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

 
Date: October 30th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1552 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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


304/00:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 1

304/02:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 2

307/03:37:45 968 -0 4 4 5 4 5
N/A 4 3 -0 5 222 6
000/00:01:27 935 1 4 -0 1 215 1

308/04:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 215 2

311/14:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 3
000/00:00:00 000 0 0 0 0 215 4

314/21:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 215 5

Coasting Arc #1 (Orbit 2571)
---------------------------------------

Vector Time (GMT): 2016/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908899
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1427295
78                 A    =         6787666
31  meter
 Y    =       -6470251
18  meter          E    =           
0020372
 Z    =        1428424
13                 I    =           51
99710
 XDOT =       4992
955451                 Wp   =          118
56798
 YDOT =       -196
165393  meter/sec      RA   =          112
13762  deg
 ZDOT =      -5824
354802                 TA   =           45
91958
                                          MA   =           45
75206
                                          Ha   =            222
856  n
mi
                                          Hp   =            212
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4682728
93                 X    =         1492602
88
 Y    =      -21227858
21  feet           Y    =        -6453924
92  meter
 Z    =        4686430
88                 Z    =         1435516
93
 XDOT =      16381
087438                 XDOT =        5023
070745
 YDOT =       -643
587247  feet/sec       YDOT =        -140
162950  meter/sec
 ZDOT =     -19108
775597                 ZDOT =       -5800
026594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8854744
71                 X    =         2698926
19
 Y    =       19845433
95  feet           Y    =         6048888
27  meter
 Z    =        4718558
69                 Z    =         1438216
69
 XDOT =     -11452
968484                 XDOT =       -3490
864794
 YDOT =       9669
448160  feet/sec       YDOT =        2947
247799  meter/sec
 ZDOT =     -19002
215271                 ZDOT =       -5791
875214


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   16302
53500896  
00016717  00000-0  10270-3 0  9005
2 25544  51
6382 112
9465 0006512 117
2860 242
8957 15
54400916 25722


Satellite: ISS
Catalog Number: 25544
Epoch time:      16302
53500896   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:       112
9465  deg
Eccentricity:     
0006512     
Arg of perigee:   117
2860  deg
Mean anomaly:     242
8957  deg
Mean motion:   15
54400916  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2572
Checksum:              301


Coasting Arc #2 (Orbit 2587)
---------------------------------------

Vector Time (GMT): 2016/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908899
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2249001
35                 A    =         6788560
35  meter
 Y    =        6392518
29  meter          E    =           
0016053
 Z    =         331902
30                 I    =           52
01069
 XDOT =      -4355
164405                 Wp   =           73
02315
 YDOT =      -1857
547911  meter/sec      RA   =          107
19063  deg
 ZDOT =       6030
340789                 TA   =          290
53549
                                          MA   =          290
70768
                                          Ha   =            222
978  n
mi
                                          Hp   =            212
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7378613
36                 X    =        -2321929
25
 Y    =       20972829
03  feet           Y    =         6366960
71  meter
 Z    =        1088918
32                 Z    =          320799
31
 XDOT =     -14288
597129                 XDOT =       -4363
362651
 YDOT =      -6094
317293  feet/sec       YDOT =       -1906
295641  meter/sec
 ZDOT =      19784
582642                 ZDOT =        6009
164216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6868716
88                 X    =        -2093584
91
 Y    =      -21147812
45  feet           Y    =        -6445853
24  meter
 Z    =        1039226
94                 Z    =          316756
37
 XDOT =      13611
459559                 XDOT =        4148
772874
 YDOT =      -3413
468390  feet/sec       YDOT =       -1040
425165  meter/sec
 ZDOT =      19692
162907                 ZDOT =        6002
171254


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   16303
56368456  
00016717  00000-0  10270-3 0  9014
2 25544  51
6378 107
8164 0006893 122
3593 237
8227 15
54378377 25884


Satellite: ISS
Catalog Number: 25544
Epoch time:      16303
56368456   =   yrday
fracday
Element set:     901
Inclination:       51
6378  deg
RA of node:       107
8164  deg
Eccentricity:     
0006893     
Arg of perigee:   122
3593  deg
Mean anomaly:     237
8227  deg
Mean motion:   15
54378377  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2588
Checksum:              342


Coasting Arc #3 (Orbit 2595)
---------------------------------------

Vector Time (GMT): 2016/304/00:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893668
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4344832
05                 A    =         6779670
24  meter
 Y    =        2429707
17  meter          E    =           
0015138
 Z    =        4594482
57                 I    =           51
98646
 XDOT =       -654
258695                 Wp   =          117
53195
 YDOT =      -7002
525074  meter/sec      RA   =          104
61209  deg
 ZDOT =       3069
915272                 TA   =          301
87946
                                          MA   =          302
02667
                                          Ha   =            222
931  n
mi
                                          Hp   =            212
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14254698
33                 X    =        -4393997
33
 Y    =        7971480
22  feet           Y    =         2380845
78  meter
 Z    =       15073761
71                 Z    =         4573256
33
 XDOT =      -2146
518028                 XDOT =        -590
818750
 YDOT =     -22974
163629  feet/sec       YDOT =       -7009
486496  meter/sec
 ZDOT =      10071
900498                 ZDOT =        3066
891568

