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

 
Date: April 22nd 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 67 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


113/17:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 213 8

Coasting Arc #1 (Orbit 3597)
---------------------------------------

Vector Time (GMT): 2016/111/08:19:37
794
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6364821
64                 A    =         6788678
49  meter
 Y    =       -2216556
24  meter          E    =           
0012302
 Z    =        -766046
90                 I    =           51
57610
 XDOT =       2209
068745                 Wp   =           40
16346
 YDOT =       4309
926080  meter/sec      RA   =          345
97231  deg
 ZDOT =       5946
094670                 TA   =          311
54833
                                          MA   =          311
65377
                                          Ha   =            221
309  n
mi
                                          Hp   =            213
956

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20881960
76                 X    =         6392855
85
 Y    =       -7272166
13  feet           Y    =        -2145223
89  meter
 Z    =       -2513277
23                 Z    =         -735059
48
 XDOT =       7247
600869                 XDOT =        2131
825937
 YDOT =      14140
177427  feet/sec       YDOT =        4334
198019  meter/sec
 ZDOT =      19508
184612                 ZDOT =        5956
637899

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21916936
24                 X    =         6680282
16
 Y    =        3041236
98  feet           Y    =          926969
03  meter
 Z    =       -2378241
28                 Z    =         -724887
94
 XDOT =        122
889589                 XDOT =          37
456747
 YDOT =      14235
525678  feet/sec       YDOT =        4338
988227  meter/sec
 ZDOT =      19553
124969                 ZDOT =        5959
792491


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   16111
34836702  
00016717  00000-0  10270-3 0  9000
2 25544  51
6420 346
5375 0001826  43
8494 316
2804 15
54274926 35986


Satellite: ISS
Catalog Number: 25544
Epoch time:      16111
34836702   =   yrday
fracday
Element set:     900
Inclination:       51
6420  deg
RA of node:       346
5375  deg
Eccentricity:     
0001826     
Arg of perigee:    43
8494  deg
Mean anomaly:     316
2804  deg
Mean motion:   15
54274926  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3598
Checksum:              310


Coasting Arc #2 (Orbit 3613)
---------------------------------------

Vector Time (GMT): 2016/112/08:19:37
794
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6559869
35                 A    =         6788383
86  meter
 Y    =        1400500
79  meter          E    =           
0009576
 Z    =       -1022347
96                 I    =           51
54560
 XDOT =       -134
960676                 Wp   =          130
71268
 YDOT =      -4902
600447  meter/sec      RA   =          340
99656  deg
 ZDOT =      -5892
370270                 TA   =           60
38056
                                          MA   =           60
28521
                                          Ha   =            221
227  n
mi
                                          Hp   =            213
931

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21521881
05                 X    =        -6570076
34
 Y    =        4594818
88  feet           Y    =         1327086
82  meter
 Z    =       -3354159
97                 Z    =        -1054239
59
 XDOT =       -442
784371                 XDOT =         -51
505475
 YDOT =     -16084
647135  feet/sec       YDOT =       -4903
643523  meter/sec
 ZDOT =     -19331
923457                 ZDOT =       -5892
822779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21328557
02                 X    =        -6500944
18
 Y    =       -5333485
04  feet           Y    =        -1625646
24  meter
 Z    =       -3492951
00                 Z    =        -1064651
46
 XDOT =       6402
741841                 XDOT =        1951
555713
 YDOT =     -13030
540178  feet/sec       YDOT =       -3971
708646  meter/sec
 ZDOT =     -19332
916322                 ZDOT =       -5892
672895


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   16112
37709375  
00016717  00000-0  10270-3 0  9010
2 25544  51
6431 341
4084 0001745  46
8429 313
2869 15
54287116 36142


Satellite: ISS
Catalog Number: 25544
Epoch time:      16112
37709375   =   yrday
fracday
Element set:     901
Inclination:       51
6431  deg
RA of node:       341
4084  deg
Eccentricity:     
0001745     
Arg of perigee:    46
8429  deg
Mean anomaly:     313
2869  deg
Mean motion:   15
54287116  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3614
Checksum:              306


