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

 
Date: May 14th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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


135/07:32:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 213 1

Coasting Arc #1 (Orbit 3956)
---------------------------------------

Vector Time (GMT): 2016/134/09:28:33
804
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4746320
09                 A    =         6787751
16  meter
 Y    =        4778018
50  meter          E    =           
0015021
 Z    =         788654
05                 I    =           51
37026
 XDOT =      -2925
797059                 Wp   =          124
50396
 YDOT =       3896
259317  meter/sec      RA   =          230
56033  deg
 ZDOT =      -5924
788832                 TA   =           46
93381
                                          MA   =           46
80816
                                          Ha   =            220
889  n
mi
                                          Hp   =            213
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15571916
29                 X    =         4688707
37
 Y    =       15675913
72  feet           Y    =         4830772
86  meter
 Z    =        2587447
68                 Z    =          811570
77
 XDOT =      -9599
071716                 XDOT =       -2940
368351
 YDOT =      12783
003009  feet/sec       YDOT =        3863
459773  meter/sec
 ZDOT =     -19438
283570                 ZDOT =       -5939
036988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18654166
29                 X    =         5685789
89
 Y    =       11820327
45  feet           Y    =         3602835
81  meter
 Z    =        2686200
32                 Z    =          818753
86
 XDOT =      -5528
987390                 XDOT =       -1685
235356
 YDOT =      13209
080010  feet/sec       YDOT =        4026
127587  meter/sec
 ZDOT =     -19500
865626                 ZDOT =       -5943
863843


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   16134
42860402  
00016717  00000-0  10270-3 0  9008
2 25544  51
6399 231
4325 0001724 108
6422 251
4918 15
54574644 39571


Satellite: ISS
Catalog Number: 25544
Epoch time:      16134
42860402   =   yrday
fracday
Element set:     900
Inclination:       51
6399  deg
RA of node:       231
4325  deg
Eccentricity:     
0001724     
Arg of perigee:   108
6422  deg
Mean anomaly:     251
4918  deg
Mean motion:   15
54574644  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3957
Checksum:              303


Coasting Arc #2 (Orbit 3970)
---------------------------------------

Vector Time (GMT): 2016/135/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3690880
99                 A    =         6776229
78  meter
 Y    =        2218443
56  meter          E    =           
0016317
 Z    =       -5246251
89                 I    =           51
35102
 XDOT =      -4776
335312                 Wp   =           97
80267
 YDOT =      -5923
363472  meter/sec      RA   =          225
95967  deg
 ZDOT =        855
632634                 TA   =          180
42272
                                          MA   =          180
42410
                                          Ha   =            220
910  n
mi
                                          Hp   =            213
148

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12109189
60                 X    =        -3689929
70
 Y    =        7278358
13  feet           Y    =         2177175
06  meter
 Z    =      -17212112
49                 Z    =        -5264179
02
 XDOT =     -15670
391444                 XDOT =       -4713
900110
 YDOT =     -19433
607190  feet/sec       YDOT =       -5976
426547  meter/sec
 ZDOT =       2807
193682                 ZDOT =         832
581839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13497929
99                 X    =        -4114169
06
 Y    =        3835615
37  feet           Y    =         1169095
56  meter
 Z    =      -17290394
07                 Z    =        -5270112
11
 XDOT =      -9695
206201                 XDOT =       -2955
098850
 YDOT =     -21912
754823  feet/sec       YDOT =       -6679
007670  meter/sec
 ZDOT =       2708
038956                 ZDOT =         825
410274


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   16135
32857121  
00016717  00000-0  10270-3 0  9013
2 25544  51
6397 226
9443 0001817 106
4066 253
7287 15
54593931 39712


Satellite: ISS
Catalog Number: 25544
Epoch time:      16135
32857121   =   yrday
fracday
Element set:     901
Inclination:       51
6397  deg
RA of node:       226
9443  deg
Eccentricity:     
0001817     
Arg of perigee:   106
4066  deg
Mean anomaly:     253
7287  deg
Mean motion:   15
54593931  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3971
Checksum:              319