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4051651
74                 X    =        -1234943
45
 Y    =       15910088
83  feet           Y    =         4849395
08  meter
 Z    =       14980400
70                 Z    =         4566026
13
 XDOT =     -17066
034581                 XDOT =       -5201
727340
 YDOT =     -13863
203654  feet/sec       YDOT =       -4225
504474  meter/sec
 ZDOT =      10059
842855                 ZDOT =        3066
240102


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   16304
07801780  
00016717  00000-0  10270-3 0  9024
2 25544  51
6382 105
2557 0006565 122
6562 237
5225 15
54403819 25966


Satellite: ISS
Catalog Number: 25544
Epoch time:      16304
07801780   =   yrday
fracday
Element set:     902
Inclination:       51
6382  deg
RA of node:       105
2557  deg
Eccentricity:     
0006565     
Arg of perigee:   122
6562  deg
Mean anomaly:     237
5225  deg
Mean motion:   15
54403819  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2596
Checksum:              304


Coasting Arc #4 (Orbit 2596)
---------------------------------------

Vector Time (GMT): 2016/304/02:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893668
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3225647
83                 A    =         6786421
30  meter
 Y    =       -5517439
12  meter          E    =           
0012420
 Z    =       -2276449
22                 I    =           52
01130
 XDOT =       3345
749707                 Wp   =          128
44837
 YDOT =       4201
532567  meter/sec      RA   =          104
16068  deg
 ZDOT =      -5470
076321                 TA   =           76
74902
                                          MA   =           76
61051
                                          Ha   =            222
891  n
mi
                                          Hp   =            212
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10582834
10                 X    =         3298163
80
 Y    =      -18101834
37  feet           Y    =        -5480962
46  meter
 Z    =       -7468665
43                 Z    =        -2260602
90
 XDOT =      10976
869118                 XDOT =        3325
090388
 YDOT =      13784
555667  feet/sec       YDOT =        4238
831082  meter/sec
 ZDOT =     -17946
444624                 ZDOT =       -5453
873573

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15801575
22                 X    =        -4816320
13
 Y    =      -13821307
27  feet           Y    =        -4212734
46  meter
 Z    =       -7398339
97                 Z    =        -2255014
02
 XDOT =      14602
470817                 XDOT =        4450
833105
 YDOT =      -7174
751646  feet/sec       YDOT =       -2186
864302  meter/sec
 ZDOT =     -17876
202814                 ZDOT =       -5448
666618


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   16304
14231080  
00016717  00000-0  10270-3 0  9033
2 25544  51
6399 104
9344 0006552 121
1295 239
0502 15
54385178 25970


Satellite: ISS
Catalog Number: 25544
Epoch time:      16304
14231080   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       104
9344  deg
Eccentricity:     
0006552     
Arg of perigee:   121
1295  deg
Mean anomaly:     239
0502  deg
Mean motion:   15
54385178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2597
Checksum:              297


Coasting Arc #5 (Orbit 2612)
---------------------------------------

Vector Time (GMT): 2016/305/02:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893668
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3653785
33                 A    =         6782695
08  meter
 Y    =        4317507
54  meter          E    =           
0017660
 Z    =        3733286
86                 I    =           52
00661
 XDOT =      -2469
569162                 Wp   =          106
33556
 YDOT =      -5841
828349  meter/sec      RA   =           99
20504  deg
 ZDOT =       4317
338582                 TA   =          298
01153
                                          MA   =          298
19007
                                          Ha   =            222
837  n
mi
                                          Hp   =            212
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11987484
67                 X    =        -3719928
43
 Y    =       14165050
99  feet           Y    =         4276278
84  meter
 Z    =       12248316
46                 Z    =         3715376
30
 XDOT =      -8102
261031                 XDOT =       -2425
033141
 YDOT =     -19166
103508  feet/sec       YDOT =       -5869
195471  meter/sec
 ZDOT =      14164
496659                 ZDOT =        4305
450213

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11914166
28                 X    =         3631437
88
 Y    =       14294557
68  feet           Y    =         4356981
18  meter
 Z    =       12169140
36                 Z    =         3709153
98
 XDOT =     -19234
583317                 XDOT =       -5862
700995
 YDOT =       3955
613389  feet/sec       YDOT =        1205
670961  meter/sec
 ZDOT =      14113
438501                 ZDOT =        4301
776055


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   16305
17097248  
00016717  00000-0  10270-3 0  9044
2 25544  51
6405  99
8052 0006528 126
0896 234
0862 15
54402735 26132


