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

 
Date: July 19th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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


201/08:38:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 213 0

202/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 213 0

Coasting Arc #1 (Orbit 994)
---------------------------------------

Vector Time (GMT): 2016/201/03:19:58
807
Vector Time (MET): N/A
Weight (LBS)     : 894430
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4362517
68                 A    =         6777552
38  meter
 Y    =       -2095196
07  meter          E    =           
0012349
 Z    =       -4756466
39                 I    =           51
26421
 XDOT =        588
464360                 Wp   =          102
06910
 YDOT =      -7172
502232  meter/sec      RA   =          257
69021  deg
 ZDOT =       2622
978520                 TA   =          193
95401
                                          MA   =          193
98816
                                          Ha   =            220
383  n
mi
                                          Hp   =            212
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14312722
05                 X    =        -4315659
96
 Y    =       -6874002
86  feet           Y    =        -2143718
16  meter
 Z    =      -15605204
69                 Z    =        -4777544
48
 XDOT =       1930
657348                 XDOT =         655
884261
 YDOT =     -23531
831471  feet/sec       YDOT =       -7165
544940  meter/sec
 ZDOT =       8605
572572                 ZDOT =        2626
000083

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12213878
39                 X    =        -3722790
13
 Y    =      -10003209
78  feet           Y    =        -3048978
34  meter
 Z    =      -15696665
57                 Z    =        -4784343
67
 XDOT =       6587
125121                 XDOT =        2007
755737
 YDOT =     -21552
451652  feet/sec       YDOT =       -6569
187263  meter/sec
 ZDOT =       8620
057283                 ZDOT =        2627
393460


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   16201
15032813  
00016717  00000-0  10270-3 0  9000
2 25544  51
6393 258
5643 0001704  53
3338 306
7972 15
54845570  9950


Satellite: ISS
Catalog Number: 25544
Epoch time:      16201
15032813   =   yrday
fracday
Element set:     900
Inclination:       51
6393  deg
RA of node:       258
5643  deg
Eccentricity:     
0001704     
Arg of perigee:    53
3338  deg
Mean anomaly:     306
7972  deg
Mean motion:   15
54845570  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             995
Checksum:              304


Coasting Arc #2 (Orbit 998)
---------------------------------------

Vector Time (GMT): 2016/201/08:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4201386
91                 A    =         6775194
64  meter
 Y    =        -625315
03  meter          E    =           
0004038
 Z    =        5275070
47                 I    =           51
26172
 XDOT =       1524
449438                 Wp   =           70
50413
 YDOT =       7513
228665  meter/sec      RA   =          256
59923  deg
 ZDOT =       -322
007018                 TA   =           22
58884
                                          MA   =           22
57107
                                          Ha   =            220
174  n
mi
                                          Hp   =            212
994

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13784077
79                 X    =         4182443
51
 Y    =       -2051558
50  feet           Y    =         -578438
78  meter
 Z    =       17306661
63                 Z    =         5295433
33
 XDOT =       5001
474534                 XDOT =        1441
885467
 YDOT =      24649
700344  feet/sec       YDOT =        7529
814466  meter/sec
 ZDOT =      -1056
453472                 ZDOT =        -314
801513

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3636477
74                 X    =         1108398
42
 Y    =      -13338012
61  feet           Y    =        -4065426
24  meter
 Z    =       17395507
44                 Z    =         5302150
67
 XDOT =      23603
891736                 XDOT =        7194
466201
 YDOT =       5090
187166  feet/sec       YDOT =        1551
489048  meter/sec
 ZDOT =      -1026
432689                 ZDOT =        -312
856684


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   16201
40741780  
00016717  00000-0  10270-3 0  9019
2 25544  51
6429 257
2805 0001521  61
6693 298
4613 15
54877878  9998


Satellite: ISS
Catalog Number: 25544
Epoch time:      16201
40741780   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:       257
2805  deg
Eccentricity:     
0001521     
Arg of perigee:    61
6693  deg
Mean anomaly:     298
4613  deg
Mean motion:   15
54877878  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             999
Checksum:              331