Coasting Arc #3 (Orbit 3986)
---------------------------------------

Vector Time (GMT): 2016/136/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4881010
36                 A    =         6778736
73  meter
 Y    =        -681118
51  meter          E    =           
0009450
 Z    =        4647915
35                 I    =           51
38206
 XDOT =       3592
649187                 Wp   =           72
23220
 YDOT =       6145
341705  meter/sec      RA   =          220
93787  deg
 ZDOT =      -2864
624585                 TA   =           46
34961
                                          MA   =           46
27129
                                          Ha   =            220
825  n
mi
                                          Hp   =            213
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16013813
51                 X    =         4865686
29
 Y    =       -2234640
78  feet           Y    =         -626621
51  meter
 Z    =       15249066
11                 Z    =         4671589
03
 XDOT =      11786
906782                 XDOT =        3537
578643
 YDOT =      20161
882234  feet/sec       YDOT =        6185
209198  meter/sec
 ZDOT =      -9398
374623                 ZDOT =       -2847
305987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15971055
55                 X    =         4867977
73
 Y    =        1791470
82  feet           Y    =          546040
31  meter
 Z    =       15352064
25                 Z    =         4679309
18
 XDOT =       6596
612826                 XDOT =        2010
647589
 YDOT =      21307
876444  feet/sec       YDOT =        6494
640740  meter/sec
 ZDOT =      -9324
152090                 ZDOT =       -2842
001557


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   16136
35709557  
00016717  00000-0  10270-3 0  9027
2 25544  51
6394 221
8123 0001878 109
2384 250
8972 15
54570963 39875


Satellite: ISS
Catalog Number: 25544
Epoch time:      16136
35709557   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:       221
8123  deg
Eccentricity:     
0001878     
Arg of perigee:   109
2384  deg
Mean anomaly:     250
8972  deg
Mean motion:   15
54570963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3987
Checksum:              336


Coasting Arc #4 (Orbit 4001)
---------------------------------------

Vector Time (GMT): 2016/137/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5769680
00                 A    =         6782634
51  meter
 Y    =        -737372
37  meter          E    =           
0006935
 Z    =       -3495812
32                 I    =           51
42113
 XDOT =      -1976
403984                 Wp   =           99
66004
 YDOT =      -5872
329845  meter/sec      RA   =          215
93010  deg
 ZDOT =       4507
128642                 TA   =          219
12063
                                          MA   =          219
17079
                                          Ha   =            220
850  n
mi
                                          Hp   =            213
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18929396
32                 X    =        -5744024
37
 Y    =       -2419200
68  feet           Y    =         -801749
30  meter
 Z    =      -11469200
53                 Z    =        -3523777
97
 XDOT =      -6484
265041                 XDOT =       -1932
485150
 YDOT =     -19266
174031  feet/sec       YDOT =       -5894
185766  meter/sec
 ZDOT =      14787
167461                 ZDOT =        4497
634313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17780708
72                 X    =        -5419560
02
 Y    =       -6724658
32  feet           Y    =        -2049675
86  meter
 Z    =      -11590621
45                 Z    =        -3532821
42
 XDOT =      -2425
294858                 XDOT =        -739
229873
 YDOT =     -18968
570506  feet/sec       YDOT =       -5781
620290  meter/sec
 ZDOT =      14746
891917                 ZDOT =        4494
852656


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   16137
32132757  
00016717  00000-0  10270-3 0  9038
2 25544  51
6402 217
0031 0001830 111
3364 248
7984 15
54611226 40026


Satellite: ISS
Catalog Number: 25544
Epoch time:      16137
32132757   =   yrday
fracday
Element set:     903
Inclination:       51
6402  deg
RA of node:       217
0031  deg
Eccentricity:     
0001830     
Arg of perigee:   111
3364  deg
Mean anomaly:     248
7984  deg
Mean motion:   15
54611226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4002
Checksum:              268