Satellite: ISS
Catalog Number: 25544
Epoch time:      16305
17097248   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:        99
8052  deg
Eccentricity:     
0006528     
Arg of perigee:   126
0896  deg
Mean anomaly:     234
0862  deg
Mean motion:   15
54402735  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2613
Checksum:              310


Coasting Arc #6 (Orbit 2627)
---------------------------------------

Vector Time (GMT): 2016/306/02:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893668
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3968774
55                 A    =         6778803
98  meter
 Y    =       -2677900
57  meter          E    =           
0015881
 Z    =       -4812449
00                 I    =           51
99869
 XDOT =       1546
996704                 Wp   =           91
35637
 YDOT =       7020
040085  meter/sec      RA   =           94
23709  deg
 ZDOT =      -2638
392896                 TA   =          152
75642
                                          MA   =          152
67302
                                          Ha   =            222
748  n
mi
                                          Hp   =            212
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13020913
88                 X    =         4021802
00
 Y    =       -8785763
03  feet           Y    =        -2633222
77  meter
 Z    =      -15788874
67                 Z    =        -4793040
25
 XDOT =       5075
448503                 XDOT =        1481
198373
 YDOT =      23031
627574  feet/sec       YDOT =        7036
971634  meter/sec
 ZDOT =      -8656
144671                 ZDOT =       -2631
037869

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6681112
59                 X    =        -2036403
12
 Y    =      -14310418
65  feet           Y    =        -4361815
61  meter
 Z    =      -15703408
74                 Z    =        -4786398
99
 XDOT =      22500
700751                 XDOT =        6858
213589
 YDOT =      -1068
638060  feet/sec       YDOT =        -325
720881  meter/sec
 ZDOT =      -8625
158929                 ZDOT =       -2628
948441


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   16306
13533551  
00016717  00000-0  10270-3 0  9054
2 25544  51
6412  94
9954 0006500 127
4645 232
7100 15
54415209 26280


Satellite: ISS
Catalog Number: 25544
Epoch time:      16306
13533551   =   yrday
fracday
Element set:     905
Inclination:       51
6412  deg
RA of node:        94
9954  deg
Eccentricity:     
0006500     
Arg of perigee:   127
4645  deg
Mean anomaly:     232
7100  deg
Mean motion:   15
54415209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2628
Checksum:              288


Coasting Arc #7 (Orbit 2643)
---------------------------------------

Vector Time (GMT): 2016/307/02:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893668
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4132810
72                 A    =         6776557
13  meter
 Y    =         821090
65  meter          E    =           
0009284
 Z    =        5301505
61                 I    =           51
99298
 XDOT =       -630
888829                 Wp   =          127
39804
 YDOT =      -7618
167731  meter/sec      RA   =           89
26260  deg
 ZDOT =        681
772499                 TA   =          316
09156
                                          MA   =          316
16531
                                          Ha   =            222
696  n
mi
                                          Hp   =            212
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13559090
30                 X    =        -4167438
33
 Y    =        2693866
96  feet           Y    =          774681
30  meter
 Z    =       17393391
10                 Z    =         5281344
78
 XDOT =      -2069
845239                 XDOT =        -548
965487
 YDOT =     -24993
988619  feet/sec       YDOT =       -7624
764676  meter/sec
 ZDOT =       2236
786415                 ZDOT =         678
906893

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         816419
53                 X    =          248844
67
 Y    =       13910718
21  feet           Y    =         4239986
91  meter
 Z    =       17304949
61                 Z    =         5274548
64
 XDOT =     -24031
156552                 XDOT =       -7324
696517
 YDOT =      -1384
119950  feet/sec       YDOT =        -421
879761  meter/sec
 ZDOT =       2225
585641                 ZDOT =         678
358503


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   16307
16398046  
00016717  00000-0  10270-3 0  9067
2 25544  51
6412  89
8669 0006345 132
8013 227
3674 15
54451004 26449


Satellite: ISS
Catalog Number: 25544
Epoch time:      16307
16398046   =   yrday
fracday
Element set:     906
Inclination:       51
6412  deg
RA of node:        89
8669  deg
Eccentricity:     
0006345     
Arg of perigee:   132
8013  deg
Mean anomaly:     227
3674  deg
Mean motion:   15
54451004  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2644
Checksum:              310


Coasting Arc #8 (Orbit 2643)
---------------------------------------

Vector Time (GMT): 2016/307/03:38:29
935
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3928143
38                 A    =         6780599
37  meter
 Y    =        2434303
42  meter          E    =           
0014754
 Z    =       -4975507
66                 I    =           51
99928
 XDOT =      -1616
145203                 Wp   =          116
39215
 YDOT =       7146
707620  meter/sec      RA   =           89
05343  deg
 ZDOT =       2219
346649                 TA   =          175
19958
                                          MA   =          175
18542
                                          Ha   =            222
644  n
mi
                                          Hp   =            215
085