Coasting Arc #3 (Orbit 1013)
---------------------------------------

Vector Time (GMT): 2016/202/08:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909574
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4553009
67                 A    =         6777178
81  meter
 Y    =       -1419112
66  meter          E    =           
0013032
 Z    =       -4827416
06                 I    =           51
27599
 XDOT =       -340
664906                 Wp   =          103
21053
 YDOT =      -7247
363958  meter/sec      RA   =          251
56938  deg
 ZDOT =       2454
490983                 TA   =          191
02751
                                          MA   =          191
05611
                                          Ha   =            220
369  n
mi
                                          Hp   =            212
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14937695
77                 X    =        -4513353
36
 Y    =       -4655881
42  feet           Y    =        -1469805
29  meter
 Z    =      -15837979
20                 Z    =        -4849436
82
 XDOT =      -1117
667015                 XDOT =        -271
520361
 YDOT =     -23777
440806  feet/sec       YDOT =       -7250
787105  meter/sec
 ZDOT =       8052
791938                 ZDOT =        2453
003455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10040641
34                 X    =        -3060387
48
 Y    =       11872520
28  feet           Y    =         3618744
18  meter
 Z    =      -15933686
18                 Z    =        -4856587
55
 XDOT =     -21507
482149                 XDOT =       -6555
480559
 YDOT =      -7400
307713  feet/sec       YDOT =       -2255
613791  meter/sec
 ZDOT =       8047
619748                 ZDOT =        2452
914499


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   16202
37150387  
00016717  00000-0  10270-3 0  9024
2 25544  51
6422 252
4712 0001604  67
9368 292
1955 15
54873168 10142


Satellite: ISS
Catalog Number: 25544
Epoch time:      16202
37150387   =   yrday
fracday
Element set:     902
Inclination:       51
6422  deg
RA of node:       252
4712  deg
Eccentricity:     
0001604     
Arg of perigee:    67
9368  deg
Mean anomaly:     292
1955  deg
Mean motion:   15
54873168  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1014
Checksum:              300


Coasting Arc #4 (Orbit 1015)
---------------------------------------

Vector Time (GMT): 2016/202/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4527102
34                 A    =         6779398
01  meter
 Y    =        2729270
23  meter          E    =           
0011438
 Z    =        4237578
43                 I    =           51
28399
 XDOT =       -713
688983                 Wp   =           71
20093
 YDOT =       6751
712072  meter/sec      RA   =          251
07054  deg
 ZDOT =      -3574
523739                 TA   =           55
51348
                                          MA   =           55
40549
                                          Ha   =            220
203  n
mi
                                          Hp   =            212
973

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14852697
98                 X    =         4475662
57
 Y    =        8954298
66  feet           Y    =         2779607
33  meter
 Z    =       13902816
37                 Z    =         4259444
82
 XDOT =      -2341
499287                 XDOT =        -771
772136
 YDOT =      22151
286324  feet/sec       YDOT =        6743
406670  meter/sec
 ZDOT =     -11727
440089                 ZDOT =       -3578
131087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5460951
63                 X    =         1664498
06
 Y    =      -16380329
02  feet           Y    =        -4992724
29  meter
 Z    =       13997615
27                 Z    =         4266473
13
 XDOT =      20906
997639                 XDOT =        6372
452880
 YDOT =      -3098
131183  feet/sec       YDOT =        -944
310384  meter/sec
 ZDOT =     -11744
379468                 ZDOT =       -3579
686862


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   16202
50004680  
00016717  00000-0  10270-3 0  9034
2 25544  51
6417 251
8308 0001562  57
3349 302
7955 15
54884451 10162


Satellite: ISS
Catalog Number: 25544
Epoch time:      16202
50004680   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:       251
8308  deg
Eccentricity:     
0001562     
Arg of perigee:    57
3349  deg
Mean anomaly:     302
7955  deg
Mean motion:   15
54884451  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1016
Checksum:              290