Coasting Arc #3 (Orbit 3629)
---------------------------------------

Vector Time (GMT): 2016/113/08:19:37
794
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6218187
53                 A    =         6785749
67  meter
 Y    =        -451110
06  meter          E    =           
0015166
 Z    =        2660320
80                 I    =           51
50669
 XDOT =      -1842
975406                 Wp   =           74
55669
 YDOT =       5339
525410  meter/sec      RA   =          336
01414  deg
 ZDOT =       5192
416486                 TA   =          315
53888
                                          MA   =          315
66051
                                          Ha   =            221
214  n
mi
                                          Hp   =            213
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20400877
73                 X    =         6209846
87
 Y    =       -1480019
87  feet           Y    =         -381620
60  meter
 Z    =        8728086
61                 Z    =         2690507
53
 XDOT =      -6046
507238                 XDOT =       -1927
769332
 YDOT =      17518
127984  feet/sec       YDOT =        5318
442270  meter/sec
 ZDOT =      17035
487160                 ZDOT =        5183
257291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19048534
13                 X    =         5805993
20
 Y    =        7296050
15  feet           Y    =         2223836
08  meter
 Z    =        8859275
74                 Z    =         2700307
24
 XDOT =     -12478
303018                 XDOT =       -3803
386760
 YDOT =      11861
084174  feet/sec       YDOT =        3615
258456  meter/sec
 ZDOT =      16994
650075                 ZDOT =        5179
969343


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   16113
40581336  
00016717  00000-0  10270-3 0  9021
2 25544  51
6429 336
2791 0001852  49
5765 310
5549 15
54296827 36300


Satellite: ISS
Catalog Number: 25544
Epoch time:      16113
40581336   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:       336
2791  deg
Eccentricity:     
0001852     
Arg of perigee:    49
5765  deg
Mean anomaly:     310
5549  deg
Mean motion:   15
54296827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3630
Checksum:              315


Coasting Arc #4 (Orbit 3634)
---------------------------------------

Vector Time (GMT): 2016/113/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -238525
45                 A    =         6777622
73  meter
 Y    =       -4430373
60  meter          E    =           
0014963
 Z    =       -5136890
32                 I    =           51
46752
 XDOT =       7193
032982                 Wp   =           97
78038
 YDOT =      -2143
892476  meter/sec      RA   =          334
14192  deg
 ZDOT =       1516
841893                 TA   =          186
87778
                                          MA   =          186
89834
                                          Ha   =            221
260  n
mi
                                          Hp   =            213
796

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -782563
80                 X    =         -164012
89
 Y    =      -14535346
47  feet           Y    =        -4432624
64  meter
 Z    =      -16853314
68                 Z    =        -5137867
78
 XDOT =      23599
189572                 XDOT =        7209
103611
 YDOT =      -7033
767966  feet/sec       YDOT =       -2063
365247  meter/sec
 ZDOT =       4976
515397                 ZDOT =        1551
823682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13675514
99                 X    =        -4168296
97
 Y    =        4975491
13  feet           Y    =         1516529
69  meter
 Z    =      -16856681
07                 Z    =        -5137916
39
 XDOT =     -13373
802826                 XDOT =       -4076
335101
 YDOT =     -19402
798983  feet/sec       YDOT =       -5913
973130  meter/sec
 ZDOT =       5128
861588                 ZDOT =        1563
277012


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   16113
72728648  
00016717  00000-0  10270-3 0  9036
2 25544  51
6417 334
6724 0001629  66
3066 293
8257 15
54314939 36357


Satellite: ISS
Catalog Number: 25544
Epoch time:      16113
72728648   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:       334
6724  deg
Eccentricity:     
0001629     
Arg of perigee:    66
3066  deg
Mean anomaly:     293
8257  deg
Mean motion:   15
54314939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3635
Checksum:              327


