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

 
Date: December 28th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1552 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


There are no maneuvers



Coasting Arc #1 (Orbit 3519)
---------------------------------------

Vector Time (GMT): 2016/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5013290
50                 A    =         6785992
32  meter
 Y    =        3467167
93  meter          E    =           
0010469
 Z    =       -2978828
83                 I    =           51
71535
 XDOT =      -5006
019584                 Wp   =           42
89441
 YDOT =      -2965
360539  meter/sec      RA   =          168
02202  deg
 ZDOT =       4991
305916                 TA   =          283
09347
                                          MA   =          283
21029
                                          Ha   =            223
059  n
mi
                                          Hp   =            213
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16447803
48                 X    =        -5037218
92
 Y    =       11375222
88  feet           Y    =         3410972
47  meter
 Z    =       -9773060
48                 Z    =        -3003239
71
 XDOT =     -16423
948767                 XDOT =       -4996
733517
 YDOT =      -9728
873159  feet/sec       YDOT =       -3021
289814  meter/sec
 ZDOT =      16375
675577                 ZDOT =        4967
010365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13163698
03                 X    =        -4012295
16
 Y    =      -14984219
02  feet           Y    =        -4567189
96  meter
 Z    =       -9880732
79                 Z    =        -3011647
35
 XDOT =       6691
816782                 XDOT =        2039
665755
 YDOT =     -16569
004249  feet/sec       YDOT =       -5050
232495  meter/sec
 ZDOT =      16269
564565                 ZDOT =        4958
963279


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   16363
50616079  
00016717  00000-0  10270-3 0  9000
2 25544  51
6370 169
1620 0006791  24
4499 335
6975 15
53951907 35207


Satellite: ISS
Catalog Number: 25544
Epoch time:      16363
50616079   =   yrday
fracday
Element set:     900
Inclination:       51
6370  deg
RA of node:       169
1620  deg
Eccentricity:     
0006791     
Arg of perigee:    24
4499  deg
Mean anomaly:     335
6975  deg
Mean motion:   15
53951907  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3520
Checksum:              321


Coasting Arc #2 (Orbit 3535)
---------------------------------------

Vector Time (GMT): 2016/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5913342
92                 A    =         6788829
78  meter
 Y    =       -2996025
33  meter          E    =           
0015228
 Z    =        1449483
11                 I    =           51
75608
 XDOT =       3335
166659                 Wp   =           92
15607
 YDOT =       3755
635945  meter/sec      RA   =          163
05450  deg
 ZDOT =      -5791
493860                 TA   =           72
06163
                                          MA   =           71
89567
                                          Ha   =            223
116  n
mi
                                          Hp   =            213
439

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19400731
37                 X    =         5939364
87
 Y    =       -9829479
42  feet           Y    =        -2929753
00  meter
 Z    =        4755522
01                 Z    =         1478271
21
 XDOT =      10942
147831                 XDOT =        3321
054546
 YDOT =      12321
640239  feet/sec       YDOT =        3792
853709  meter/sec
 ZDOT =     -19000
964108                 ZDOT =       -5775
326533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12277967
94                 X    =         3742324
63
 Y    =       17917484
76  feet           Y    =         5461249
36  meter
 Z    =        4882343
29                 Z    =         1488138
23
 XDOT =      -9460
229478                 XDOT =       -2883
477945
 YDOT =      11686
300604  feet/sec       YDOT =        3561
984424  meter/sec
 ZDOT =     -18930
635334                 ZDOT =       -5770
057650


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   16364
53510916  
00016717  00000-0  10270-3 0  9018
2 25544  51
6367 164
0338 0006837  26
2261 333
9237 15
53977884 35362


Satellite: ISS
Catalog Number: 25544
Epoch time:      16364
53510916   =   yrday
fracday
Element set:     901
Inclination:       51
6367  deg
RA of node:       164
0338  deg
Eccentricity:     
0006837     
Arg of perigee:    26
2261  deg
Mean anomaly:     333
9237  deg
Mean motion:   15
53977884  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3536
Checksum:              324