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12887609
53                 X    =         3924799
95
 Y    =        7986559
78  feet           Y    =         2478211
74  meter
 Z    =      -16323844
02                 Z    =        -4956433
39
 XDOT =      -5302
313658                 XDOT =       -1706
722315
 YDOT =      23447
203477  feet/sec       YDOT =        7128
128406  meter/sec
 ZDOT =       7281
321028                 ZDOT =        2211
275432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6675024
12                 X    =         2034547
35
 Y    =      -13712256
71  feet           Y    =        -4179495
85  meter
 Z    =      -16240737
94                 Z    =        -4950176
92
 XDOT =      22858
940768                 XDOT =        6967
405146
 YDOT =       2541
916983  feet/sec       YDOT =         774
776296  meter/sec
 ZDOT =       7244
705738                 ZDOT =        2208
186309


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   16307
16398163  
00016717  00000-0  10270-3 0  9078
2 25544  51
6426  89
8653 0003414 156
3626 203
7684 15
53570542 26449


Satellite: ISS
Catalog Number: 25544
Epoch time:      16307
16398163   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:        89
8653  deg
Eccentricity:     
0003414     
Arg of perigee:   156
3626  deg
Mean anomaly:     203
7684  deg
Mean motion:   15
53570542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2644
Checksum:              321


Coasting Arc #9 (Orbit 2659)
---------------------------------------

Vector Time (GMT): 2016/308/03:38:29
935
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3693094
49                 A    =         6783531
54  meter
 Y    =       -3829738
86  meter          E    =           
0011084
 Z    =        4198454
91                 I    =           52
00785
 XDOT =       2280
519273                 Wp   =           93
05719
 YDOT =      -6302
166482  meter/sec      RA   =           84
09184  deg
 ZDOT =      -3734
790175                 TA   =           35
12510
                                          MA   =           35
05207
                                          Ha   =            222
690  n
mi
                                          Hp   =            215
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12116451
75                 X    =        -3670389
69
 Y    =      -12564760
03  feet           Y    =        -3870910
52  meter
 Z    =       13774458
36                 Z    =         4180569
53
 XDOT =       7482
018611                 XDOT =        2368
964668
 YDOT =     -20676
399220  feet/sec       YDOT =       -6276
169699  meter/sec
 ZDOT =     -12253
248606                 ZDOT =       -3723
496809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11076794
48                 X    =        -3376206
96
 Y    =       13569054
76  feet           Y    =         4135847
89  meter
 Z    =       13696812
69                 Z    =         4174788
51
 XDOT =     -20420
294134                 XDOT =       -6224
105652
 YDOT =      -4325
823126  feet/sec       YDOT =       -1318
510889  meter/sec
 ZDOT =     -12202
653272                 ZDOT =       -3719
368717


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   16308
19318120  
00016717  00000-0  10270-3 0  9088
2 25544  51
6428  84
7402 0003414 160
7245 199
4037 15
53578117 26600


Satellite: ISS
Catalog Number: 25544
Epoch time:      16308
19318120   =   yrday
fracday
Element set:     908
Inclination:       51
6428  deg
RA of node:        84
7402  deg
Eccentricity:     
0003414     
Arg of perigee:   160
7245  deg
Mean anomaly:     199
4037  deg
Mean motion:   15
53578117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2660
Checksum:              302


Coasting Arc #10 (Orbit 2659)
---------------------------------------

Vector Time (GMT): 2016/308/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4158427
12                 A    =         6780249
08  meter
 Y    =        1831580
95  meter          E    =           
0014834
 Z    =       -5045810
14                 I    =           51
99788
 XDOT =       -798
787069                 Wp   =          115
86051
 YDOT =       7345
231708  meter/sec      RA   =           83
95748  deg
 ZDOT =       2006
227517                 TA   =          173
57253
                                          MA   =          173
55348
                                          Ha   =            222
497  n
mi
                                          Hp   =            215
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13643133
59                 X    =         4162147
83
 Y    =        6009123
85  feet           Y    =         1878104
02  meter
 Z    =      -16554495
20                 Z    =        -5025600
02
 XDOT =      -2620
692484                 XDOT =        -890
609590
 YDOT =      24098
529225  feet/sec       YDOT =        7335
785746  meter/sec
 ZDOT =       6582
111277                 ZDOT =        2002
124002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1723367
97                 X    =          525282
56
 Y    =      -14905927
01  feet           Y    =        -4543326
55  meter
 Z    =      -16466308
57                 Z    =        -5018930
85
 XDOT =      22737
324276                 XDOT =        6930
336439
 YDOT =      -4627
264587  feet/sec       YDOT =       -1410
390246  meter/sec
 ZDOT =       6562
817931                 ZDOT =        2000
346905


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   16308
19318016  
00016717  00000-0  10270-3 0  9093
2 25544  51
6437  84
7400 0003351 163
0036 197
1229 15
53591240 26602


Satellite: ISS
Catalog Number: 25544
Epoch time:      16308
19318016   =   yrday
fracday
Element set:     909
Inclination:       51
6437  deg
RA of node:        84
7400  deg
Eccentricity:     
0003351     
Arg of perigee:   163
0036  deg
Mean anomaly:     197
1229  deg
Mean motion:   15
53591240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2660
Checksum:              289