Coasting Arc #5 (Orbit 3650)
---------------------------------------

Vector Time (GMT): 2016/114/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1458536
97                 A    =         6780720
20  meter
 Y    =        4949607
46  meter          E    =           
0011072
 Z    =        4392223
43                 I    =           51
44838
 XDOT =      -6832
185261                 Wp   =           70
50932
 YDOT =        971
134855  meter/sec      RA   =          329
13222  deg
 ZDOT =      -3352
626156                 TA   =           53
51259
                                          MA   =           53
41063
                                          Ha   =            221
350  n
mi
                                          Hp   =            213
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4785226
29                 X    =        -1535112
27
 Y    =       16238869
63  feet           Y    =         4932869
17  meter
 Z    =       14410181
86                 Z    =         4384951
87
 XDOT =     -22415
305973                 XDOT =       -6826
251009
 YDOT =       3186
137977  feet/sec       YDOT =         894
765847  meter/sec
 ZDOT =     -10999
429647                 ZDOT =       -3385
801490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16950249
31                 X    =         5166435
99
 Y    =        -474999
30  feet           Y    =         -144779
79  meter
 Z    =       14377622
98                 Z    =         4382299
49
 XDOT =      10013
431350                 XDOT =        3052
093875
 YDOT =      18973
850544  feet/sec       YDOT =        5783
229646  meter/sec
 ZDOT =     -11143
690676                 ZDOT =       -3396
596918


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   16114
75599991  
00016717  00000-0  10270-3 0  9048
2 25544  51
6410 329
5423 0001613  72
4687 287
6642 15
54284437 36515


Satellite: ISS
Catalog Number: 25544
Epoch time:      16114
75599991   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       329
5423  deg
Eccentricity:     
0001613     
Arg of perigee:    72
4687  deg
Mean anomaly:     287
6642  deg
Mean motion:   15
54284437  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3651
Checksum:              327


Coasting Arc #6 (Orbit 3665)
---------------------------------------

Vector Time (GMT): 2016/115/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2912644
68                 A    =         6784551
29  meter
 Y    =       -5237785
10  meter          E    =           
0006051
 Z    =       -3183266
84                 I    =           51
43556
 XDOT =       5963
101272                 Wp   =           75
25059
 YDOT =        406
853567  meter/sec      RA   =          324
13172  deg
 ZDOT =       4795
871913                 TA   =          247
88480
                                          MA   =          247
94905
                                          Ha   =            221
254  n
mi
                                          Hp   =            213
884

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9555920
87                 X    =         2986461
66
 Y    =      -17184334
32  feet           Y    =        -5204801
32  meter
 Z    =      -10443788
86                 Z    =        -3168938
23
 XDOT =      19563
980552                 XDOT =        5934
811810
 YDOT =       1334
821414  feet/sec       YDOT =         473
378890  meter/sec
 ZDOT =      15734
487904                 ZDOT =        4824
771002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19400513
39                 X    =        -5913276
48
 Y    =       -3399171
75  feet           Y    =        -1036067
55  meter
 Z    =      -10380530
19                 Z    =        -3163985
60
 XDOT =      -5422
156505                 XDOT =       -1652
673303
 YDOT =     -17394
744796  feet/sec       YDOT =       -5301
918214  meter/sec
 ZDOT =      15859
901062                 ZDOT =        4834
097844


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   16115
72041226  
00016717  00000-0  10270-3 0  9050
2 25544  51
6421 324
7337 0001524  69
1227 291
0089 15
54311281 36660


Satellite: ISS
Catalog Number: 25544
Epoch time:      16115
72041226   =   yrday
fracday
Element set:     905
Inclination:       51
6421  deg
RA of node:       324
7337  deg
Eccentricity:     
0001524     
Arg of perigee:    69
1227  deg
Mean anomaly:     291
0089  deg
Mean motion:   15
54311281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3666
Checksum:              284


