orbit 689)
---------------------------------------

Vector Time (GMT): 2016/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -990733
48                 A    =         6776231
84  meter
 Y    =        4210608
05  meter          E    =           
0004627
 Z    =        5213589
75                 I    =           51
60068
 XDOT =      -7578
296462                 Wp   =           46
95345
 YDOT =       -375
581601  meter/sec      RA   =          356
04020  deg
 ZDOT =      -1133
041464                 TA   =           53
93047
                                          MA   =           53
88762
                                          Ha   =            220
246  n
mi
                                          Hp   =            213
774

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3250437
93                 X    =        -1063069
36
 Y    =       13814330
88  feet           Y    =         4199124
06  meter
 Z    =       17104953
25                 Z    =         5208601
71
 XDOT =     -24863
177370                 XDOT =       -7568
029538
 YDOT =      -1232
223102  feet/sec       YDOT =        -460
269649  meter/sec
 ZDOT =      -3717
327639                 ZDOT =       -1169
830133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14126752
60                 X    =         4305834
19
 Y    =        1615365
49  feet           Y    =          492363
40  meter
 Z    =       17082329
03                 Z    =         5206693
89
 XDOT =       1985
677229                 XDOT =         605
234420
 YDOT =      23768
856694  feet/sec       YDOT =        7244
747520  meter/sec
 ZDOT =      -3877
539193                 ZDOT =       -1181
873946


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   16181
54620922  
00016717  00000-0  10270-3 0  9093
2 25544  51
6403 356
3786 0000908   6
3226 353
7938 15
54670454  6909


Satellite: ISS
Catalog Number: 25544
Epoch time:      16181
54620922   =   yrday
fracday
Element set:     909
Inclination:       51
6403  deg
RA of node:       356
3786  deg
Eccentricity:     
0000908     
Arg of perigee:     6
3226  deg
Mean anomaly:     353
7938  deg
Mean motion:   15
54670454  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             690
Checksum:              316


Coasting Arc #11 (Orbit 704)
---------------------------------------

Vector Time (GMT): 2016/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2937936
01                 A    =         6779000
15  meter
 Y    =       -4104683
77  meter          E    =           
0009701
 Z    =       -4534358
70                 I    =           51
57811
 XDOT =       6841
029962                 Wp   =          104
83892
 YDOT =       1437
640471  meter/sec      RA   =          351
03486  deg
 ZDOT =       3134
266674                 TA   =          196
62525
                                          MA   =          196
65708
                                          Ha   =            220
225  n
mi
                                          Hp   =            213
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9638897
68                 X    =         3005643
29
 Y    =      -13466810
26  feet           Y    =        -4071450
72  meter
 Z    =      -14876504
92                 Z    =        -4519922
91
 XDOT =      22444
324023                 XDOT =        6809
220504
 YDOT =       4716
668212  feet/sec       YDOT =        1513
963210  meter/sec
 ZDOT =      10283
027147                 ZDOT =        3167
421692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14710052
08                 X    =        -4483623
87
 Y    =       -7731159
49  feet           Y    =        -2356457
41  meter
 Z    =      -14812740
02                 Z    =        -4514923
16
 XDOT =        940
279658                 XDOT =         286
597240
 YDOT =     -21747
211208  feet/sec       YDOT =       -6628
549976  meter/sec
 ZDOT =      10427
175011                 ZDOT =        3178
202943


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   16182
51038021  
00016717  00000-0  10270-3 0  9106
2 25544  51
6402 351
5677 0000862  20
7896 339
3292 15
54711265  7052


Satellite: ISS
Catalog Number: 25544
Epoch time:      16182
51038021   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:       351
5677  deg
Eccentricity:     
0000862     
Arg of perigee:    20
7896  deg
Mean anomaly:     339
3292  deg
Mean motion:   15
54711265  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             705
Checksum:              292


Coasting Arc #12 (Orbit 720)
---------------------------------------

Vector Time (GMT): 2016/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4583829
40                 A    =         6783253
41  meter
 Y    =        3794105
53  meter          E    =           
0012954
 Z    =        3245600
07                 I    =           51
55965
 XDOT =      -5467
505584                 Wp   =           89
35248
 YDOT =      -2526
907418  meter/sec      RA   =          346
03929  deg
 ZDOT =      -4751
366364                 TA   =           52
96004
                                          MA   =           52
84163
                                          Ha   =            220
230  n
mi
                                          Hp   =            213
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15038810
36                 X    =        -4641681
10
 Y    =       12447852
78  feet           Y    =         3742522
20  meter
 Z    =       10648294
19                 Z    =         3223192
93
 XDOT =     -17938
010445                 XDOT =       -5415
762599
 YDOT =      -8290
378668  feet/sec       YDOT =       -2587
758769  meter/sec
 ZDOT =     -15588
472322                 ZDOT =       -4777
800828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14685908
85                 X    =         4476265
02
 Y    =       12943160
97  feet           Y    =         3945075
46  meter
 Z    =       10549866
83                 Z    =         3215599
41
 XDOT =      -4416
130011                 XDOT =       -1346
036427
 YDOT =      17854
899251  feet/sec       YDOT =        5442
173292  meter/sec
 ZDOT =     -15703
105080                 ZDOT =       -4786
306428


