ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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

There are no maneuvers



Coasting Arc #1 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2015/364/12:02:47
312
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         866044
02                 A    =         6774508
18  meter
 Y    =       -4148982
14  meter          E    =           
0009064
 Z    =        5285841
21                 I    =           51
59151
 XDOT =       7600
350195                 Wp   =          358
24357
 YDOT =        866
027825  meter/sec      RA   =          183
19313  deg
 ZDOT =       -556
650012                 TA   =           97
12232
                                          MA   =           97
01925
                                          Ha   =            220
532  n
mi
                                          Hp   =            213
355

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2841351
78                 X    =          886698
38
 Y    =      -13612146
13  feet           Y    =        -4139182
17  meter
 Z    =       17341998
72                 Z    =         5290098
23
 XDOT =      24935
532135                 XDOT =        7592
805139
 YDOT =       2841
298639  feet/sec       YDOT =         950
977799  meter/sec
 ZDOT =      -1826
279568                 ZDOT =        -519
747883

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13864132
64                 X    =         4225787
63
 Y    =         696635
07  feet           Y    =          212334
37  meter
 Z    =       17361141
88                 Z    =         5291676
05
 XDOT =        913
310706                 XDOT =         278
377103
 YDOT =      24082
182982  feet/sec       YDOT =        7340
249373  meter/sec
 ZDOT =      -1666
690233                 ZDOT =        -508
007183


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   15364
54928979  
00016717  00000-0  10270-3 0  9009
2 25544  51
6380 184
0965 0008556 340
1456  19
9363 15
55134726 18598


Satellite: ISS
Catalog Number: 25544
Epoch time:      15364
54928979   =   yrday
fracday
Element set:     900
Inclination:       51
6380  deg
RA of node:       184
0965  deg
Eccentricity:     
0008556     
Arg of perigee:   340
1456  deg
Mean anomaly:      19
9363  deg
Mean motion:   15
55134726  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              341