Coasting Arc #7 (Orbit 3681)
---------------------------------------

Vector Time (GMT): 2016/116/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4070572
94                 A    =         6787735
63  meter
 Y    =        5188038
93  meter          E    =           
0015078
 Z    =        1580454
55                 I    =           51
42126
 XDOT =      -4721
898364                 Wp   =          113
09881
 YDOT =      -1950
290002  meter/sec      RA   =          319
13960  deg
 ZDOT =      -5721
786641                 TA   =           49
55554
                                          MA   =           49
42415
                                          Ha   =            221
248  n
mi
                                          Hp   =            213
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13354898
11                 X    =        -4135961
66
 Y    =       17021125
08  feet           Y    =         5142153
48  meter
 Z    =        5185218
34                 Z    =         1560521
48
 XDOT =     -15491
792532                 XDOT =       -4671
944325
 YDOT =      -6398
589244  feet/sec       YDOT =       -2002
814182  meter/sec
 ZDOT =     -18772
265883                 ZDOT =       -5744
603485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20608473
48                 X    =         6281462
72
 Y    =        6653075
39  feet           Y    =         2027857
38  meter
 Z    =        5097636
74                 Z    =         1553759
68
 XDOT =       -186
630175                 XDOT =         -56
884877
 YDOT =      15133
646036  feet/sec       YDOT =        4612
735312  meter/sec
 ZDOT =     -18870
960064                 ZDOT =       -5751
868628


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   16116
74911434  
00016717  00000-0  10270-3 0  9061
2 25544  51
6424 319
6038 0001558  74
3310 285
8015 15
54325655 36820


Satellite: ISS
Catalog Number: 25544
Epoch time:      16116
74911434   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:       319
6038  deg
Eccentricity:     
0001558     
Arg of perigee:    74
3310  deg
Mean anomaly:     285
8015  deg
Mean motion:   15
54325655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3682
Checksum:              305


Coasting Arc #8 (Orbit 3697)
---------------------------------------

Vector Time (GMT): 2016/117/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4815428
88                 A    =         6788723
61  meter
 Y    =       -4773507
53  meter          E    =           
0013978
 Z    =         162739
06                 I    =           51
40141
 XDOT =       3261
709906                 Wp   =           50
18580
 YDOT =       3505
989316  meter/sec      RA   =          314
15270  deg
 ZDOT =       5991
122213                 TA   =          311
57354
                                          MA   =          311
69328
                                          Ha   =            221
275  n
mi
                                          Hp   =            213
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15798651
17                 X    =         4867659
01
 Y    =      -15661113
94  feet           Y    =        -4719366
16  meter
 Z    =         533920
79                 Z    =          186258
45
 XDOT =      10701
147984                 XDOT =        3193
159908
 YDOT =      11502
589620  feet/sec       YDOT =        3542
080671  meter/sec
 ZDOT =      19655
912771                 ZDOT =        6006
800502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20325622
66                 X    =        -6195249
79
 Y    =       -9034171
17  feet           Y    =        -2753615
37  meter
 Z    =         636988
87                 Z    =          194154
21
 XDOT =       6223
481081                 XDOT =        1896
917034
 YDOT =     -12546
545697  feet/sec       YDOT =       -3824
187128  meter/sec
 ZDOT =      19723
303299                 ZDOT =        6011
662845


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   16117
77781183  
00016717  00000-0  10270-3 0  9072
2 25544  51
6428 314
4748 0001674  74
9451 285
1887 15
54332167 36989


Satellite: ISS
Catalog Number: 25544
Epoch time:      16117
77781183   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       314
4748  deg
Eccentricity:     
0001674     
Arg of perigee:    74
9451  deg
Mean anomaly:     285
1887  deg
Mean motion:   15
54332167  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3698
Checksum:              345