Coasting Arc #5 (Orbit 4017)
---------------------------------------

Vector Time (GMT): 2016/138/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6206719
40                 A    =         6786353
59  meter
 Y    =        1982340
61  meter          E    =           
0015688
 Z    =        1870919
84                 I    =           51
45995
 XDOT =         30
604365                 Wp   =          113
76691
 YDOT =       5230
796225  meter/sec      RA   =          210
93526  deg
 ZDOT =      -5612
730501                 TA   =           45
57118
                                          MA   =           45
44290
                                          Ha   =            220
762  n
mi
                                          Hp   =            213
284

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20363252
61                 X    =         6175002
82
 Y    =        6503742
17  feet           Y    =         2051570
93  meter
 Z    =        6138188
45                 Z    =         1900993
92
 XDOT =        100
408022                 XDOT =           -
625388
 YDOT =      17161
404939  feet/sec       YDOT =        5230
963900  meter/sec
 ZDOT =     -18414
470148                 ZDOT =       -5612
657636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18449429
90                 X    =         5623386
23
 Y    =       10722013
11  feet           Y    =         3268069
59  meter
 Z    =        6268576
23                 Z    =         1910662
04
 XDOT =      -2693
883611                 XDOT =        -821
095725
 YDOT =      15460
075980  feet/sec       YDOT =        4712
231159  meter/sec
 ZDOT =     -18415
030326                 ZDOT =       -5612
901243


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   16138
34983457  
00016717  00000-0  10270-3 0  9043
2 25544  51
6400 211
8720 0001736 117
2802 242
8528 15
54620734 40188


Satellite: ISS
Catalog Number: 25544
Epoch time:      16138
34983457   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       211
8720  deg
Eccentricity:     
0001736     
Arg of perigee:   117
2802  deg
Mean anomaly:     242
8528  deg
Mean motion:   15
54620734  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4018
Checksum:              295


Coasting Arc #6 (Orbit 4032)
---------------------------------------

Vector Time (GMT): 2016/139/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6113964
00                 A    =         6787839
15  meter
 Y    =       -2936437
92  meter          E    =           
0012629
 Z    =         -44155
32                 I    =           51
49474
 XDOT =       2038
903842                 Wp   =           52
84062
 YDOT =      -4317
518897  meter/sec      RA   =          205
95098  deg
 ZDOT =       6001
120772                 TA   =          306
68274
                                          MA   =          306
79872
                                          Ha   =            220
771  n
mi
                                          Hp   =            213
289

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20058936
99                 X    =        -6080459
12
 Y    =       -9633982
69  feet           Y    =        -3004621
00  meter
 Z    =        -144866
54                 Z    =          -73774
58
 XDOT =       6689
317068                 XDOT =        2057
880552
 YDOT =     -14165
088245  feet/sec       YDOT =       -4294
612527  meter/sec
 ZDOT =      19688
716444                 ZDOT =        6011
071427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17750429
64                 X    =        -5410330
96
 Y    =      -13418018
08  feet           Y    =        -4089811
91  meter
 Z    =        -273130
66                 Z    =          -83250
22
 XDOT =       8260
716295                 XDOT =        2517
866327
 YDOT =     -11287
379052  feet/sec       YDOT =       -3440
393135  meter/sec
 ZDOT =      19732
693897                 ZDOT =        6014
525100


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   16139
31405196  
00016717  00000-0  10270-3 0  9051
2 25544  51
6417 207
0622 0001761 116
0673 244
0661 15
54639571 40333


Satellite: ISS
Catalog Number: 25544
Epoch time:      16139
31405196   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:       207
0622  deg
Eccentricity:     
0001761     
Arg of perigee:   116
0673  deg
Mean anomaly:     244
0661  deg
Mean motion:   15
54639571  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4033
Checksum:              288


