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

 
Date: June 9th 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) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


160/14:01:59 311 -0 8 1 4 1 4
N/A 0 6 -0 1 220 3
000/00:03:58 622 1 1 0 0 214 2

161/01:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 214 2

166/12:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 1

170/05:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 214 0

171/22:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 0

Coasting Arc #1 (Orbit 333)
---------------------------------------

Vector Time (GMT): 2016/158/14:32:13
705
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4414619
76                 A    =         6781447
86  meter
 Y    =        3455933
85  meter          E    =           
0012164
 Z    =        3806840
83                 I    =           51
98755
 XDOT =      -1249
248679                 Wp   =          100
84582
 YDOT =      -6274
733948  meter/sec      RA   =          109
88942  deg
 ZDOT =       4233
985493                 TA   =          304
63306
                                          MA   =          304
74769
                                          Ha   =            220
314  n
mi
                                          Hp   =            213
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14483660
63                 X    =        -4471428
83
 Y    =       11338365
66  feet           Y    =         3406248
45  meter
 Z    =       12489635
28                 Z    =         3785258
15
 XDOT =      -4098
584904                 XDOT =       -1199
557131
 YDOT =     -20586
397467  feet/sec       YDOT =       -6288
426645  meter/sec
 ZDOT =      13891
028519                 ZDOT =        4228
036725

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16072024
42                 X    =         4898753
04
 Y    =        9076395
14  feet           Y    =         2766485
24  meter
 Z    =       12394959
99                 Z    =         3777983
81
 XDOT =     -16724
724236                 XDOT =       -5097
695947
 YDOT =      10617
498418  feet/sec       YDOT =        3236
213518  meter/sec
 ZDOT =      13866
269507                 ZDOT =        4226
438946


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   16158
66190516  
00016717  00000-0  10270-3 0  9002
2 25544  51
6424 110
5376 0001021 150
9705 209
1505 15
54755394  3348


Satellite: ISS
Catalog Number: 25544
Epoch time:      16158
66190516   =   yrday
fracday
Element set:     900
Inclination:       51
6424  deg
RA of node:       110
5376  deg
Eccentricity:     
0001021     
Arg of perigee:   150
9705  deg
Mean anomaly:     209
1505  deg
Mean motion:   15
54755394  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             334
Checksum:              284


Coasting Arc #2 (Orbit 348)
---------------------------------------

Vector Time (GMT): 2016/159/14:32:13
705
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4399653
74                 A    =         6777366
09  meter
 Y    =       -1634707
44  meter          E    =           
0012128
 Z    =       -4900305
22                 I    =           51
98536
 XDOT =         15
686281                 Wp   =           77
19661
 YDOT =       7269
702270  meter/sec      RA   =          104
91749  deg
 ZDOT =      -2413
441829                 TA   =          169
24336
                                          MA   =          169
21740
                                          Ha   =            220
183  n
mi
                                          Hp   =            213
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14434559
51                 X    =         4441410
01
 Y    =       -5363213
38  feet           Y    =        -1585273
44  meter
 Z    =      -16077116
87                 Z    =        -4878831
62
 XDOT =         51
464176                 XDOT =         -53
883067
 YDOT =      23850
729232  feet/sec       YDOT =        7269
489030  meter/sec
 ZDOT =      -7918
116236                 ZDOT =       -2413
533607

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10741359
91                 X    =        -3273966
50
 Y    =      -11169308
04  feet           Y    =        -3404405
09  meter
 Z    =      -15983241
16                 Z    =        -4871691
91
 XDOT =      20995
315336                 XDOT =        6399
372114
 YDOT =      -8868
929945  feet/sec       YDOT =       -2703
249847  meter/sec
 ZDOT =      -7919
871777                 ZDOT =       -2413
976918


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   16159
62604132  
00016717  00000-0  10270-3 0  9014
2 25544  51
6435 105
7274 0000967 148
5774 211
5437 15
54787024  3492


Satellite: ISS
Catalog Number: 25544
Epoch time:      16159
62604132   =   yrday
fracday
Element set:     901
Inclination:       51
6435  deg
RA of node:       105
7274  deg
Eccentricity:     
0000967     
Arg of perigee:   148
5774  deg
Mean anomaly:     211
5437  deg
Mean motion:   15
54787024  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             349
Checksum:              310