Coasting Arc #9 (Orbit 3712)
---------------------------------------

Vector Time (GMT): 2016/118/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5186595
80                 A    =         6787045
62  meter
 Y    =        3926554
72  meter          E    =           
0007762
 Z    =       -1929438
61                 I    =           51
37451
 XDOT =      -1697
852733                 Wp   =          129
76786
 YDOT =      -4974
557231  meter/sec      RA   =          309
16347  deg
 ZDOT =      -5579
389337                 TA   =           71
57662
                                          MA   =           71
49225
                                          Ha   =            221
187  n
mi
                                          Hp   =            213
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17016390
41                 X    =        -5220745
54
 Y    =       12882397
39  feet           Y    =         3868363
81  meter
 Z    =       -6330179
17                 Z    =        -1954717
06
 XDOT =      -5570
382981                 XDOT =       -1614
997204
 YDOT =     -16320
725823  feet/sec       YDOT =       -4993
080487  meter/sec
 ZDOT =     -18305
083126                 ZDOT =       -5587
435923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18353255
87                 X    =         5594072
39
 Y    =       10828668
89  feet           Y    =         3300578
28  meter
 Z    =       -6440714
47                 Z    =        -1963129
77
 XDOT =     -12249
778521                 XDOT =       -3733
732493
 YDOT =       9892
159697  feet/sec       YDOT =        3015
130276  meter/sec
 ZDOT =     -18339
050711                 ZDOT =       -5589
742657


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   16118
74221101  
00016717  00000-0  10270-3 0  9080
2 25544  51
6429 309
6662 0001582  80
0771 280
0560 15
54350430 37135


Satellite: ISS
Catalog Number: 25544
Epoch time:      16118
74221101   =   yrday
fracday
Element set:     908
Inclination:       51
6429  deg
RA of node:       309
6662  deg
Eccentricity:     
0001582     
Arg of perigee:    80
0771  deg
Mean anomaly:     280
0560  deg
Mean motion:   15
54350430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3713
Checksum:              279


Coasting Arc #10 (Orbit 3728)
---------------------------------------

Vector Time (GMT): 2016/119/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5169144
23                 A    =         6783467
44  meter
 Y    =       -2715579
61  meter          E    =           
0013865
 Z    =        3440611
66                 I    =           51
34441
 XDOT =        205
997304                 Wp   =           89
89221
 YDOT =       6175
313064  meter/sec      RA   =          304
16488  deg
 ZDOT =       4548
633003                 TA   =          310
65615
                                          MA   =          310
77660
                                          Ha   =            221
085  n
mi
                                          Hp   =            213
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16959134
63                 X    =         5182413
17
 Y    =       -8909381
91  feet           Y    =        -2657700
59  meter
 Z    =       11288095
99                 Z    =         3465754
54
 XDOT =        675
844174                 XDOT =         114
832594
 YDOT =      20260
213463  feet/sec       YDOT =        6177
106949  meter/sec
 ZDOT =      14923
336624                 ZDOT =        4549
412240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14850855
00                 X    =        -4526540
60
 Y    =      -11998027
18  feet           Y    =        -3656998
68  meter
 Z    =       11397802
15                 Z    =         3474050
10
 XDOT =      17512
200833                 XDOT =        5337
718814
 YDOT =      -7448
293668  feet/sec       YDOT =       -2270
239910  meter/sec
 ZDOT =      14925
520932                 ZDOT =        4549
298780


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   16119
77089710  
00016717  00000-0  10270-3 0  9093
2 25544  51
6439 304
5369 0001599  82
6945 277
4389 15
54383310 37292


Satellite: ISS
Catalog Number: 25544
Epoch time:      16119
77089710   =   yrday
fracday
Element set:     909
Inclination:       51
6439  deg
RA of node:       304
5369  deg
Eccentricity:     
0001599     
Arg of perigee:    82
6945  deg
Mean anomaly:     277
4389  deg
Mean motion:   15
54383310  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3729
Checksum:              349