Coasting Arc #5 (Orbit 1030)
---------------------------------------

Vector Time (GMT): 2016/203/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4396206
17                 A    =         6783729
90  meter
 Y    =       -4326713
63  meter          E    =           
0006271
 Z    =       -2824423
87                 I    =           51
30856
 XDOT =       2048
226940                 Wp   =           63
22730
 YDOT =      -5378
376073  meter/sec      RA   =          246
05786  deg
 ZDOT =       5062
528848                 TA   =          264
53753
                                          MA   =          264
60907
                                          Ha   =            220
354  n
mi
                                          Hp   =            212
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14423248
59                 X    =        -4333777
49
 Y    =      -14195254
71  feet           Y    =        -4375525
70  meter
 Z    =       -9266482
53                 Z    =        -2845627
76
 XDOT =       6719
904658                 XDOT =        2083
626004
 YDOT =     -17645
590790  feet/sec       YDOT =       -5355
273847  meter/sec
 ZDOT =      16609
346615                 ZDOT =        5072
564028

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10363064
26                 X    =        -3158661
99
 Y    =       17333074
04  feet           Y    =         5283120
97  meter
 Z    =       -9358124
71                 Z    =        -2852356
41
 XDOT =     -17447
731472                 XDOT =       -5318
068553
 YDOT =      -1460
260584  feet/sec       YDOT =        -445
087426  meter/sec
 ZDOT =      16654
039390                 ZDOT =        5076
151206


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   16203
46412868  
00016717  00000-0  10270-3 0  9042
2 25544  51
6406 247
0201 0001621  64
9371 295
1950 15
54866194 10315


Satellite: ISS
Catalog Number: 25544
Epoch time:      16203
46412868   =   yrday
fracday
Element set:     904
Inclination:       51
6406  deg
RA of node:       247
0201  deg
Eccentricity:     
0001621     
Arg of perigee:    64
9371  deg
Mean anomaly:     295
1950  deg
Mean motion:   15
54866194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1031
Checksum:              291


Coasting Arc #6 (Orbit 1046)
---------------------------------------

Vector Time (GMT): 2016/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3915959
97                 A    =         6786679
40  meter
 Y    =        5446374
29  meter          E    =           
0014545
 Z    =         988757
30                 I    =           51
33311
 XDOT =      -3421
908439                 Wp   =          117
81964
 YDOT =       3539
154977  meter/sec      RA   =          241
05750  deg
 ZDOT =      -5882
560623                 TA   =           51
41640
                                          MA   =           51
28620
                                          Ha   =            220
408  n
mi
                                          Hp   =            212
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12847637
71                 X    =         3849963
35
 Y    =       17868682
05  feet           Y    =         5489796
11  meter
 Z    =        3243954
39                 Z    =         1007619
63
 XDOT =     -11226
733725                 XDOT =       -3432
655485
 YDOT =      11611
400843  feet/sec       YDOT =        3500
829109  meter/sec
 ZDOT =     -19299
739578                 ZDOT =       -5899
208987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14006704
78                 X    =         4269243
62
 Y    =      -16959658
49  feet           Y    =        -5169303
91  meter
 Z    =        3325212
49                 Z    =         1013524
77
 XDOT =      12820
433876                 XDOT =        3907
668245
 YDOT =       6752
317462  feet/sec       YDOT =        2058
106362  meter/sec
 ZDOT =     -19372
923447                 ZDOT =       -5904
867067


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   16204
49247571  
00016717  00000-0  10270-3 0  9054
2 25544  51
6412 241
8877 0001851  62
6255 297
5087 15
54891246 10474


Satellite: ISS
Catalog Number: 25544
Epoch time:      16204
49247571   =   yrday
fracday
Element set:     905
Inclination:       51
6412  deg
RA of node:       241
8877  deg
Eccentricity:     
0001851     
Arg of perigee:    62
6255  deg
Mean anomaly:     297
5087  deg
Mean motion:   15
54891246  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1047
Checksum:              322


Coasting Arc #7 (Orbit 1062)
---------------------------------------

Vector Time (GMT): 2016/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3097624
96                 A    =         6786929
04  meter
 Y    =       -5956248
72  meter          E    =           
0015446
 Z    =         944318
32                 I    =           51
34880
 XDOT =       4679
456850                 Wp   =           56
50650
 YDOT =      -1489
413388  meter/sec      RA   =          236
06376  deg
 ZDOT =       5894
127810                 TA   =          313
76732
                                          MA   =          313
89503
                                          Ha   =            220
560  n
mi
                                          Hp   =            212
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10162811
54                 X    =        -3035377
47
 Y    =      -19541498
43  feet           Y    =        -5990540
41  meter
 Z    =        3098157
23                 Z    =          929422
11
 XDOT =      15352
548720                 XDOT =        4667
133456
 YDOT =      -4886
526865  feet/sec       YDOT =       -1437
153669  meter/sec
 ZDOT =      19337
689665                 ZDOT =        5916
829043