Coasting Arc #11 (Orbit 2675)
---------------------------------------

Vector Time (GMT): 2016/309/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4072364
00                 A    =         6782974
38  meter
 Y    =       -3272159
20  meter          E    =           
0010208
 Z    =        4317499
50                 I    =           52
00354
 XDOT =       1542
336499                 Wp   =           90
86835
 YDOT =      -6621
041974  meter/sec      RA   =           78
99405  deg
 ZDOT =      -3556
128158                 TA   =           35
19259
                                          MA   =           35
12522
                                          Ha   =            222
501  n
mi
                                          Hp   =            215
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13360774
29                 X    =        -4056444
23
 Y    =      -10735430
43  feet           Y    =        -3317610
08  meter
 Z    =       14165024
62                 Z    =         4297755
21
 XDOT =       5060
159119                 XDOT =        1633
534576
 YDOT =     -21722
578656  feet/sec       YDOT =       -6603
284621  meter/sec
 ZDOT =     -11667
087134                 ZDOT =       -3548
414179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6054100
58                 X    =        -1845289
86
 Y    =       16110038
03  feet           Y    =         4910339
59  meter
 Z    =       14079141
29                 Z    =         4291322
27
 XDOT =     -21072
897707                 XDOT =       -6423
019221
 YDOT =       2267
000670  feet/sec       YDOT =         690
981804  meter/sec
 ZDOT =     -11632
094191                 ZDOT =       -3545
462309


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   16309
22237014  
00016717  00000-0  10270-3 0  9108
2 25544  51
6443  79
6143 0003199 165
2992 194
8254 15
53625489 26763


Satellite: ISS
Catalog Number: 25544
Epoch time:      16309
22237014   =   yrday
fracday
Element set:     910
Inclination:       51
6443  deg
RA of node:        79
6143  deg
Eccentricity:     
0003199     
Arg of perigee:   165
2992  deg
Mean anomaly:     194
8254  deg
Mean motion:   15
53625489  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2676
Checksum:              325


Coasting Arc #12 (Orbit 2690)
---------------------------------------

Vector Time (GMT): 2016/310/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3924320
96                 A    =         6786445
54  meter
 Y    =        4487204
14  meter          E    =           
0005648
 Z    =       -3250636
09                 I    =           52
00739
 XDOT =      -2322
502422                 Wp   =          114
94302
 YDOT =       5502
599151  meter/sec      RA   =           74
03762  deg
 ZDOT =       4796
193378                 TA   =          207
64938
                                          MA   =          207
67942
                                          Ha   =            222
337  n
mi
                                          Hp   =            215
273

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12875068
75                 X    =         3889642
72
 Y    =       14721798
37  feet           Y    =         4530894
64  meter
 Z    =      -10664816
57                 Z    =        -3231656
58
 XDOT =      -7619
758603                 XDOT =       -2407
159570
 YDOT =      18053
146820  feet/sec       YDOT =        5476
154017  meter/sec
 ZDOT =      15735
542579                 ZDOT =        4784
705406

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9711403
64                 X    =         2960035
83
 Y    =      -17027511
97  feet           Y    =        -5189985
65  meter
 Z    =      -10582510
61                 Z    =        -3225549
23
 XDOT =      18342
591714                 XDOT =        5590
821954
 YDOT =        722
407070  feet/sec       YDOT =         220
189675  meter/sec
 ZDOT =      15684
210167                 ZDOT =        4780
547259


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   16310
18722994  
00016717  00000-0  10270-3 0  9112
2 25544  51
6438  74
8086 0003174 169
3054 190
8166 15
53604820 26918


Satellite: ISS
Catalog Number: 25544
Epoch time:      16310
18722994   =   yrday
fracday
Element set:     911
Inclination:       51
6438  deg
RA of node:        74
8086  deg
Eccentricity:     
0003174     
Arg of perigee:   169
3054  deg
Mean anomaly:     190
8166  deg
Mean motion:   15
53604820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2691
Checksum:              314


Coasting Arc #13 (Orbit 2706)
---------------------------------------

Vector Time (GMT): 2016/311/04:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3637322
50                 A    =         6789423
10  meter
 Y    =       -5404717
88  meter          E    =           
0015945
 Z    =        1880432
35                 I    =           52
00739
 XDOT =       3162
019696                 Wp   =          123
54312
 YDOT =      -4105
401594  meter/sec      RA   =           69
08943  deg
 ZDOT =      -5657
597929                 TA   =           35
85373
                                          MA   =           35
74681
                                          Ha   =            222
391  n
mi
                                          Hp   =            215
262