Coasting Arc #3 (Orbit 363)
---------------------------------------

Vector Time (GMT): 2016/160/14:03:58
622
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         499959
88                 A    =         6786420
49  meter
 Y    =        6442878
29  meter          E    =           
0006456
 Z    =       -2065500
32                 I    =           52
01974
 XDOT =      -4800
506537                 Wp   =           38
59237
 YDOT =       2155
240238  meter/sec      RA   =          100
01320  deg
 ZDOT =       5575
084255                 TA   =          298
68616
                                          MA   =          298
75105
                                          Ha   =            220
317  n
mi
                                          Hp   =            214
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1640288
32                 X    =          437910
12
 Y    =       21138052
15  feet           Y    =         6448122
49  meter
 Z    =       -6776575
87                 Z    =        -2063221
57
 XDOT =     -15749
693364                 XDOT =       -4851
331452
 YDOT =       7070
998155  feet/sec       YDOT =        2101
272915  meter/sec
 ZDOT =      18290
958841                 ZDOT =        5551
641490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19648626
22                 X    =         5988901
27
 Y    =       -7972288
90  feet           Y    =        -2429953
66  meter
 Z    =       -6767855
81                 Z    =        -2062842
45
 XDOT =      10942
112824                 XDOT =        3335
155989
 YDOT =      11567
322848  feet/sec       YDOT =        3525
720004  meter/sec
 ZDOT =      18188
393689                 ZDOT =        5543
822397


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   16160
59017408  
00016717  00000-0  10270-3 0  9027
2 25544  51
6430 100
9170 0000276 289
7583  70
3540 15
54506769  3646


Satellite: ISS
Catalog Number: 25544
Epoch time:      16160
59017408   =   yrday
fracday
Element set:     902
Inclination:       51
6430  deg
RA of node:       100
9170  deg
Eccentricity:     
0000276     
Arg of perigee:   289
7583  deg
Mean anomaly:      70
3540  deg
Mean motion:   15
54506769  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             364
Checksum:              297


Coasting Arc #4 (Orbit 371)
---------------------------------------

Vector Time (GMT): 2016/161/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3733655
28                 A    =         6777043
21  meter
 Y    =       -2359399
97  meter          E    =           
0004505
 Z    =        5137605
23                 I    =           51
99208
 XDOT =       2255
156807                 Wp   =           55
34642
 YDOT =      -7146
736248  meter/sec      RA   =           97
66773  deg
 ZDOT =      -1639
672881                 TA   =           50
41320
                                          MA   =           50
37342
                                          Ha   =            220
359  n
mi
                                          Hp   =            214
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12249525
19                 X    =        -3731950
55
 Y    =       -7740813
55  feet           Y    =        -2401143
24  meter
 Z    =       16855660
21                 Z    =         5119472
01
 XDOT =       7398
808423                 XDOT =        2342
870586
 YDOT =     -23447
297403  feet/sec       YDOT =       -7121
026959  meter/sec
 ZDOT =      -5379
504202                 ZDOT =       -1628
505709

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5885531
00                 X    =         1793909
85
 Y    =      -13340706
18  feet           Y    =        -4066247
24  meter
 Z    =       16777080
40                 Z    =         5113654
10
 XDOT =      23299
057931                 XDOT =        7101
552857
 YDOT =       3562
020257  feet/sec       YDOT =        1085
703774  meter/sec
 ZDOT =      -5329
490446                 ZDOT =       -1624
428688


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   16161
10446490  
00016717  00000-0  10270-3 0  9033
2 25544  51
6438  98
3485 0000489 231
7355 128
3754 15
54532693  3728


Satellite: ISS
Catalog Number: 25544
Epoch time:      16161
10446490   =   yrday
fracday
Element set:     903
Inclination:       51
6438  deg
RA of node:        98
3485  deg
Eccentricity:     
0000489     
Arg of perigee:   231
7355  deg
Mean anomaly:     128
3754  deg
Mean motion:   15
54532693  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             372
Checksum:              315