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16040421
15                 X    =        -4889120
37
 Y    =       15107933
48  feet           Y    =         4604898
12  meter
 Z    =        3034256
54                 Z    =          924841
39
 XDOT =      -7735
742707                 XDOT =       -2357
854377
 YDOT =     -12158
175699  feet/sec       YDOT =       -3705
811953  meter/sec
 ZDOT =      19436
899491                 ZDOT =        5924
366965


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   16205
52082096  
00016717  00000-0  10270-3 0  9069
2 25544  51
6403 236
7561 0001986  65
1529 294
9830 15
54831148 10638


Satellite: ISS
Catalog Number: 25544
Epoch time:      16205
52082096   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       236
7561  deg
Eccentricity:     
0001986     
Arg of perigee:    65
1529  deg
Mean anomaly:     294
9830  deg
Mean motion:   15
54831148  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1063
Checksum:              311


Coasting Arc #8 (Orbit 1077)
---------------------------------------

Vector Time (GMT): 2016/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1888985
20                 A    =         6783842
77  meter
 Y    =        5888718
48  meter          E    =           
0006206
 Z    =       -2790890
24                 I    =           51
35866
 XDOT =      -5699
880862                 Wp   =          107
74743
 YDOT =       -578
980738  meter/sec      RA   =          231
06594  deg
 ZDOT =      -5090
761827                 TA   =          104
03111
                                          MA   =          103
96211
                                          Ha   =            220
493  n
mi
                                          Hp   =            212
803

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6197458
01                 X    =         1836552
41
 Y    =       19319942
51  feet           Y    =         5909549
26  meter
 Z    =       -9156464
05                 Z    =        -2781841
39
 XDOT =     -18700
396529                 XDOT =       -5668
254571
 YDOT =      -1899
543105  feet/sec       YDOT =        -642
543677  meter/sec
 ZDOT =     -16701
974499                 ZDOT =       -5118
373204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16696815
69                 X    =         5089189
42
 Y    =      -11558004
34  feet           Y    =        -3522879
72  meter
 Z    =       -9118024
98                 Z    =        -2779174
01
 XDOT =       2694
148155                 XDOT =         821
176358
 YDOT =      17133
774943  feet/sec       YDOT =        5222
374603  meter/sec
 ZDOT =     -16822
238758                 ZDOT =       -5127
418373


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   16206
48488746  
00016717  00000-0  10270-3 0  9078
2 25544  51
6411 231
9446 0001927  72
8193 287
3171 15
54887887 10784


Satellite: ISS
Catalog Number: 25544
Epoch time:      16206
48488746   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       231
9446  deg
Eccentricity:     
0001927     
Arg of perigee:    72
8193  deg
Mean anomaly:     287
3171  deg
Mean motion:   15
54887887  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1078
Checksum:              346


Coasting Arc #9 (Orbit 1093)
---------------------------------------

Vector Time (GMT): 2016/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -403021
55                 A    =         6779547
21  meter
 Y    =       -5281771
15  meter          E    =           
0011875
 Z    =        4222529
09                 I    =           51
36515
 XDOT =       6328
927515                 Wp   =          101
01578
 YDOT =       2410
628033  meter/sec      RA   =          226
05769  deg
 ZDOT =       3608
544237                 TA   =          311
92109
                                          MA   =          312
02229
                                          Ha   =            220
516  n
mi
                                          Hp   =            212
754