Coasting Arc #3 (Orbit 3551)
---------------------------------------

Vector Time (GMT): 2016/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6338226
42                 A    =         6789780
79  meter
 Y    =        2400712
97  meter          E    =           
0018990
 Z    =         174475
87                 I    =           51
79202
 XDOT =      -1527
812739                 Wp   =           41
88900
 YDOT =      -4498
003539  meter/sec      RA   =          158
09386  deg
 ZDOT =       6025
853793                 TA   =          319
98780
                                          MA   =          320
12756
                                          Ha   =            223
206  n
mi
                                          Hp   =            213
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20794706
09                 X    =        -6365448
25
 Y    =        7876354
89  feet           Y    =         2329682
44  meter
 Z    =         572427
38                 Z    =          143620
92
 XDOT =      -5012
508986                 XDOT =       -1506
671916
 YDOT =     -14757
229459  feet/sec       YDOT =       -4514
970934  meter/sec
 ZDOT =      19769
861526                 ZDOT =        6018
483093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10864355
50                 X    =        -3311455
56
 Y    =      -19405143
39  feet           Y    =        -5914687
70  meter
 Z    =         436612
56                 Z    =          133079
51
 XDOT =      12418
292543                 XDOT =        3785
095567
 YDOT =      -6473
338452  feet/sec       YDOT =       -1973
073560  meter/sec
 ZDOT =      19738
252314                 ZDOT =        6016
219305


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   16365
56405553  
00016717  00000-0  10270-3 0  9023
2 25544  51
6389 158
9056 0006782  31
9109 328
2453 15
53972833 35522


Satellite: ISS
Catalog Number: 25544
Epoch time:      16365
56405553   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:       158
9056  deg
Eccentricity:     
0006782     
Arg of perigee:    31
9109  deg
Mean anomaly:     328
2453  deg
Mean motion:   15
53972833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3552
Checksum:              329


Coasting Arc #4 (Orbit 3566)
---------------------------------------

Vector Time (GMT): 2016/366/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930840
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6340378
76                 A    =         6788365
32  meter
 Y    =       -1594804
20  meter          E    =           
0008606
 Z    =       -1834157
42                 I    =           51
81677
 XDOT =       -332
913261                 Wp   =           90
89362
 YDOT =       5155
396606  meter/sec      RA   =          153
13500  deg
 ZDOT =      -5656
509880                 TA   =          109
20525
                                          MA   =          109
11211
                                          Ha   =            223
329  n
mi
                                          Hp   =            213
198

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20801767
59                 X    =         6366650
43
 Y    =       -5232297
25  feet           Y    =        -1523754
78  meter
 Z    =       -6017576
84                 Z    =        -1803294
31
 XDOT =      -1092
235109                 XDOT =        -363
061089
 YDOT =      16914
030858  feet/sec       YDOT =        5151
505644  meter/sec
 ZDOT =     -18558
103280                 ZDOT =       -5658
199861

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8596134
70                 X    =         2620101
86
 Y    =       19692946
52  feet           Y    =         6002410
10  meter
 Z    =       -5881838
64                 Z    =        -1792784
42
 XDOT =     -15405
137572                 XDOT =       -4695
485932
 YDOT =       1202
227149  feet/sec       YDOT =         366
438835  meter/sec
 ZDOT =     -18566
370784                 ZDOT =       -5659
029815


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   16366
52868773  
00016717  00000-0  10270-3 0  9038
2 25544  51
6386 154
0979 0006977  35
1737 324
9874 15
53989243 35678


Satellite: ISS
Catalog Number: 25544
Epoch time:      16366
52868773   =   yrday
fracday
Element set:     903
Inclination:       51
6386  deg
RA of node:       154
0979  deg
Eccentricity:     
0006977     
Arg of perigee:    35
1737  deg
Mean anomaly:     324
9874  deg
Mean motion:   15
53989243  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3567
Checksum:              370
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