Coasting Arc #5 (Orbit 386)
---------------------------------------

Vector Time (GMT): 2016/162/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3206792
46                 A    =         6780203
91  meter
 Y    =        4105768
27  meter          E    =           
0008367
 Z    =       -4348039
39                 I    =           52
00604
 XDOT =      -3036
052571                 Wp   =          113
09245
 YDOT =       6092
196733  meter/sec      RA   =           92
69538  deg
 ZDOT =       3515
742750                 TA   =          192
51053
                                          MA   =          192
53131
                                          Ha   =            220
236  n
mi
                                          Hp   =            214
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10520972
65                 X    =         3181763
20
 Y    =       13470368
36  feet           Y    =         4141489
24  meter
 Z    =      -14265221
11                 Z    =        -4332522
06
 XDOT =      -9960
802398                 XDOT =       -3121
029283
 YDOT =      19987
522090  feet/sec       YDOT =        6057
770100  meter/sec
 ZDOT =      11534
589076                 ZDOT =        3500
788621

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11590822
37                 X    =        -3532882
66
 Y    =       12637139
09  feet           Y    =         3851799
99  meter
 Z    =      -14198372
25                 Z    =        -4327663
86
 XDOT =     -20418
695978                 XDOT =       -6223
618534
 YDOT =      -5851
037963  feet/sec       YDOT =       -1783
396371  meter/sec
 ZDOT =      11468
258672                 ZDOT =        3495
525243


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   16162
06875903  
00016717  00000-0  10270-3 0  9045
2 25544  51
6438  93
5400 0000449 231
8926 128
2187 15
54538535  3879


Satellite: ISS
Catalog Number: 25544
Epoch time:      16162
06875903   =   yrday
fracday
Element set:     904
Inclination:       51
6438  deg
RA of node:        93
5400  deg
Eccentricity:     
0000449     
Arg of perigee:   231
8926  deg
Mean anomaly:     128
2187  deg
Mean motion:   15
54538535  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             387
Checksum:              318


Coasting Arc #6 (Orbit 402)
---------------------------------------

Vector Time (GMT): 2016/163/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2571591
65                 A    =         6784368
67  meter
 Y    =       -5500817
39  meter          E    =           
0012871
 Z    =        3012648
85                 I    =           52
01995
 XDOT =       3722
113044                 Wp   =           97
80712
 YDOT =      -4482
413799  meter/sec      RA   =           87
73365  deg
 ZDOT =      -4990
820317                 TA   =           47
87034
                                          MA   =           47
76102
                                          Ha   =            220
315  n
mi
                                          Hp   =            214
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8436980
49                 X    =        -2524523
11
 Y    =      -18047301
14  feet           Y    =        -5529311
71  meter
 Z    =        9884018
54                 Z    =         3000270
61
 XDOT =      12211
656967                 XDOT =        3796
203057
 YDOT =     -14706
082018  feet/sec       YDOT =       -4440
375980  meter/sec
 ZDOT =     -16374
082404                 ZDOT =       -4972
559695

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16251272
82                 X    =         4953387
96
 Y    =      -11568350
14  feet           Y    =        -3526033
12  meter
 Z    =        9831121
36                 Z    =         2996525
79
 XDOT =      15816
504311                 XDOT =        4820
870514
 YDOT =       8326
144184  feet/sec       YDOT =        2537
808747  meter/sec
 ZDOT =     -16293
637767                 ZDOT =       -4966
300791


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   16163
09733336  
00016717  00000-0  10270-3 0  9053
2 25544  51
6434  88
4101 0000340 242
6884 117
4234 15
54524772  4039


Satellite: ISS
Catalog Number: 25544
Epoch time:      16163
09733336   =   yrday
fracday
Element set:     905
Inclination:       51
6434  deg
RA of node:        88
4101  deg
Eccentricity:     
0000340     
Arg of perigee:   242
6884  deg
Mean anomaly:     117
4234  deg
Mean motion:   15
54524772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             403
Checksum:              286