Coasting Arc #7 (Orbit 4048)
---------------------------------------

Vector Time (GMT): 2016/140/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5423333
10                 A    =         6786404
60  meter
 Y    =        3639174
99  meter          E    =           
0009011
 Z    =       -1833330
50                 I    =           51
51851
 XDOT =      -4069
155167                 Wp   =          137
44356
 YDOT =       3237
050497  meter/sec      RA   =          200
96926  deg
 ZDOT =      -5634
466099                 TA   =           62
75306
                                          MA   =           62
66129
                                          Ha   =            220
782  n
mi
                                          Hp   =            213
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17793087
61                 X    =         5391141
55
 Y    =       11939550
49  feet           Y    =         3699642
38  meter
 Z    =       -6014863
84                 Z    =        -1807062
89
 XDOT =     -13350
246612                 XDOT =       -4077
679940
 YDOT =      10620
244413  feet/sec       YDOT =        3191
499016  meter/sec
 ZDOT =     -18485
781166                 ZDOT =       -5654
253997

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15371478
21                 X    =         4685226
56
 Y    =       14973911
73  feet           Y    =         4564048
29  meter
 Z    =       -5901274
84                 Z    =        -1798708
57
 XDOT =     -13844
853370                 XDOT =       -4219
911307
 YDOT =       6922
948552  feet/sec       YDOT =        2110
114719  meter/sec
 ZDOT =     -18572
348831                 ZDOT =       -5660
851924


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   16140
34254335  
00016717  00000-0  10270-3 0  9064
2 25544  51
6409 201
9317 0001764 118
0999 242
0333 15
54661245 40498


Satellite: ISS
Catalog Number: 25544
Epoch time:      16140
34254335   =   yrday
fracday
Element set:     906
Inclination:       51
6409  deg
RA of node:       201
9317  deg
Eccentricity:     
0001764     
Arg of perigee:   118
0999  deg
Mean anomaly:     242
0333  deg
Mean motion:   15
54661245  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4049
Checksum:              296


Coasting Arc #8 (Orbit 4064)
---------------------------------------

Vector Time (GMT): 2016/141/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4203591
30                 A    =         6782733
08  meter
 Y    =       -4049706
14  meter          E    =           
0013839
 Z    =        3443983
82                 I    =           51
53715
 XDOT =       5791
665188                 Wp   =           94
90286
 YDOT =      -2114
243550  meter/sec      RA   =          195
98151  deg
 ZDOT =       4566
002551                 TA   =          305
56268
                                          MA   =          305
69161
                                          Ha   =            220
709  n
mi
                                          Hp   =            213
284

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13791310
03                 X    =        -4174723
76
 Y    =      -13286437
45  feet           Y    =        -4096552
25  meter
 Z    =       11299159
52                 Z    =         3423633
35
 XDOT =      19001
526206                 XDOT =        5792
696638
 YDOT =      -6936
494585  feet/sec       YDOT =       -2049
471752  meter/sec
 ZDOT =      14980
323329                 ZDOT =        4594
139955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11491780
59                 X    =        -3502694
72
 Y    =      -15383275
90  feet           Y    =        -4688822
49  meter
 Z    =       11211354
07                 Z    =         3417220
72
 XDOT =      18665
627064                 XDOT =        5689
283129
 YDOT =      -2895
771426  feet/sec       YDOT =        -882
631131  meter/sec
 ZDOT =      15103
016493                 ZDOT =        4603
399427


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   16141
37102713  
00016717  00000-0  10270-3 0  9071
2 25544  51
6413 196
8013 0001738 127
0524 233
0788 15
54693135 40658


Satellite: ISS
Catalog Number: 25544
Epoch time:      16141
37102713   =   yrday
fracday
Element set:     907
Inclination:       51
6413  deg
RA of node:       196
8013  deg
Eccentricity:     
0001738     
Arg of perigee:   127
0524  deg
Mean anomaly:     233
0788  deg
Mean motion:   15
54693135  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4065
Checksum:              293