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   16183
53882446  
00016717  00000-0  10270-3 0  9118
2 25544  51
6391 346
4366 0000808  12
8539 347
2634 15
54709430  7210


Satellite: ISS
Catalog Number: 25544
Epoch time:      16183
53882446   =   yrday
fracday
Element set:     911
Inclination:       51
6391  deg
RA of node:       346
4366  deg
Eccentricity:     
0000808     
Arg of perigee:    12
8539  deg
Mean anomaly:     347
2634  deg
Mean motion:   15
54709430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             721
Checksum:              312


Coasting Arc #13 (Orbit 735)
---------------------------------------

Vector Time (GMT): 2016/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5726289
73                 A    =         6786579
58  meter
 Y    =       -3280934
17  meter          E    =           
0009028
 Z    =       -1566153
47                 I    =           51
54226
 XDOT =       3613
419996                 Wp   =           36
00412
 YDOT =       3578
602194  meter/sec      RA   =          341
05306  deg
 ZDOT =       5738
828116                 TA   =          306
84658
                                          MA   =          306
92933
                                          Ha   =            220
232  n
mi
                                          Hp   =            213
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18787039
80                 X    =         5770160
05
 Y    =      -10764219
72  feet           Y    =        -3216653
47  meter
 Z    =       -5138298
80                 Z    =        -1538230
57
 XDOT =      11855
052479                 XDOT =        3545
257929
 YDOT =      11740
820845  feet/sec       YDOT =        3618
627921  meter/sec
 ZDOT =      18828
176233                 ZDOT =        5756
216123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13899744
14                 X    =        -4236642
01
 Y    =      -16639133
13  feet           Y    =        -5071607
78  meter
 Z    =       -5015951
28                 Z    =        -1528861
95
 XDOT =       8288
424609                 XDOT =        2526
311821
 YDOT =     -12598
020767  feet/sec       YDOT =       -3839
876730  meter/sec
 ZDOT =      18903
172266                 ZDOT =        5761
686907


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   16184
50298634  
00016717  00000-0  10270-3 0  9127
2 25544  51
6413 341
6256 0000847  24
7548 335
3645 15
54731980  7366


Satellite: ISS
Catalog Number: 25544
Epoch time:      16184
50298634   =   yrday
fracday
Element set:     912
Inclination:       51
6413  deg
RA of node:       341
6256  deg
Eccentricity:     
0000847     
Arg of perigee:    24
7548  deg
Mean anomaly:     335
3645  deg
Mean motion:   15
54731980  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             736
Checksum:              317


Coasting Arc #14 (Orbit 751)
---------------------------------------

Vector Time (GMT): 2016/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6300096
29                 A    =         6787416
79  meter
 Y    =        2488031
70  meter          E    =           
0010916
 Z    =        -353479
99                 I    =           51
51443
 XDOT =      -1470
681113                 Wp   =          132
24781
 YDOT =      -4557
101244  meter/sec      RA   =          336
07217  deg
 ZDOT =      -5989
672133                 TA   =           51
56959
                                          MA   =           51
47165
                                          Ha   =            220
165  n
mi
                                          Hp   =            213
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20669607
24                 X    =        -6325732
81
 Y    =        8162833
65  feet           Y    =         2417436
53  meter
 Z    =       -1159711
26                 Z    =         -384145
97
 XDOT =      -4825
069268                 XDOT =       -1390
518124
 YDOT =     -14951
119566  feet/sec       YDOT =       -4573
098276  meter/sec
 ZDOT =     -19651
155293                 ZDOT =       -5996
622254

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11984830
49                 X    =         3652976
33
 Y    =       18705594
45  feet           Y    =         5701465
19  meter
 Z    =       -1293839
91                 Z    =         -394362
41
 XDOT =     -12405
918557                 XDOT =       -3781
323976
 YDOT =       6612
882699  feet/sec       YDOT =        2015
606647  meter/sec
 ZDOT =     -19680
471699                 ZDOT =       -5998
607774