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11933472
76                 X    =        -3585749
71
 Y    =      -17732014
04  feet           Y    =        -5445104
50  meter
 Z    =        6169397
46                 Z    =         1862888
13
 XDOT =      10374
080366                 XDOT =        3235
174964
 YDOT =     -13469
165336  feet/sec       YDOT =       -4069
632740  meter/sec
 ZDOT =     -18561
672994                 ZDOT =       -5642
059680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12578204
13                 X    =        -3833836
62
 Y    =       17307539
59  feet           Y    =         5275338
07  meter
 Z    =        6093555
06                 Z    =         1857315
58
 XDOT =     -14982
177804                 XDOT =       -4566
567795
 YDOT =      -4347
204738  feet/sec       YDOT =       -1325
028004  meter/sec
 ZDOT =     -18492
848016                 ZDOT =       -5636
620075


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   16311
21640802  
00016717  00000-0  10270-3 0  9125
2 25544  51
6437  69
6831 0003298 171
7134 188
4074 15
53594810 27076


Satellite: ISS
Catalog Number: 25544
Epoch time:      16311
21640802   =   yrday
fracday
Element set:     912
Inclination:       51
6437  deg
RA of node:        69
6831  deg
Eccentricity:     
0003298     
Arg of perigee:   171
7134  deg
Mean anomaly:     188
4074  deg
Mean motion:   15
53594810  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2707
Checksum:              305


Coasting Arc #14 (Orbit 2712)
---------------------------------------

Vector Time (GMT): 2016/311/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3985930
25                 A    =         6778884
81  meter
 Y    =       -1298943
45  meter          E    =           
0015570
 Z    =       -5340231
03                 I    =           51
96738
 XDOT =       2751
014621                 Wp   =          105
72837
 YDOT =       7138
312899  meter/sec      RA   =           67
08589  deg
 ZDOT =        313
699817                 TA   =          167
27301
                                          MA   =          167
23366
                                          Ha   =            222
288  n
mi
                                          Hp   =            215
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13077199
00                 X    =         4026100
07
 Y    =       -4261625
50  feet           Y    =        -1254145
52  meter
 Z    =      -17520443
00                 Z    =        -5320770
50
 XDOT =       9025
638521                 XDOT =        2669
463877
 YDOT =      23419
661742  feet/sec       YDOT =        7168
620615  meter/sec
 ZDOT =       1029
198874                 ZDOT =         326
865655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1093538
16                 X    =          333310
43
 Y    =       13819077
89  feet           Y    =         4212054
94  meter
 Z    =      -17434958
24                 Z    =        -5314175
27
 XDOT =     -23863
769749                 XDOT =       -7273
677019
 YDOT =       3271
885644  feet/sec       YDOT =         997
270744  meter/sec
 ZDOT =       1085
536097                 ZDOT =         330
871402


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   16311
60234579  
00016717  00000-0  10270-3 0  9139
2 25544  51
6434  67
7572 0003605 177
3012 182
8161 15
53616574 27137


Satellite: ISS
Catalog Number: 25544
Epoch time:      16311
60234579   =   yrday
fracday
Element set:     913
Inclination:       51
6434  deg
RA of node:        67
7572  deg
Eccentricity:     
0003605     
Arg of perigee:   177
3012  deg
Mean anomaly:     182
8161  deg
Mean motion:   15
53616574  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2713
Checksum:              300


Coasting Arc #15 (Orbit 2728)
---------------------------------------

Vector Time (GMT): 2016/312/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4543458
68                 A    =         6780070
40  meter
 Y    =        -179922
74  meter          E    =           
0004970
 Z    =        5024995
30                 I    =           51
95917
 XDOT =      -1970
524924                 Wp   =           91
44426
 YDOT =      -7128
816002  meter/sec      RA   =           62
11419  deg
 ZDOT =      -2035
334453                 TA   =           18
25219
                                          MA   =           18
23436
                                          Ha   =            222
249  n
mi
                                          Hp   =            215
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14906360
49                 X    =        -4565518
66
 Y    =        -590297
70  feet           Y    =         -230854
02  meter
 Z    =       16486205
06                 Z    =         5002870
43
 XDOT =      -6464
976784                 XDOT =       -1880
775309
 YDOT =     -23388
503945  feet/sec       YDOT =       -7150
349944  meter/sec
 ZDOT =      -6677
606473                 ZDOT =       -2044
688807

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3799100
32                 X    =         1157965
78
 Y    =      -14536156
32  feet           Y    =        -4430620
45  meter
 Z    =       16389325
42                 Z    =         4995466
39
 XDOT =      23162
462198                 XDOT =        7059
918478
 YDOT =      -1525
958837  feet/sec       YDOT =        -465
112253  meter/sec
 ZDOT =      -6717
239780                 ZDOT =       -2047
414685


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   16312
63150987  
00016717  00000-0  10270-3 0  9144
2 25544  51
6442  62
6306 0003457 181
0434 179
0712 15
53668652 27291