Coasting Arc #9 (Orbit 4079)
---------------------------------------

Vector Time (GMT): 2016/142/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2510702
45                 A    =         6778667
73  meter
 Y    =        4251762
51  meter          E    =           
0011401
 Z    =       -4655069
32                 I    =           51
55491
 XDOT =      -7023
026100                 Wp   =           77
75668
 YDOT =        979
570748  meter/sec      RA   =          190
98339  deg
 ZDOT =      -2896
795865                 TA   =          163
38972
                                          MA   =          163
35234
                                          Ha   =            220
687  n
mi
                                          Hp   =            213
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8237212
76                 X    =         2485584
33
 Y    =       13949352
07  feet           Y    =         4279698
72  meter
 Z    =      -15272537
15                 Z    =        -4642933
45
 XDOT =     -23041
424213                 XDOT =       -7019
386283
 YDOT =       3213
814790  feet/sec       YDOT =         901
055140  meter/sec
 ZDOT =      -9503
923441                 ZDOT =       -2930
903715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6189023
38                 X    =         1886414
33
 Y    =       15023966
36  feet           Y    =         4579304
95  meter
 Z    =      -15220476
76                 Z    =        -4639201
32
 XDOT =     -22106
763002                 XDOT =       -6738
141363
 YDOT =       -659
771580  feet/sec       YDOT =        -201
098378  meter/sec
 ZDOT =      -9652
404819                 ZDOT =       -2942
052989


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   16142
33522650  
00016717  00000-0  10270-3 0  9085
2 25544  51
6418 191
9916 0001682 127
1791 232
9516 15
54661232 40803


Satellite: ISS
Catalog Number: 25544
Epoch time:      16142
33522650   =   yrday
fracday
Element set:     908
Inclination:       51
6418  deg
RA of node:       191
9916  deg
Eccentricity:     
0001682     
Arg of perigee:   127
1791  deg
Mean anomaly:     232
9516  deg
Mean motion:   15
54661232  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4080
Checksum:              302


Coasting Arc #10 (Orbit 4095)
---------------------------------------

Vector Time (GMT): 2016/143/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -549312
94                 A    =         6775920
36  meter
 Y    =       -4244525
33  meter          E    =           
0005106
 Z    =        5249810
04                 I    =           51
57777
 XDOT =       7622
012143                 Wp   =          123
60603
 YDOT =        100
024213  meter/sec      RA   =          185
97617  deg
 ZDOT =        875
017734                 TA   =          318
00445
                                          MA   =          318
04359
                                          Ha   =            220
605  n
mi
                                          Hp   =            213
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1802207
82                 X    =         -527310
54
 Y    =      -13925608
05  feet           Y    =        -4250545
52  meter
 Z    =       17223786
22                 Z    =         5247194
66
 XDOT =      25006
601520                 XDOT =        7616
076627
 YDOT =        328
163427  feet/sec       YDOT =         185
225364  meter/sec
 ZDOT =       2870
793090                 ZDOT =         912
029809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -82131
83                 X    =          -25033
78
 Y    =      -14054569
58  feet           Y    =        -4283832
81  meter
 Z    =       17213124
43                 Z    =         5246560
33
 XDOT =      23706
804472                 XDOT =        7225
834003
 YDOT =       3588
139325  feet/sec       YDOT =        1093
664866  meter/sec
 ZDOT =       3031
744510                 ZDOT =         924
075727


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   16143
36369612  
00016717  00000-0  10270-3 0  9097
2 25544  51
6415 186
8604 0001652 127
4515 232
6788 15
54715146 40960


Satellite: ISS
Catalog Number: 25544
Epoch time:      16143
36369612   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       186
8604  deg
Eccentricity:     
0001652     
Arg of perigee:   127
4515  deg
Mean anomaly:     232
6788  deg
Mean motion:   15
54715146  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4096
Checksum:              321