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   16185
53141848  
00016717  00000-0  10270-3 0  9136
2 25544  51
6404 336
4938 0001040  24
6708 335
4495 15
54763342  7527


Satellite: ISS
Catalog Number: 25544
Epoch time:      16185
53141848   =   yrday
fracday
Element set:     913
Inclination:       51
6404  deg
RA of node:       336
4938  deg
Eccentricity:     
0001040     
Arg of perigee:    24
6708  deg
Mean anomaly:     335
4495  deg
Mean motion:   15
54763342  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             752
Checksum:              307


Coasting Arc #15 (Orbit 767)
---------------------------------------

Vector Time (GMT): 2016/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6246576
30                 A    =         6785356
13  meter
 Y    =       -1456781
74  meter          E    =           
0014483
 Z    =        2191883
98                 I    =           51
47963
 XDOT =       -679
419900                 Wp   =           69
15417
 YDOT =       5343
540693  meter/sec      RA   =          331
08815  deg
 ZDOT =       5463
544541                 TA   =          315
25846
                                          MA   =          315
37519
                                          Ha   =            220
101  n
mi
                                          Hp   =            213
466

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20494016
74                 X    =         6251755
04
 Y    =       -4779467
65  feet           Y    =        -1386899
72  meter
 Z    =        7191220
40                 Z    =         2222240
30
 XDOT =      -2229
067912                 XDOT =        -765
661448
 YDOT =      17531
301485  feet/sec       YDOT =        5335
459977  meter/sec
 ZDOT =      17925
014898                 ZDOT =        5460
035427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8950892
69                 X    =        -2728232
09
 Y    =      -18994879
30  feet           Y    =        -5789639
21  meter
 Z    =        7323780
75                 Z    =         2232288
37
 XDOT =      16250
396602                 XDOT =        4953
120884
 YDOT =       -722
656029  feet/sec       YDOT =        -220
265558  meter/sec
 ZDOT =      17908
602960                 ZDOT =        5458
542182


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   16186
55984622  
00016717  00000-0  10270-3 0  9145
2 25544  51
6414 331
3630 0000777  32
4292 327
6909 15
54769339  7684


Satellite: ISS
Catalog Number: 25544
Epoch time:      16186
55984622   =   yrday
fracday
Element set:     914
Inclination:       51
6414  deg
RA of node:       331
3630  deg
Eccentricity:     
0000777     
Arg of perigee:    32
4292  deg
Mean anomaly:     327
6909  deg
Mean motion:   15
54769339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             768
Checksum:              333


Coasting Arc #16 (Orbit 777)
---------------------------------------

Vector Time (GMT): 2016/187/04:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 876584
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6042500
78                 A    =         6783933
53  meter
 Y    =        1100381
60  meter          E    =           
0004501
 Z    =       -2883828
77                 I    =           51
45875
 XDOT =       1376
615814                 Wp   =           98
10654
 YDOT =      -5612
796709  meter/sec      RA   =          327
71430  deg
 ZDOT =      -5033
471819                 TA   =          114
80807
                                          MA   =          114
76124
                                          Ha   =            220
170  n
mi
                                          Hp   =            213
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19824477
63                 X    =        -6040348
24
 Y    =        3610175
86  feet           Y    =         1032822
76  meter
 Z    =       -9461380
47                 Z    =        -2913175
93
 XDOT =       4516
456082                 XDOT =        1463
727289
 YDOT =     -18414
687366  feet/sec       YDOT =       -5596
914720  meter/sec
 ZDOT =     -16514
015153                 ZDOT =       -5026
573841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20054364
04                 X    =        -6112570
16
 Y    =       -1193979
61  feet           Y    =         -363924
99  meter
 Z    =       -9589468
13                 Z    =        -2922869
89
 XDOT =       8782
706762                 XDOT =        2676
969021
 YDOT =     -15326
198509  feet/sec       YDOT =       -4671
425305  meter/sec
 ZDOT =     -16482
787791                 ZDOT =       -5023
953719


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   16187
20261189  
00016717  00000-0  10270-3 0  9155
2 25544  51
6444 328
1616 0001252  13
0399 347
0786 15
54737591  7782


Satellite: ISS
Catalog Number: 25544
Epoch time:      16187
20261189   =   yrday
fracday
Element set:     915
Inclination:       51
6444  deg
RA of node:       328
1616  deg
Eccentricity:     
0001252     
Arg of perigee:    13
0399  deg
Mean anomaly:     347
0786  deg
Mean motion:   15
54737591  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             778
Checksum:              321
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