Coasting Arc #11 (Orbit 3743)
---------------------------------------

Vector Time (GMT): 2016/120/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4859820
26                 A    =         6779645
87  meter
 Y    =        1160566
30  meter          E    =           
0011819
 Z    =       -4594062
76                 I    =           51
31367
 XDOT =       1151
439120                 Wp   =           71
45990
 YDOT =      -6961
047414  meter/sec      RA   =          299
15448  deg
 ZDOT =      -2979
200694                 TA   =          168
66361
                                          MA   =          168
63696
                                          Ha   =            221
207  n
mi
                                          Hp   =            213
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15944292
18                 X    =        -4850120
66
 Y    =        3807632
21  feet           Y    =         1106274
74  meter
 Z    =      -15072384
39                 Z    =        -4617647
19
 XDOT =       3777
687401                 XDOT =        1243
665496
 YDOT =     -22838
082068  feet/sec       YDOT =       -6947
655622  meter/sec
 ZDOT =      -9774
280491                 ZDOT =       -2973
383161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9976069
56                 X    =         3040706
00
 Y    =       12887672
59  feet           Y    =         3928162
61  meter
 Z    =      -15175019
57                 Z    =        -4625345
96
 XDOT =     -21462
647932                 XDOT =       -6541
815090
 YDOT =       5146
142378  feet/sec       YDOT =        1568
544197  meter/sec
 ZDOT =      -9747
678681                 ZDOT =       -2971
092462


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   16120
73528780  
00016717  00000-0  10270-3 0  9108
2 25544  51
6435 299
7289 0001546  82
4619 277
6709 15
54345182 37442


Satellite: ISS
Catalog Number: 25544
Epoch time:      16120
73528780   =   yrday
fracday
Element set:     910
Inclination:       51
6435  deg
RA of node:       299
7289  deg
Eccentricity:     
0001546     
Arg of perigee:    82
4619  deg
Mean anomaly:     277
6709  deg
Mean motion:   15
54345182  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3744
Checksum:              334


Coasting Arc #12 (Orbit 3759)
---------------------------------------

Vector Time (GMT): 2016/121/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4305718
70                 A    =         6776945
71  meter
 Y    =         577475
83  meter          E    =           
0005074
 Z    =        5197590
21                 I    =           51
29024
 XDOT =      -2288
512723                 Wp   =          111
88919
 YDOT =       7241
925174  meter/sec      RA   =          294
13254  deg
 ZDOT =       1088
492700                 TA   =          327
62018
                                          MA   =          327
65130
                                          Ha   =            220
997  n
mi
                                          Hp   =            213
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14126373
70                 X    =         4273693
38
 Y    =        1894605
74  feet           Y    =          625446
29  meter
 Z    =       17052461
33                 Z    =         5218428
67
 XDOT =      -7508
243842                 XDOT =       -2374
611118
 YDOT =      23759
597027  feet/sec       YDOT =        7215
852121  meter/sec
 ZDOT =       3571
170275                 ZDOT =        1077
166315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4257436
99                 X    =        -1297666
79
 Y    =      -13488057
59  feet           Y    =        -4111159
95  meter
 Z    =       17142839
18                 Z    =         5225137
38
 XDOT =      23720
332742                 XDOT =        7229
957420
 YDOT =      -3001
371912  feet/sec       YDOT =        -914
818159  meter/sec
 ZDOT =       3520
606929                 ZDOT =        1073
080992


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   16121
76396480  
00016717  00000-0  10270-3 0  9113
2 25544  51
6434 294
5996 0001558  85
0199 275
1132 15
54396272 37601


Satellite: ISS
Catalog Number: 25544
Epoch time:      16121
76396480   =   yrday
fracday
Element set:     911
Inclination:       51
6434  deg
RA of node:       294
5996  deg
Eccentricity:     
0001558     
Arg of perigee:    85
0199  deg
Mean anomaly:     275
1132  deg
Mean motion:   15
54396272  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3760
Checksum:              328