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1322249
18                 X    =         -364440
50
 Y    =      -17328645
51  feet           Y    =        -5286062
36  meter
 Z    =       13853441
89                 Z    =         4220664
95
 XDOT =      20764
197883                 XDOT =        6283
972327
 YDOT =       7908
884622  feet/sec       YDOT =        2481
150903  meter/sec
 ZDOT =      11839
055895                 ZDOT =        3639
179096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16074079
39                 X    =        -4899379
40
 Y    =        6622281
22  feet           Y    =         2018471
32  meter
 Z    =       13846209
36                 Z    =         4220324
61
 XDOT =       1716
015318                 XDOT =         523
041469
 YDOT =     -20941
463213  feet/sec       YDOT =       -6382
957987  meter/sec
 ZDOT =      11972
200624                 ZDOT =        3649
126750


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   16207
51322106  
00016717  00000-0  10270-3 0  9081
2 25544  51
6410 226
8125 0002023  74
4879 285
6498 15
54889786 10948


Satellite: ISS
Catalog Number: 25544
Epoch time:      16207
51322106   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:       226
8125  deg
Eccentricity:     
0002023     
Arg of perigee:    74
4879  deg
Mean anomaly:     285
6498  deg
Mean motion:   15
54889786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1094
Checksum:              323


Coasting Arc #10 (Orbit 1108)
---------------------------------------

Vector Time (GMT): 2016/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1300574
47                 A    =         6776065
52  meter
 Y    =        4276630
35  meter          E    =           
0015388
 Z    =       -5106384
84                 I    =           51
37759
 XDOT =      -6407
917224                 Wp   =           77
80414
 YDOT =      -3871
331230  meter/sec      RA   =          221
03838  deg
 ZDOT =      -1611
131606                 TA   =          176
57936
                                          MA   =          176
56883
                                          Ha   =            220
503  n
mi
                                          Hp   =            212
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4266976
62                 X    =        -1323495
75
 Y    =       14030939
48  feet           Y    =         4261958
43  meter
 Z    =      -16753231
09                 Z    =        -5112758
21
 XDOT =     -21023
350473                 XDOT =       -6356
324651
 YDOT =     -12701
217945  feet/sec       YDOT =       -3942
700326  meter/sec
 ZDOT =      -5285
864849                 ZDOT =       -1642
134210

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14621924
92                 X    =         4456762
72
 Y    =        -563666
39  feet           Y    =         -171805
51  meter
 Z    =      -16781736
98                 Z    =        -5115073
43
 XDOT =      -5335
168893                 XDOT =       -1626
159478
 YDOT =      22888
603746  feet/sec       YDOT =        6976
446422  meter/sec
 ZDOT =      -5420
381438                 ZDOT =       -1652
132262


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   16208
47728024  
00016717  00000-0  10270-3 0  9097
2 25544  51
6421 222
0018 0001925  77
0283 283
1085 15
54882941 11095


Satellite: ISS
Catalog Number: 25544
Epoch time:      16208
47728024   =   yrday
fracday
Element set:     909
Inclination:       51
6421  deg
RA of node:       222
0018  deg
Eccentricity:     
0001925     
Arg of perigee:    77
0283  deg
Mean anomaly:     283
1085  deg
Mean motion:   15
54882941  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1109
Checksum:              296


Coasting Arc #11 (Orbit 1124)
---------------------------------------

Vector Time (GMT): 2016/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3019949
69                 A    =         6775190
76  meter
 Y    =       -3002059
75  meter          E    =           
0004873
 Z    =        5265886
27                 I    =           51
39829
 XDOT =       5894
891292                 Wp   =           72
79323
 YDOT =       4876
140582  meter/sec      RA   =          216
01347  deg
 ZDOT =       -598
938003                 TA   =           22
94951
                                          MA   =           22
92775
                                          Ha   =            220
421  n
mi
                                          Hp   =            212
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9907971
41                 X    =         3027715
78
 Y    =       -9849277
38  feet           Y    =        -2968245
45  meter
 Z    =       17276529
76                 Z    =         5280575
08
 XDOT =      19340
194526                 XDOT =        5842
836301
 YDOT =      15997
836556  feet/sec       YDOT =        4941
770161  meter/sec
 ZDOT =      -1965
019696                 ZDOT =        -570
428508

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12573994
01                 X    =        -3832553
37
 Y    =       -5902227
43  feet           Y    =        -1798998
92  meter
 Z    =       17341079
24                 Z    =         5285560
95
 XDOT =       8105
485547                 XDOT =        2470
551995
 YDOT =     -22696
278833  feet/sec       YDOT =       -6917
825788  meter/sec
 ZDOT =      -1841
524903                 ZDOT =        -561
296791