Coasting Arc #11 (Orbit 4110)
---------------------------------------

Vector Time (GMT): 2016/144/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1505432
22                 A    =         6776164
09  meter
 Y    =        4094336
55  meter          E    =           
0015628
 Z    =       -5199047
95                 I    =           51
61024
 XDOT =      -7466
270867                 Wp   =          102
86147
 YDOT =      -1132
508565  meter/sec      RA   =          180
96866  deg
 ZDOT =       1269
881807                 TA   =          179
35400
                                          MA   =          179
35198
                                          Ha   =            220
610  n
mi
                                          Hp   =            213
192

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4939082
10                 X    =        -1525849
11
 Y    =       13432862
68  feet           Y    =         4077388
13  meter
 Z    =      -17057243
92                 Z    =        -5206410
28
 XDOT =     -24495
639329                 XDOT =       -7459
220594
 YDOT =      -3715
579282  feet/sec       YDOT =       -1215
962072  meter/sec
 ZDOT =       4166
278894                 ZDOT =        1233
628994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6319159
97                 X    =        -1926079
96
 Y    =       12797948
53  feet           Y    =         3900814
71  meter
 Z    =      -17089957
07                 Z    =        -5209018
91
 XDOT =     -23010
207931                 XDOT =       -7013
511377
 YDOT =      -6007
636912  feet/sec       YDOT =       -1831
127731  meter/sec
 ZDOT =       4008
780394                 ZDOT =        1221
876264


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   16144
32788345  
00016717  00000-0  10270-3 0  9104
2 25544  51
6411 182
0514 0001715 128
2256 231
9051 15
54708638 41116


Satellite: ISS
Catalog Number: 25544
Epoch time:      16144
32788345   =   yrday
fracday
Element set:     910
Inclination:       51
6411  deg
RA of node:       182
0514  deg
Eccentricity:     
0001715     
Arg of perigee:   128
2256  deg
Mean anomaly:     231
9051  deg
Mean motion:   15
54708638  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4111
Checksum:              284


Coasting Arc #12 (Orbit 4126)
---------------------------------------

Vector Time (GMT): 2016/145/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3421590
13                 A    =         6779138
59  meter
 Y    =       -3779275
76  meter          E    =           
0009937
 Z    =        4461202
51                 I    =           51
65255
 XDOT =       6611
872626                 Wp   =           77
52028
 YDOT =       2122
774359  meter/sec      RA   =          175
96661  deg
 ZDOT =      -3264
552703                 TA   =           45
37226
                                          MA   =           45
29126
                                          Ha   =            220
543  n
mi
                                          Hp   =            213
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11225689
39                 X    =         3441925
77
 Y    =      -12399198
70  feet           Y    =        -3740900
01  meter
 Z    =       14636491
17                 Z    =         4477872
96
 XDOT =      21692
495493                 XDOT =        6603
501803
 YDOT =       6964
482806  feet/sec       YDOT =        2196
666241  meter/sec
 ZDOT =     -10710
474749                 ZDOT =       -3232
453607

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12271591
58                 X    =         3740381
11
 Y    =      -11270195
40  feet           Y    =        -3435155
56  meter
 Z    =       14709651
26                 Z    =         4483501
70
 XDOT =      20168
890141                 XDOT =        6147
477715
 YDOT =       8128
556812  feet/sec       YDOT =        2477
584116  meter/sec
 ZDOT =     -10571
189958                 ZDOT =       -3222
098699


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   16145
35634290  
00016717  00000-0  10270-3 0  9118
2 25544  51
6414 176
9197 0001709 130
1307 229
9996 15
54695178 41276


Satellite: ISS
Catalog Number: 25544
Epoch time:      16145
35634290   =   yrday
fracday
Element set:     911
Inclination:       51
6414  deg
RA of node:       176
9197  deg
Eccentricity:     
0001709     
Arg of perigee:   130
1307  deg
Mean anomaly:     229
9996  deg
Mean motion:   15
54695178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4127
Checksum:              328