Coasting Arc #7 (Orbit 417)
---------------------------------------

Vector Time (GMT): 2016/164/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1863352
15                 A    =         6787513
95  meter
 Y    =        6383516
23  meter          E    =           
0008541
 Z    =       -1340917
94                 I    =           52
02761
 XDOT =      -4290
594510                 Wp   =           35
18229
 YDOT =       2476
437873  meter/sec      RA   =           82
78262  deg
 ZDOT =       5852
229722                 TA   =          310
29598
                                          MA   =          310
37060
                                          Ha   =            220
275  n
mi
                                          Hp   =            214
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6113360
09                 X    =         1798345
18
 Y    =       20943294
71  feet           Y    =         6403990
10  meter
 Z    =       -4399337
08                 Z    =        -1332023
67
 XDOT =     -14076
753642                 XDOT =       -4346
395350
 YDOT =       8124
796171  feet/sec       YDOT =        2428
145151  meter/sec
 ZDOT =      19200
228748                 ZDOT =        5831
251761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19349660
41                 X    =        -5897776
49
 Y    =       10095258
86  feet           Y    =         3077034
90  meter
 Z    =       -4361802
60                 Z    =        -1329477
43
 XDOT =      -9995
626772                 XDOT =       -3046
667040
 YDOT =     -10938
779490  feet/sec       YDOT =       -3334
139989  meter/sec
 ZDOT =      19108
318767                 ZDOT =        5824
215560


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   16164
06161606  
00016717  00000-0  10270-3 0  9067
2 25544  51
6430  83
6008 0000453 271
6052  88
5049 15
54493767  4189


Satellite: ISS
Catalog Number: 25544
Epoch time:      16164
06161606   =   yrday
fracday
Element set:     906
Inclination:       51
6430  deg
RA of node:        83
6008  deg
Eccentricity:     
0000453     
Arg of perigee:   271
6052  deg
Mean anomaly:      88
5049  deg
Mean motion:   15
54493767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             418
Checksum:              300


Coasting Arc #8 (Orbit 433)
---------------------------------------

Vector Time (GMT): 2016/165/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1019296
61                 A    =         6788005
32  meter
 Y    =       -6685032
81  meter          E    =           
0010759
 Z    =        -527875
93                 I    =           52
02473
 XDOT =       4748
944874                 Wp   =          140
33904
 YDOT =       -254
991338  meter/sec      RA   =           77
83719  deg
 ZDOT =      -6016
044732                 TA   =           45
32689
                                          MA   =           45
23926
                                          Ha   =            220
216  n
mi
                                          Hp   =            214
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3344149
00                 X    =         -941902
95
 Y    =      -21932522
34  feet           Y    =        -6695998
49  meter
 Z    =       -1731876
43                 Z    =         -532639
94
 XDOT =      15580
527802                 XDOT =        4780
666696
 YDOT =       -836
585753  feet/sec       YDOT =        -201
707664  meter/sec
 ZDOT =     -19737
679567                 ZDOT =       -5992
898479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20733867
91                 X    =         6319682
94
 Y    =       -7890360
99  feet           Y    =        -2404982
03  meter
 Z    =       -1751339
40                 Z    =         -533808
25
 XDOT =       3561
881594                 XDOT =        1085
661510
 YDOT =      13664
031196  feet/sec       YDOT =        4164
796709  meter/sec
 ZDOT =     -19636
746291                 ZDOT =       -5985
280269


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   16165
09017824  
00016717  00000-0  10270-3 0  9074
2 25544  51
6429  78
4706 0000380 260
6728  99
4382 15
54542047  4346


Satellite: ISS
Catalog Number: 25544
Epoch time:      16165
09017824   =   yrday
fracday
Element set:     907
Inclination:       51
6429  deg
RA of node:        78
4706  deg
Eccentricity:     
0000380     
Arg of perigee:   260
6728  deg
Mean anomaly:      99
4382  deg
Mean motion:   15
54542047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             434
Checksum:              314


Coasting Arc #9 (Orbit 449)
---------------------------------------

Vector Time (GMT): 2016/166/01:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          80656
38                 A    =         6785855
75  meter
 Y    =        6375706
86  meter          E    =           
0013560
 Z    =        2303281
94                 I    =           52
01024
 XDOT =      -5045
155014                 Wp   =           71
67025
 YDOT =      -1914
029972  meter/sec      RA   =           72
88844  deg
 ZDOT =       5452
837014                 TA   =          313
86590
                                          MA   =          313
97785
                                          Ha   =            220
236  n
mi
                                          Hp   =            214
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         264620
65                 X    =           -1832
77
 Y    =       20917673
42  feet           Y    =         6376147
41  meter
 Z    =        7556699
29                 Z    =         2303473
89
 XDOT =     -16552
345846                 XDOT =       -5049
864524
 YDOT =      -6279
625894  feet/sec       YDOT =       -1970
475013  meter/sec
 ZDOT =      17889
885217                 ZDOT =        5428
317222