Coasting Arc #13 (Orbit 3774)
---------------------------------------

Vector Time (GMT): 2016/122/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3615053
50                 A    =         6776919
81  meter
 Y    =       -2376356
70  meter          E    =           
0015940
 Z    =       -5230416
63                 I    =           51
27745
 XDOT =       3184
015517                 Wp   =           95
78678
 YDOT =      -6900
548325  meter/sec      RA   =          289
10578  deg
 ZDOT =        935
381221                 TA   =          183
21640
                                          MA   =          183
22666
                                          Ha   =            221
171  n
mi
                                          Hp   =            213
546

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11860411
74                 X    =        -3562804
48
 Y    =       -7796445
87  feet           Y    =        -2416490
67  meter
 Z    =      -17160159
56                 Z    =        -5247850
82
 XDOT =      10446
245136                 XDOT =        3256
398811
 YDOT =     -22639
594242  feet/sec       YDOT =       -6864
537794  meter/sec
 ZDOT =       3068
836028                 ZDOT =         951
024545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1807304
27                 X    =         -550866
34
 Y    =       13985674
09  feet           Y    =         4262833
46  meter
 Z    =      -17235416
51                 Z    =        -5253354
95
 XDOT =     -23896
630489                 XDOT =       -7283
692973
 YDOT =        775
599155  feet/sec       YDOT =         236
402622  meter/sec
 ZDOT =       3138
065888                 ZDOT =         956
482483


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   16122
72834603  
00016717  00000-0  10270-3 0  9125
2 25544  51
6432 289
7913 0001581  82
9436 277
1897 15
54382795 37751


Satellite: ISS
Catalog Number: 25544
Epoch time:      16122
72834603   =   yrday
fracday
Element set:     912
Inclination:       51
6432  deg
RA of node:       289
7913  deg
Eccentricity:     
0001581     
Arg of perigee:    82
9436  deg
Mean anomaly:     277
1897  deg
Mean motion:   15
54382795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3775
Checksum:              340


Coasting Arc #14 (Orbit 3790)
---------------------------------------

Vector Time (GMT): 2016/123/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2820005
22                 A    =         6779293
08  meter
 Y    =        4051633
39  meter          E    =           
0009705
 Z    =        4640599
78                 I    =           51
27615
 XDOT =      -3865
310979                 Wp   =           67
03792
 YDOT =       5978
011888  meter/sec      RA   =          284
08077  deg
 ZDOT =      -2861
918859                 TA   =           51
56774
                                          MA   =           51
48066
                                          Ha   =            221
058  n
mi
                                          Hp   =            213
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9251985
64                 X    =         2751946
98
 Y    =       13292760
47  feet           Y    =         4082788
23  meter
 Z    =       15225064
89                 Z    =         4654133
33
 XDOT =     -12681
466468                 XDOT =       -3917
969201
 YDOT =      19612
899894  feet/sec       YDOT =        5934
492855  meter/sec
 ZDOT =      -9389
497569                 ZDOT =       -2880
823936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7641430
35                 X    =         2329107
97
 Y    =      -14217435
36  feet           Y    =        -4333474
30  meter
 Z    =       15283075
41                 Z    =         4658281
39
 XDOT =      22175
193518                 XDOT =        6758
998984
 YDOT =       1705
863803  feet/sec       YDOT =         519
947287  meter/sec
 ZDOT =      -9472
704909                 ZDOT =       -2887
280456


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   16123
75701272  
00016717  00000-0  10270-3 0  9135
2 25544  51
6433 284
6613 0001617  82
0293 278
1043 15
54409434 37917


Satellite: ISS
Catalog Number: 25544
Epoch time:      16123
75701272   =   yrday
fracday
Element set:     913
Inclination:       51
6433  deg
RA of node:       284
6613  deg
Eccentricity:     
0001617     
Arg of perigee:    82
0293  deg
Mean anomaly:     278
1043  deg
Mean motion:   15
54409434  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3791
Checksum:              296