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   16209
50560597  
00016717  00000-0  10270-3 0  9103
2 25544  51
6405 216
8700 0002067  80
2332 279
9054 15
54904102 11256


Satellite: ISS
Catalog Number: 25544
Epoch time:      16209
50560597   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:       216
8700  deg
Eccentricity:     
0002067     
Arg of perigee:    80
2332  deg
Mean anomaly:     279
9054  deg
Mean motion:   15
54904102  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1125
Checksum:              283


Coasting Arc #12 (Orbit 1139)
---------------------------------------

Vector Time (GMT): 2016/210/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4586784
51                 A    =         6777550
15  meter
 Y    =        1639343
01  meter          E    =           
0012798
 Z    =       -4724845
25                 I    =           51
43412
 XDOT =      -4726
522885                 Wp   =          104
92559
 YDOT =      -5375
081568  meter/sec      RA   =          210
99314  deg
 ZDOT =       2726
427301                 TA   =          192
14053
                                          MA   =          192
17141
                                          Ha   =            220
481  n
mi
                                          Hp   =            212
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15048505
60                 X    =        -4581824
06
 Y    =        5378421
96  feet           Y    =         1588078
54  meter
 Z    =      -15501460
78                 Z    =        -4747114
40
 XDOT =     -15506
964846                 XDOT =       -4679
309797
 YDOT =     -17634
782046  feet/sec       YDOT =       -5427
672879  meter/sec
 ZDOT =       8944
971459                 ZDOT =        2703
581552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10311522
85                 X    =         3142952
16
 Y    =       12084235
71  feet           Y    =         3683275
04  meter
 Z    =      -15598845
27                 Z    =        -4754528
04
 XDOT =     -10116
378420                 XDOT =       -3083
472142
 YDOT =      20038
968806  feet/sec       YDOT =        6107
877692  meter/sec
 ZDOT =       8846
240131                 ZDOT =        2696
333992


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   16210
46965626  
00016717  00000-0  10270-3 0  9113
2 25544  51
6419 212
0593 0001911  78
8160 281
3208 15
54888156 11403


Satellite: ISS
Catalog Number: 25544
Epoch time:      16210
46965626   =   yrday
fracday
Element set:     911
Inclination:       51
6419  deg
RA of node:       212
0593  deg
Eccentricity:     
0001911     
Arg of perigee:    78
8160  deg
Mean anomaly:     281
3208  deg
Mean motion:   15
54888156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1140
Checksum:              300


Coasting Arc #13 (Orbit 1155)
---------------------------------------

Vector Time (GMT): 2016/211/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5793016
72                 A    =         6781649
15  meter
 Y    =        -279222
28  meter          E    =           
0014191
 Z    =        3503238
35                 I    =           51
47461
 XDOT =       2994
275322                 Wp   =           86
98993
 YDOT =       5445
818098  meter/sec      RA   =          205
98515  deg
 ZDOT =      -4500
832654                 TA   =           51
64262
                                          MA   =           51
51519
                                          Ha   =            220
378  n
mi
                                          Hp   =            212
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19005960
37                 X    =         5778691
45
 Y    =        -916083
58  feet           Y    =         -214521
24  meter
 Z    =       11493564
14                 Z    =         3531344
29
 XDOT =       9823
737934                 XDOT =        2955
019160
 YDOT =      17866
857276  feet/sec       YDOT =        5479
082911  meter/sec
 ZDOT =     -14766
511331                 ZDOT =       -4486
382313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7842621
22                 X    =        -2390430
95
 Y    =      -17254713
48  feet           Y    =        -5259236
67  meter
 Z    =       11616191
75                 Z    =         3540615
25
 XDOT =      11680
418139                 XDOT =        3560
191449
 YDOT =     -15244
316121  feet/sec       YDOT =       -4646
467554  meter/sec
 ZDOT =     -14704
390318                 ZDOT =       -4481
898169


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   16211
49797148  
00016717  00000-0  10270-3 0  9120
2 25544  51
6400 206
9272 0002072  80
4650 279
6738 15
54939454 11564