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20318177
43                 X    =        -6192980
48
 Y    =        4979663
41  feet           Y    =         1517801
41  meter
 Z    =        7556282
69                 Z    =         2303154
96
 XDOT =       2675
517595                 XDOT =         815
497763
 YDOT =     -16178
094100  feet/sec       YDOT =       -4931
083082  meter/sec
 ZDOT =      17783
391205                 ZDOT =        5420
377639


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   16166
11873192  
00016717  00000-0  10270-3 0  9087
2 25544  51
6432  73
3401 0000325 284
1569  75
9548 15
54550502  4505


Satellite: ISS
Catalog Number: 25544
Epoch time:      16166
11873192   =   yrday
fracday
Element set:     908
Inclination:       51
6432  deg
RA of node:        73
3401  deg
Eccentricity:     
0000325     
Arg of perigee:   284
1569  deg
Mean anomaly:      75
9548  deg
Mean motion:   15
54550502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             450
Checksum:              296


Coasting Arc #10 (Orbit 455)
---------------------------------------

Vector Time (GMT): 2016/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3700280
56                 A    =         6785927
64  meter
 Y    =        5218725
50  meter          E    =           
0006154
 Z    =       -2257610
04                 I    =           52
00684
 XDOT =      -2966
741295                 Wp   =           39
05641
 YDOT =       4467
788399  meter/sec      RA   =           70
66217  deg
 ZDOT =       5477
984100                 TA   =          295
96598
                                          MA   =          296
02936
                                          Ha   =            220
250  n
mi
                                          Hp   =            214
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12140028
08                 X    =         3652615
00
 Y    =       17121802
84  feet           Y    =         5259838
18  meter
 Z    =       -7406857
10                 Z    =        -2239750
26
 XDOT =      -9733
403200                 XDOT =       -3043
090554
 YDOT =      14658
098421  feet/sec       YDOT =        4434
184982  meter/sec
 ZDOT =      17972
388778                 ZDOT =        5463
387256

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18588730
67                 X    =         5665845
11
 Y    =       -9804461
87  feet           Y    =        -2988399
98  meter
 Z    =       -7330045
42                 Z    =        -2234197
84
 XDOT =      12506
124647                 XDOT =        3811
866792
 YDOT =      10354
163247  feet/sec       YDOT =        3155
948958  meter/sec
 ZDOT =      17907
885822                 ZDOT =        5458
323598


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   16166
50443921  
00016717  00000-0  10270-3 0  9094
2 25544  51
6437  71
4182 0000450 325
9682  34
1442 15
54568876  4563


Satellite: ISS
Catalog Number: 25544
Epoch time:      16166
50443921   =   yrday
fracday
Element set:     909
Inclination:       51
6437  deg
RA of node:        71
4182  deg
Eccentricity:     
0000450     
Arg of perigee:   325
9682  deg
Mean anomaly:      34
1442  deg
Mean motion:   15
54568876  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             456
Checksum:              311


Coasting Arc #11 (Orbit 471)
---------------------------------------

Vector Time (GMT): 2016/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3091502
63                 A    =         6788048
15  meter
 Y    =       -6020620
56  meter          E    =           
0012431
 Z    =         437365
64                 I    =           52
00250
 XDOT =       4028
171954                 Wp   =          130
31040
 YDOT =      -2513
556892  meter/sec      RA   =           65
71393  deg
 ZDOT =      -6023
307826                 TA   =           44
99560
                                          MA   =           44
89494
                                          Ha   =            220
237  n
mi
                                          Hp   =            214
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10142725
17                 X    =        -3026073
32
 Y    =      -19752692
13  feet           Y    =        -6054826
01  meter
 Z    =        1434926
64                 Z    =          422506
16
 XDOT =      13215
787252                 XDOT =        4085
238632
 YDOT =      -8246
577729  feet/sec       YDOT =       -2468
191559  meter/sec
 ZDOT =     -19761
508617                 ZDOT =       -6003
601458