Coasting Arc #15 (Orbit 3805)
---------------------------------------

Vector Time (GMT): 2016/124/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2010092
68                 A    =         6783177
02  meter
 Y    =       -5428140
85  meter          E    =           
0006838
 Z    =       -3542842
81                 I    =           51
28085
 XDOT =       4326
101444                 Wp   =           94
23146
 YDOT =      -4498
376910  meter/sec      RA   =          279
06591  deg
 ZDOT =       4444
613906                 TA   =          223
77142
                                          MA   =          223
82565
                                          Ha   =            221
149  n
mi
                                          Hp   =            213
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6594792
25                 X    =        -1932034
60
 Y    =      -17808861
04  feet           Y    =        -5450182
75  meter
 Z    =      -11623500
04                 Z    =        -3552417
64
 XDOT =      14193
246208                 XDOT =        4354
491555
 YDOT =     -14758
454429  feet/sec       YDOT =       -4449
840621  meter/sec
 ZDOT =      14582
066621                 ZDOT =        4465
698495

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12620117
44                 X    =        -3846611
80
 Y    =       14157493
30  feet           Y    =         4315203
96  meter
 Z    =      -11664072
55                 Z    =        -3555209
31
 XDOT =     -18633
683402                 XDOT =       -5679
546701
 YDOT =      -4538
958917  feet/sec       YDOT =       -1383
474678  meter/sec
 ZDOT =      14674
453504                 ZDOT =        4472
773428


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   16124
72138485  
00016717  00000-0  10270-3 0  9144
2 25544  51
6420 279
8531 0001625  89
2179 270
9160 15
54401667 38066


Satellite: ISS
Catalog Number: 25544
Epoch time:      16124
72138485   =   yrday
fracday
Element set:     914
Inclination:       51
6420  deg
RA of node:       279
8531  deg
Eccentricity:     
0001625     
Arg of perigee:    89
2179  deg
Mean anomaly:     270
9160  deg
Mean motion:   15
54401667  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3806
Checksum:              314


Coasting Arc #16 (Orbit 3821)
---------------------------------------

Vector Time (GMT): 2016/125/17:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945238
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1155705
41                 A    =         6786802
13  meter
 Y    =        6373744
85  meter          E    =           
0015466
 Z    =        2001574
22                 I    =           51
28918
 XDOT =      -4633
926787                 Wp   =          109
06629
 YDOT =       2589
007312  meter/sec      RA   =          274
06101  deg
 ZDOT =      -5538
562321                 TA   =           48
70282
                                          MA   =           48
56977
                                          Ha   =            221
137  n
mi
                                          Hp   =            213
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3791684
42                 X    =         1074623
74
 Y    =       20911236
38  feet           Y    =         6386215
44  meter
 Z    =        6566844
55                 Z    =         2006991
26
 XDOT =     -15203
171874                 XDOT =       -4635
628853
 YDOT =       8494
118478  feet/sec       YDOT =        2537
177927  meter/sec
 ZDOT =     -18171
136225                 ZDOT =       -5561
077434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16433513
72                 X    =         5008934
98
 Y    =      -13464851
99  feet           Y    =        -4104086
89  meter
 Z    =        6589196
67                 Z    =         2008387
15
 XDOT =      13785
642976                 XDOT =        4201
863979
 YDOT =       7836
414812  feet/sec       YDOT =        2388
539235  meter/sec
 ZDOT =     -18269
378018                 ZDOT =       -5568
506420


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   16125
75004202  
00016717  00000-0  10270-3 0  9158
2 25544  51
6422 274
7231 0001651  87
8413 272
2928 15
54410514 38229


Satellite: ISS
Catalog Number: 25544
Epoch time:      16125
75004202   =   yrday
fracday
Element set:     915
Inclination:       51
6422  deg
RA of node:       274
7231  deg
Eccentricity:     
0001651     
Arg of perigee:    87
8413  deg
Mean anomaly:     272
2928  deg
Mean motion:   15
54410514  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3822
Checksum:              281
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