Satellite: ISS
Catalog Number: 25544
Epoch time:      16211
49797148   =   yrday
fracday
Element set:     912
Inclination:       51
6400  deg
RA of node:       206
9272  deg
Eccentricity:     
0002072     
Arg of perigee:    80
4650  deg
Mean anomaly:     279
6738  deg
Mean motion:   15
54939454  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1156
Checksum:              318


Coasting Arc #14 (Orbit 1170)
---------------------------------------

Vector Time (GMT): 2016/212/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6466536
18                 A    =         6785450
82  meter
 Y    =        -923952
77  meter          E    =           
0008629
 Z    =       -1829084
99                 I    =           51
51622
 XDOT =       -855
023410                 Wp   =           50
02155
 YDOT =      -5126
906909  meter/sec      RA   =          200
99334  deg
 ZDOT =       5635
749004                 TA   =          289
82953
                                          MA   =          289
92253
                                          Ha   =            220
426  n
mi
                                          Hp   =            212
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21215669
90                 X    =        -6446838
92
 Y    =       -3031341
11  feet           Y    =         -996155
62  meter
 Z    =       -6000934
99                 Z    =        -1860449
60
 XDOT =      -2805
194916                 XDOT =        -825
005158
 YDOT =     -16820
560725  feet/sec       YDOT =       -5136
300934  meter/sec
 ZDOT =      18489
990171                 ZDOT =        5631
668095

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5361066
78                 X    =         1634053
15
 Y    =       20709750
63  feet           Y    =         6312331
99  meter
 Z    =       -6137596
50                 Z    =        -1870739
41
 XDOT =     -12883
447414                 XDOT =       -3926
874772
 YDOT =       8787
878579  feet/sec       YDOT =        2678
545391  meter/sec
 ZDOT =      18473
034917                 ZDOT =        5630
581043


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   16212
46201421  
00016717  00000-0  10270-3 0  9133
2 25544  51
6395 202
1166 0002077  88
8872 271
2519 15
54950335 11713


Satellite: ISS
Catalog Number: 25544
Epoch time:      16212
46201421   =   yrday
fracday
Element set:     913
Inclination:       51
6395  deg
RA of node:       202
1166  deg
Eccentricity:     
0002077     
Arg of perigee:    88
8872  deg
Mean anomaly:     271
2519  deg
Mean motion:   15
54950335  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1171
Checksum:              290


Coasting Arc #15 (Orbit 1186)
---------------------------------------

Vector Time (GMT): 2016/213/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6484930
83                 A    =         6786997
54  meter
 Y    =        1978263
41  meter          E    =           
0013368
 Z    =        -142123
11                 I    =           51
55077
 XDOT =      -1504
515995                 Wp   =          129
17180
 YDOT =       4528
361089  meter/sec      RA   =          196
01095  deg
 ZDOT =      -6004
708143                 TA   =           52
36164
                                          MA   =           52
24041
                                          Ha   =            220
505  n
mi
                                          Hp   =            212
639

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21276019
80                 X    =         6463017
78
 Y    =        6490365
51  feet           Y    =         2050659
72  meter
 Z    =        -466283
16                 Z    =         -110674
58
 XDOT =      -4936
076100                 XDOT =       -1525
873693
 YDOT =      14856
827720  feet/sec       YDOT =        4511
417591  meter/sec
 ZDOT =     -19700
486034                 ZDOT =       -6012
068131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2589433
45                 X    =         -789259
32
 Y    =      -22095194
24  feet           Y    =        -6734615
20  meter
 Z    =        -329406
65                 Z    =         -100403
15
 XDOT =      13925
254884                 XDOT =        4244
417689
 YDOT =      -1364
569225  feet/sec       YDOT =        -415
920700  meter/sec
 ZDOT =     -19733
338469                 ZDOT =       -6014
721565


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   16213
49032126  
00016717  00000-0  10270-3 0  9142
2 25544  51
6388 196
9834 0002053  86
9600 273
1788 15
54929453 11872


Satellite: ISS
Catalog Number: 25544
Epoch time:      16213
49032126   =   yrday
fracday
Element set:     914
Inclination:       51
6388  deg
RA of node:       196
9834  deg
Eccentricity:     
0002053     
Arg of perigee:    86
9600  deg
Mean anomaly:     273
1788  deg
Mean motion:   15
54929453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1187
Checksum:              328