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20795316
71                 X    =        -6338412
53
 Y    =        7795954
13  feet           Y    =         2376206
82  meter
 Z    =        1371363
19                 Z    =          417991
50
 XDOT =      -6079
222731                 XDOT =       -1852
947088
 YDOT =     -12691
959421  feet/sec       YDOT =       -3868
509231  meter/sec
 ZDOT =     -19675
116630                 ZDOT =       -5996
975549


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   16167
53298449  
00016717  00000-0  10270-3 0  9103
2 25544  51
6440  66
2886 0000405 308
8732  51
2385 15
54544142  4720


Satellite: ISS
Catalog Number: 25544
Epoch time:      16167
53298449   =   yrday
fracday
Element set:     910
Inclination:       51
6440  deg
RA of node:        66
2886  deg
Eccentricity:     
0000405     
Arg of perigee:   308
8732  deg
Mean anomaly:      51
2385  deg
Mean motion:   15
54544142  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             472
Checksum:              307


Coasting Arc #12 (Orbit 487)
---------------------------------------

Vector Time (GMT): 2016/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2235148
26                 A    =         6787187
12  meter
 Y    =        6244819
81  meter          E    =           
0013847
 Z    =        1406560
50                 I    =           51
98682
 XDOT =      -4965
918052                 Wp   =           57
93751
 YDOT =        456
650744  meter/sec      RA   =           60
76530  deg
 ZDOT =       5829
179905                 TA   =          317
32868
                                          MA   =          317
43615
                                          Ha   =            220
198  n
mi
                                          Hp   =            214
083

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7333163
58                 X    =         2158318
48
 Y    =       20488253
98  feet           Y    =         6269385
00  meter
 Z    =        4614699
79                 Z    =         1417232
42
 XDOT =     -16292
382061                 XDOT =       -4998
971222
 YDOT =       1498
197979  feet/sec       YDOT =         400
933117  meter/sec
 ZDOT =      19124
605986                 ZDOT =        5804
976290

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21109511
53                 X    =         6434179
11
 Y    =       -5245250
34  feet           Y    =        -1598752
30  meter
 Z    =        4659953
36                 Z    =         1420353
78
 XDOT =       -510
107075                 XDOT =        -155
480636
 YDOT =      14943
914794  feet/sec       YDOT =        4554
905229  meter/sec
 ZDOT =      19019
022664                 ZDOT =        5796
998108


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   16168
56152047  
00016717  00000-0  10270-3 0  9111
2 25544  51
6449  61
1578 0000642 329
1021  31
0094 15
54572502  4882


Satellite: ISS
Catalog Number: 25544
Epoch time:      16168
56152047   =   yrday
fracday
Element set:     911
Inclination:       51
6449  deg
RA of node:        61
1578  deg
Eccentricity:     
0000642     
Arg of perigee:   329
1021  deg
Mean anomaly:      31
0094  deg
Mean motion:   15
54572502  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             488
Checksum:              287


Coasting Arc #13 (Orbit 502)
---------------------------------------

Vector Time (GMT): 2016/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 908273
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1085115
30                 A    =         6783908
33  meter
 Y    =       -5930818
71  meter          E    =           
0004021
 Z    =       -3112216
76                 I    =           51
95932
 XDOT =       5683
323623                 Wp   =           99
00683
 YDOT =       1532
432244  meter/sec      RA   =           55
81087  deg
 ZDOT =      -4907
863387                 TA   =          116
61263
                                          MA   =          116
57143
                                          Ha   =            220
154  n
mi
                                          Hp   =            214
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3560089
57                 X    =        -1003596
83
 Y    =      -19458066
63  feet           Y    =        -5942497
02  meter
 Z    =      -10210684
92                 Z    =        -3117290
74
 XDOT =      18646
074880                 XDOT =        5689
605649
 YDOT =       5027
664841  feet/sec       YDOT =        1596
022669  meter/sec
 ZDOT =     -16101
914000                 ZDOT =       -4880
239566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19679214
16                 X    =        -5998224
48
 Y    =        1895194
83  feet           Y    =          577655
38  meter
 Z    =      -10231590
69                 Z    =        -3118588
84
 XDOT =       6677
067245                 XDOT =        2035
170096
 YDOT =     -16841
990948  feet/sec       YDOT =       -5133
438841  meter/sec
 ZDOT =     -15981
828410                 ZDOT =       -4871
261299