Coasting Arc #13 (Orbit 4141)
---------------------------------------

Vector Time (GMT): 2016/146/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4987667
86                 A    =         6783317
51  meter
 Y    =        3330425
96  meter          E    =           
0005606
 Z    =       -3174517
43                 I    =           51
69864
 XDOT =      -5107
062850                 Wp   =           92
80517
 YDOT =      -3051
485072  meter/sec      RA   =          170
97923  deg
 ZDOT =       4829
748589                 TA   =          230
60136
                                          MA   =          230
65102
                                          Ha   =            220
520  n
mi
                                          Hp   =            213
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16363739
69                 X    =        -5009118
25
 Y    =       10926594
34  feet           Y    =         3274530
92  meter
 Z    =      -10415083
43                 Z    =        -3198798
25
 XDOT =     -16755
455543                 XDOT =       -5096
021852
 YDOT =     -10011
433963  feet/sec       YDOT =       -3108
534399  meter/sec
 ZDOT =      15845
631854                 ZDOT =        4804
966045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17108579
81                 X    =        -5214695
12
 Y    =        9603920
92  feet           Y    =         2927275
10  meter
 Z    =      -10521292
86                 Z    =        -3206890
06
 XDOT =     -15313
284128                 XDOT =       -4667
489002
 YDOT =     -10062
935390  feet/sec       YDOT =       -3067
182707  meter/sec
 ZDOT =      15738
317781                 ZDOT =        4797
039260


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   16146
32051603  
00016717  00000-0  10270-3 0  9128
2 25544  51
6415 172
1098 0001501 132
8395 227
2884 15
54695794 41429


Satellite: ISS
Catalog Number: 25544
Epoch time:      16146
32051603   =   yrday
fracday
Element set:     912
Inclination:       51
6415  deg
RA of node:       172
1098  deg
Eccentricity:     
0001501     
Arg of perigee:   132
8395  deg
Mean anomaly:     227
2884  deg
Mean motion:   15
54695794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4142
Checksum:              301


Coasting Arc #14 (Orbit 4157)
---------------------------------------

Vector Time (GMT): 2016/147/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6055684
35                 A    =         6786721
09  meter
 Y    =       -2683016
64  meter          E    =           
0015491
 Z    =        1444369
24                 I    =           51
74088
 XDOT =       3133
076038                 Wp   =          120
71622
 YDOT =       3930
248353  meter/sec      RA   =          166
00619  deg
 ZDOT =      -5796
688841                 TA   =           43
53967
                                          MA   =           43
41749
                                          Ha   =            220
542  n
mi
                                          Hp   =            213
290

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19867730
80                 X    =         6078220
28
 Y    =       -8802548
02  feet           Y    =        -2615172
08  meter
 Z    =        4738744
22                 Z    =         1473840
89
 XDOT =      10279
120861                 XDOT =        3117
052136
 YDOT =      12894
515593  feet/sec       YDOT =        3965
195449  meter/sec
 ZDOT =     -19018
008010                 ZDOT =       -5781
507600

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20343212
74                 X    =         6200611
24
 Y    =       -7558366
68  feet           Y    =        -2303790
16  meter
 Z    =        4867449
44                 Z    =         1483598
59
 XDOT =       9032
939461                 XDOT =        2753
239948
 YDOT =      12027
916736  feet/sec       YDOT =        3666
109021  meter/sec
 ZDOT =     -18952
608994                 ZDOT =       -5776
755222


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   16147
34896357  
00016717  00000-0  10270-3 0  9135
2 25544  51
6408 166
9790 0001676 135
9456 224
1831 15
54705983 41583


Satellite: ISS
Catalog Number: 25544
Epoch time:      16147
34896357   =   yrday
fracday
Element set:     913
Inclination:       51
6408  deg
RA of node:       166
9790  deg
Eccentricity:     
0001676     
Arg of perigee:   135
9456  deg
Mean anomaly:     224
1831  deg
Mean motion:   15
54705983  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4158
Checksum:              342