Satellite: ISS
Catalog Number: 25544
Epoch time:      16312
63150987   =   yrday
fracday
Element set:     914
Inclination:       51
6442  deg
RA of node:        62
6306  deg
Eccentricity:     
0003457     
Arg of perigee:   181
0434  deg
Mean anomaly:     179
0712  deg
Mean motion:   15
53668652  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2729
Checksum:              309


Coasting Arc #16 (Orbit 2743)
---------------------------------------

Vector Time (GMT): 2016/313/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5016025
70                 A    =         6782953
66  meter
 Y    =        1562951
19  meter          E    =           
0009934
 Z    =       -4300752
31                 I    =           51
95157
 XDOT =        986
032932                 Wp   =          129
30467
 YDOT =       6696
195748  meter/sec      RA   =           57
14792  deg
 ZDOT =       3582
912692                 TA   =          177
14695
                                          MA   =          177
14128
                                          Ha   =            222
082  n
mi
                                          Hp   =            215
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16456777
22                 X    =         5019067
07
 Y    =        5127792
61  feet           Y    =         1619060
64  meter
 Z    =      -14110079
77                 Z    =        -4276378
03
 XDOT =       3235
016180                 XDOT =         893
676584
 YDOT =      21969
146156  feet/sec       YDOT =        6706
705935  meter/sec
 ZDOT =      11754
962899                 ZDOT =        3587
478148

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8300249
39                 X    =        -2529916
01
 Y    =       15205883
06  feet           Y    =         4634753
16  meter
 Z    =      -14003610
43                 Z    =        -4268300
46
 XDOT =     -21051
956501                 XDOT =       -6416
636341
 YDOT =       -646
762601  feet/sec       YDOT =        -197
133241  meter/sec
 ZDOT =      11773
691636                 ZDOT =        3588
621211


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   16313
59634576  
00016717  00000-0  10270-3 0  9152
2 25544  51
6429  57
8256 0003479 181
4699 178
6443 15
53671304 27448


Satellite: ISS
Catalog Number: 25544
Epoch time:      16313
59634576   =   yrday
fracday
Element set:     915
Inclination:       51
6429  deg
RA of node:        57
8256  deg
Eccentricity:     
0003479     
Arg of perigee:   181
4699  deg
Mean anomaly:     178
6443  deg
Mean motion:   15
53671304  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2744
Checksum:              344


Coasting Arc #17 (Orbit 2759)
---------------------------------------

Vector Time (GMT): 2016/314/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5305024
47                 A    =         6786417
67  meter
 Y    =       -2767292
89  meter          E    =           
0013183
 Z    =        3186578
30                 I    =           51
94524
 XDOT =        185
059790                 Wp   =          108
78014
 YDOT =      -5946
766812  meter/sec      RA   =           52
18775  deg
 ZDOT =      -4844
017041                 TA   =           34
56706
                                          MA   =           34
48142
                                          Ha   =            222
049  n
mi
                                          Hp   =            215
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17404935
93                 X    =        -5289164
88
 Y    =       -9079044
90  feet           Y    =        -2826528
43  meter
 Z    =       10454653
22                 Z    =         3160846
06
 XDOT =        607
151542                 XDOT =         275
074817
 YDOT =     -19510
389803  feet/sec       YDOT =       -5944
194241  meter/sec
 ZDOT =     -15892
444360                 ZDOT =       -4842
899173

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12091107
82                 X    =         3685369
66
 Y    =      -15540239
40  feet           Y    =        -4736664
97  meter
 Z    =       10342470
50                 Z    =         3152385
01
 XDOT =      17927
683807                 XDOT =        5464
358024
 YDOT =       3348
888048  feet/sec       YDOT =        1020
741077  meter/sec
 ZDOT =     -15886
413131                 ZDOT =       -4842
178722


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   16314
62549496  
00016717  00000-0  10270-3 0  9164
2 25544  51
6432  52
6992 0003339 187
0414 173
0692 15
53680563 27604


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
62549496   =   yrday
fracday
Element set:     916
Inclination:       51
6432  deg
RA of node:        52
6992  deg
Eccentricity:     
0003339     
Arg of perigee:   187
0414  deg
Mean anomaly:     173
0692  deg
Mean motion:   15
53680563  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2760
Checksum:              322


Coasting Arc #18 (Orbit 2764)
---------------------------------------

Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5334427
12                 A    =         6787877
08  meter
 Y    =       -3267068
04  meter          E    =           
0014328
 Z    =        2614924
79                 I    =           51
94211
 XDOT =        794
812885                 Wp   =          115
25128
 YDOT =      -5524
272627  meter/sec      RA   =           50
58912  deg
 ZDOT =      -5264
075154                 TA   =           35
41942
                                          MA   =           35
32435
                                          Ha   =            222
020  n
mi
                                          Hp   =            215
483

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17501401
30                 X    =        -5310199
84
 Y    =      -10718727
16  feet           Y    =        -3326585
61  meter
 Z    =        8579149
56                 Z    =         2589070
04
 XDOT =       2607
653823                 XDOT =         882
098669
 YDOT =     -18124
254027  feet/sec       YDOT =       -5514
896683  meter/sec
 ZDOT =     -17270
587774                 ZDOT =       -5260
001837