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   16169
52576604  
00016717  00000-0  10270-3 0  9128
2 25544  51
6448  56
3490 0000633 319
8734  40
2372 15
54574081  5030


Satellite: ISS
Catalog Number: 25544
Epoch time:      16169
52576604   =   yrday
fracday
Element set:     912
Inclination:       51
6448  deg
RA of node:        56
3490  deg
Eccentricity:     
0000633     
Arg of perigee:   319
8734  deg
Mean anomaly:      40
2372  deg
Mean motion:   15
54574081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             503
Checksum:              302


Coasting Arc #14 (Orbit 514)
---------------------------------------

Vector Time (GMT): 2016/170/05:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 893042
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         421272
56                 A    =         6781402
89  meter
 Y    =        5522783
16  meter          E    =           
0010796
 Z    =        3904517
65                 I    =           51
93381
 XDOT =      -5991
872737                 Wp   =           97
26831
 YDOT =      -2458
328988  meter/sec      RA   =           52
12892  deg
 ZDOT =       4112
651072                 TA   =          309
77148
                                          MA   =          309
86651
                                          Ha   =            220
119  n
mi
                                          Hp   =            214
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1382127
81                 X    =          340517
51
 Y    =       18119367
32  feet           Y    =         5527042
07  meter
 Z    =       12810097
27                 Z    =         3906368
68
 XDOT =     -19658
375122                 XDOT =       -5983
915372
 YDOT =      -8065
383819  feet/sec       YDOT =       -2525
290147  meter/sec
 ZDOT =      13492
949710                 ZDOT =        4083
562861

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -941759
37                 X    =         -287048
26
 Y    =       18142688
60  feet           Y    =         5529891
49  meter
 Z    =       12817030
90                 Z    =         3906631
02
 XDOT =     -17278
694230                 XDOT =       -5266
546001
 YDOT =     -10365
469455  feet/sec       YDOT =       -3159
395090  meter/sec
 ZDOT =      13366
673830                 ZDOT =        4074
162183


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   16170
29715777  
00016717  00000-0  10270-3 0  9131
2 25544  51
6409  52
5004 0000497 320
7979  39
3138 15
54626116  5155


Satellite: ISS
Catalog Number: 25544
Epoch time:      16170
29715777   =   yrday
fracday
Element set:     913
Inclination:       51
6409  deg
RA of node:        52
5004  deg
Eccentricity:     
0000497     
Arg of perigee:   320
7979  deg
Mean anomaly:      39
3138  deg
Mean motion:   15
54626116  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             515
Checksum:              310


Coasting Arc #15 (Orbit 529)
---------------------------------------

Vector Time (GMT): 2016/171/05:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 893042
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1060206
46                 A    =         6777703
88  meter
 Y    =       -4540968
92  meter          E    =           
0012152
 Z    =       -4929947
92                 I    =           51
90111
 XDOT =       6140
645728                 Wp   =           70
47996
 YDOT =       3948
581524  meter/sec      RA   =           47
15187  deg
 ZDOT =      -2317
151478                 TA   =          176
91593
                                          MA   =          176
90843
                                          Ha   =            220
194  n
mi
                                          Hp   =            214
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3478367
64                 X    =         1134853
58
 Y    =      -14898191
99  feet           Y    =        -4528694
90  meter
 Z    =      -16174369
81                 Z    =        -4924617
02
 XDOT =      20146
475485                 XDOT =        6107
291082
 YDOT =      12954
663793  feet/sec       YDOT =        4017
064148  meter/sec
 ZDOT =      -7602
203013                 ZDOT =       -2287
402076

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5142526
69                 X    =         1567442
13
 Y    =      -14435755
82  feet           Y    =        -4400018
37  meter
 Z    =      -16150194
37                 Z    =        -4922579
24
 XDOT =      17654
734215                 XDOT =        5381
162989
 YDOT =      14647
622501  feet/sec       YDOT =        4464
595338  meter/sec
 ZDOT =      -7473
357908                 ZDOT =       -2277
879490


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   16171
26139432  
00016717  00000-0  10270-3 0  9148
2 25544  51
6413  47
6897 0000558 339
0840  21
0290 15
54599178  5304