Coasting Arc #15 (Orbit 4173)
---------------------------------------

Vector Time (GMT): 2016/148/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6504816
22                 A    =         6787583
87  meter
 Y    =        1868545
81  meter          E    =           
0012959
 Z    =         439481
06                 I    =           51
77529
 XDOT =       -930
693647                 Wp   =           56
44229
 YDOT =      -4680
366191  meter/sec      RA   =          161
04130  deg
 ZDOT =       6003
953334                 TA   =          308
28916
                                          MA   =          308
40565
                                          Ha   =            220
497  n
mi
                                          Hp   =            213
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21341260
56                 X    =        -6527362
13
 Y    =        6130399
65  feet           Y    =         1795678
53  meter
 Z    =        1441867
00                 Z    =          407827
57
 XDOT =      -3053
456846                 XDOT =        -907
452174
 YDOT =     -15355
532122  feet/sec       YDOT =       -4690
644382  meter/sec
 ZDOT =      19698
009626                 ZDOT =        5999
488296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21602649
14                 X    =        -6584487
46
 Y    =        5170674
70  feet           Y    =         1576021
65  meter
 Z    =        1303785
22                 Z    =          397393
73
 XDOT =      -2114
196953                 XDOT =        -644
407231
 YDOT =     -13905
138157  feet/sec       YDOT =       -4238
286110  meter/sec
 ZDOT =      19679
369200                 ZDOT =        5998
271732


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   16148
37740455  
00016717  00000-0  10270-3 0  9147
2 25544  51
6415 161
8477 0001501 137
1316 222
9954 15
54706665 41741


Satellite: ISS
Catalog Number: 25544
Epoch time:      16148
37740455   =   yrday
fracday
Element set:     914
Inclination:       51
6415  deg
RA of node:       161
8477  deg
Eccentricity:     
0001501     
Arg of perigee:   137
1316  deg
Mean anomaly:     222
9954  deg
Mean motion:   15
54706665  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4174
Checksum:              312


Coasting Arc #16 (Orbit 4188)
---------------------------------------

Vector Time (GMT): 2016/149/07:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6325693
88                 A    =         6785394
32  meter
 Y    =        -818096
81  meter          E    =           
0007470
 Z    =       -2309217
65                 I    =           51
79791
 XDOT =      -1297
932736                 Wp   =          137
30894
 YDOT =       5252
307778  meter/sec      RA   =          156
07697  deg
 ZDOT =      -5431
848416                 TA   =           68
36124
                                          MA   =           68
28170
                                          Ha   =            220
507  n
mi
                                          Hp   =            213
403

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20753588
83                 X    =         6345589
12
 Y    =       -2684044
65  feet           Y    =         -747247
29  meter
 Z    =       -7576173
39                 Z    =        -2278440
64
 XDOT =      -4258
309500                 XDOT =       -1330
183226
 YDOT =      17231
980898  feet/sec       YDOT =        5237
613493  meter/sec
 ZDOT =     -17821
024987                 ZDOT =       -5438
231429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20867886
20                 X    =         6360531
71
 Y    =       -2112087
47  feet           Y    =         -643764
26  meter
 Z    =       -7442066
96                 Z    =        -2268342
01
 XDOT =      -4769
356561                 XDOT =       -1453
699880
 YDOT =      15588
232114  feet/sec       YDOT =        4751
293148  meter/sec
 ZDOT =     -17849
700225                 ZDOT =       -5440
588629


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   16149
34156125  
00016717  00000-0  10270-3 0  9151
2 25544  51
6412 157
0375 0001532 140
0094 220
1172 15
54730047 41891


Satellite: ISS
Catalog Number: 25544
Epoch time:      16149
34156125   =   yrday
fracday
Element set:     915
Inclination:       51
6412  deg
RA of node:       157
0375  deg
Eccentricity:     
0001532     
Arg of perigee:   140
0094  deg
Mean anomaly:     220
1172  deg
Mean motion:   15
54730047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4189
Checksum:              276
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