Coasting Arc #16 (Orbit 1202)
---------------------------------------

Vector Time (GMT): 2016/214/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5822390
50                 A    =         6785162
52  meter
 Y    =       -2796242
90  meter          E    =           
0015691
 Z    =        2055392
14                 I    =           51
57592
 XDOT =       3763
921278                 Wp   =           71
91694
 YDOT =      -3743
365649  meter/sec      RA   =          191
03129  deg
 ZDOT =       5539
577280                 TA   =          310
85482
                                          MA   =          310
99071
                                          Ha   =            220
404  n
mi
                                          Hp   =            212
684

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19102331
04                 X    =        -5800673
47
 Y    =       -9174025
25  feet           Y    =        -2861231
45  meter
 Z    =        6743412
55                 Z    =         2027161
61
 XDOT =      12348
823090                 XDOT =        3778
592492
 YDOT =     -12281
383363  feet/sec       YDOT =       -3701
193259  meter/sec
 ZDOT =      18174
466142                 ZDOT =        5557
896495

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -358863
70                 X    =         -109381
66
 Y    =       21226707
55  feet           Y    =         6469900
46  meter
 Z    =        6620687
78                 Z    =         2017985
64
 XDOT =     -14712
260304                 XDOT =       -4484
296941
 YDOT =      -5973
798788  feet/sec       YDOT =       -1820
813871  meter/sec
 ZDOT =      18255
009911                 ZDOT =        5564
127021


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   16214
51862084  
00016717  00000-0  10270-3 0  9151
2 25544  51
6386 191
8517 0001899  93
5107 266
6263 15
54969231 12037


Satellite: ISS
Catalog Number: 25544
Epoch time:      16214
51862084   =   yrday
fracday
Element set:     915
Inclination:       51
6386  deg
RA of node:       191
8517  deg
Eccentricity:     
0001899     
Arg of perigee:    93
5107  deg
Mean anomaly:     266
6263  deg
Mean motion:   15
54969231  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1203
Checksum:              322


Coasting Arc #17 (Orbit 1217)
---------------------------------------

Vector Time (GMT): 2016/215/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930540
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4504455
02                 A    =         6781207
23  meter
 Y    =        3446177
09  meter          E    =           
0007635
 Z    =       -3724707
43                 I    =           51
59368
 XDOT =      -5692
880032                 Wp   =           82
99701
 YDOT =       2814
875822  meter/sec      RA   =          186
04284  deg
 ZDOT =      -4286
914247                 TA   =          141
47136
                                          MA   =          141
41684
                                          Ha   =            220
488  n
mi
                                          Hp   =            212
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14778395
74                 X    =         4483676
82
 Y    =       11306355
27  feet           Y    =         3496432
89  meter
 Z    =      -12220168
75                 Z    =        -3702876
75
 XDOT =     -18677
427926                 XDOT =       -5703
110085
 YDOT =       9235
156896  feet/sec       YDOT =        2751
157212  meter/sec
 ZDOT =     -14064
679289                 ZDOT =       -4314
592921

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3770141
87                 X    =         1149139
24
 Y    =      -18284597
03  feet           Y    =        -5573145
17  meter
 Z    =      -12125457
37                 Z    =        -3695839
41
 XDOT =      15028
898458                 XDOT =        4580
808250
 YDOT =      12491
694859  feet/sec       YDOT =        3807
468593  meter/sec
 ZDOT =     -14185
924708                 ZDOT =       -4323
869851


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   16215
48265110  
00016717  00000-0  10270-3 0  9166
2 25544  51
6381 187
0395 0001997  91
9258 268
2123 15
54930294 12187


Satellite: ISS
Catalog Number: 25544
Epoch time:      16215
48265110   =   yrday
fracday
Element set:     916
Inclination:       51
6381  deg
RA of node:       187
0395  deg
Eccentricity:     
0001997     
Arg of perigee:    91
9258  deg
Mean anomaly:     268
2123  deg
Mean motion:   15
54930294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1218
Checksum:              317
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