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19843941
81                 X    =        -6048433
46
 Y    =       -5415518
14  feet           Y    =        -1650649
93  meter
 Z    =        8466528
42                 Z    =         2580597
86
 XDOT =      -2820
847011                 XDOT =        -859
794169
 YDOT =     -16720
390830  feet/sec       YDOT =       -5096
375125  meter/sec
 ZDOT =     -17251
689736                 ZDOT =       -5258
315032


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   16314
94710409  
00016717  00000-0  10270-3 0  9174
2 25544  51
6418  51
0980 0003030 186
3845 173
7269 15
53657661 27651


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
94710409   =   yrday
fracday
Element set:     917
Inclination:       51
6418  deg
RA of node:        51
0980  deg
Eccentricity:     
0003030     
Arg of perigee:   186
3845  deg
Mean anomaly:     173
7269  deg
Mean motion:   15
53657661  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2765
Checksum:              319


Coasting Arc #19 (Orbit 2779)
---------------------------------------

Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5284322
98                 A    =         6790106
36  meter
 Y    =        4098045
24  meter          E    =           
0006921
 Z    =       -1165132
34                 I    =           51
92885
 XDOT =      -2132
794999                 Wp   =           49
43102
 YDOT =       4416
842106  meter/sec      RA   =           45
63789  deg
 ZDOT =       5889
313700                 TA   =          297
97523
                                          MA   =          298
04525
                                          Ha   =            221
843  n
mi
                                          Hp   =            215
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17337017
66                 X    =         5243764
67
 Y    =       13445030
30  feet           Y    =         4156911
25  meter
 Z    =       -3822612
68                 Z    =        -1139560
64
 XDOT =      -6997
358921                 XDOT =       -2210
635054
 YDOT =      14490
951791  feet/sec       YDOT =        4392
556820  meter/sec
 ZDOT =      19321
895342                 ZDOT =        5878
763628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20550481
79                 X    =         6263786
85
 Y    =        7736703
98  feet           Y    =         2358147
37  meter
 Z    =       -3711401
17                 Z    =        -1131235
08
 XDOT =      -1975
215984                 XDOT =        -602
045832
 YDOT =      14448
803858  feet/sec       YDOT =        4403
995416  meter/sec
 ZDOT =      19274
836196                 ZDOT =        5874
970073


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   16315
91191945  
00016717  00000-0  10270-3 0  9181
2 25544  51
6421  46
2920 0002944 189
9741 170
1353 15
53672882 27806


Satellite: ISS
Catalog Number: 25544
Epoch time:      16315
91191945   =   yrday
fracday
Element set:     918
Inclination:       51
6421  deg
RA of node:        46
2920  deg
Eccentricity:     
0002944     
Arg of perigee:   189
9741  deg
Mean anomaly:     170
1353  deg
Mean motion:   15
53672882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2780
Checksum:              321


Coasting Arc #20 (Orbit 2795)
---------------------------------------

Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893219
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4912539
73                 A    =         6790544
28  meter
 Y    =       -4658836
73  meter          E    =           
0012983
 Z    =        -420778
94                 I    =           51
90772
 XDOT =       3529
300060                 Wp   =          148
32409
 YDOT =      -3186
537607  meter/sec      RA   =           40
68918  deg
 ZDOT =      -6017
689549                 TA   =           36
19649
                                          MA   =           36
10869
                                          Ha   =            221
729  n
mi
                                          Hp   =            215
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16117256
33                 X    =        -4858034
30
 Y    =      -15284897
42  feet           Y    =        -4713467
31  meter
 Z    =       -1380508
33                 Z    =         -444510
79
 XDOT =      11579
068438                 XDOT =        3593
902467
 YDOT =     -10454
519709  feet/sec       YDOT =       -3146
709658  meter/sec
 ZDOT =     -19743
075947                 ZDOT =       -6000
387631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20061212
14                 X    =        -6114657
46
 Y    =       -9520857
12  feet           Y    =        -2901957
25  meter
 Z    =       -1483540
24                 Z    =         -452183
07
 XDOT =       7182
339656                 XDOT =        2189
177127
 YDOT =     -12114
356319  feet/sec       YDOT =       -3692
455806  meter/sec
 ZDOT =     -19666
680436                 ZDOT =       -5994
404197


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   16316
94104704  
00016717  00000-0  10270-3 0  9193
2 25544  51
6426  41
1656 0002879 193
9610 166
1463 15
53681174 27966


Satellite: ISS
Catalog Number: 25544
Epoch time:      16316
94104704   =   yrday
fracday
Element set:     919
Inclination:       51
6426  deg
RA of node:        41
1656  deg
Eccentricity:     
0002879     
Arg of perigee:   193
9610  deg
Mean anomaly:     166
1463  deg
Mean motion:   15
53681174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2796
Checksum:              323
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