Satellite: ISS
Catalog Number: 25544
Epoch time:      16171
26139432   =   yrday
fracday
Element set:     914
Inclination:       51
6413  deg
RA of node:        47
6897  deg
Eccentricity:     
0000558     
Arg of perigee:   339
0840  deg
Mean anomaly:      21
0290  deg
Mean motion:   15
54599178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             530
Checksum:              306


Coasting Arc #16 (Orbit 540)
---------------------------------------

Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893042
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5685808
68                 A    =         6784459
41  meter
 Y    =       -2314762
81  meter          E    =           
0012998
 Z    =        2874791
35                 I    =           51
91140
 XDOT =       -242
071147                 Wp   =           97
99082
 YDOT =      -5740
565005  meter/sec      RA   =           43
68468  deg
 ZDOT =      -5083
198566                 TA   =           49
40510
                                          MA   =           49
29208
                                          Ha   =            220
171  n
mi
                                          Hp   =            214
034

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18654227
97                 X    =        -5673466
37
 Y    =       -7594366
19  feet           Y    =        -2378276
73  meter
 Z    =        9431730
16                 Z    =         2847200
69
 XDOT =       -794
196677                 XDOT =        -153
168680
 YDOT =     -18833
874689  feet/sec       YDOT =       -5742
774170  meter/sec
 ZDOT =     -16677
160651                 ZDOT =       -5084
159407

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15327369
40                 X    =         4671782
19
 Y    =      -13151857
17  feet           Y    =        -4008686
07  meter
 Z    =        9311957
52                 Z    =         2838284
65
 XDOT =      16095
706126                 XDOT =        4905
971227
 YDOT =       6906
094575  feet/sec       YDOT =        2104
977626  meter/sec
 ZDOT =     -16680
153001                 ZDOT =       -5084
110635


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   16171
96849461  
00016717  00000-0  10270-3 0  9156
2 25544  51
6443  44
1617 0000452 314
8773  45
2344 15
54628481  5418


Satellite: ISS
Catalog Number: 25544
Epoch time:      16171
96849461   =   yrday
fracday
Element set:     915
Inclination:       51
6443  deg
RA of node:        44
1617  deg
Eccentricity:     
0000452     
Arg of perigee:   314
8773  deg
Mean anomaly:      45
2344  deg
Mean motion:   15
54628481  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             541
Checksum:              308


Coasting Arc #17 (Orbit 555)
---------------------------------------

Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893042
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5731935
54                 A    =         6787472
21  meter
 Y    =        3439246
70  meter          E    =           
0009639
 Z    =       -1151193
94                 I    =           51
89642
 XDOT =      -1604
911963                 Wp   =           34
16336
 YDOT =       4636
751785  meter/sec      RA   =           38
72603  deg
 ZDOT =       5893
097251                 TA   =          313
38119
                                          MA   =          313
46143
                                          Ha   =            220
196  n
mi
                                          Hp   =            214
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18805562
80                 X    =         5698643
01
 Y    =       11283617
80  feet           Y    =         3503159
05  meter
 Z    =       -3776883
01                 Z    =        -1123430
01
 XDOT =      -5265
459195                 XDOT =       -1685
268089
 YDOT =      15212
440239  feet/sec       YDOT =        4618
354410  meter/sec
 ZDOT =      19334
308565                 ZDOT =        5885
106519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18457668
67                 X    =        -5625897
41
 Y    =       11881829
09  feet           Y    =         3621581
51  meter
 Z    =       -3656593
09                 Z    =        -1114529
57
 XDOT =     -10385
217690                 XDOT =       -3165
414352
 YDOT =     -10226
716381  feet/sec       YDOT =       -3117
103153  meter/sec
 ZDOT =      19298
509021                 ZDOT =        5882
185550


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16172
93271870  
00016717  00000-0  10270-3 0  9168
2 25544  51
6434  39
3522 0000647 325
6263  34
4848 15
54585007  5560


Satellite: ISS
Catalog Number: 25544
Epoch time:      16172
93271870   =   yrday
fracday
Element set:     916
Inclination:       51
6434  deg
RA of node:        39
3522  deg
Eccentricity:     
0000647     
Arg of perigee:   325
6263  deg
Mean anomaly:      34
4848  deg
Mean motion:   15
54585007  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             556
Checksum:              312
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