ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 163)
---------------------------------------

Vector Time (GMT): 2014/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5933790
28                 A    =         6793174
70  meter
 Y    =        3283144
61  meter          E    =           
0017189
 Z    =         123390
32                 I    =           51
47881
 XDOT =      -2213
125170                 Wp   =          153
13566
 YDOT =       4237
137302  meter/sec      RA   =          209
78550  deg
 ZDOT =      -6000
645579                 TA   =           25
53196
                                          MA   =           25
44716
                                          Ha   =            224
091  n
mi
                                          Hp   =            216
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19467815
87                 X    =         5896036
99
 Y    =       10771471
82  feet           Y    =         3349289
01  meter
 Z    =         404823
89                 Z    =          152124
11
 XDOT =      -7260
909351                 XDOT =       -2231
192294
 YDOT =      13901
369100  feet/sec       YDOT =        4212
287904  meter/sec
 ZDOT =     -19687
157410                 ZDOT =       -6011
440298

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8307246
68                 X    =        -2532048
79
 Y    =       20637256
34  feet           Y    =         6290235
73  meter
 Z    =         526921
03                 Z    =          160605
53
 XDOT =     -13163
835305                 XDOT =       -4012
337001
 YDOT =      -4774
988678  feet/sec       YDOT =       -1455
416549  meter/sec
 ZDOT =     -19733
951762                 ZDOT =       -6014
908497


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   14363
53252078  
00016717  00000-0  10270-3 0  9006
2 25544  51
6441 210
7047 0006938 190
0957 170
0057 15
52804799  1642


Satellite: ISS
Catalog Number: 25544
Epoch time:      14363
53252078   =   yrday
fracday
Element set:     900
Inclination:       51
6441  deg
RA of node:       210
7047  deg
Eccentricity:     
0006938     
Arg of perigee:   190
0957  deg
Mean anomaly:     170
0057  deg
Mean motion:   15
52804799  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             164
Checksum:              302


Coasting Arc #2 (Orbit 179)
---------------------------------------

Vector Time (GMT): 2014/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5638517
02                 A    =         6792490
20  meter
 Y    =       -3607569
47  meter          E    =           
0009733
 Z    =        1142580
63                 I    =           51
50365
 XDOT =       3455
780212                 Wp   =           86
30366
 YDOT =      -3533
211697  meter/sec      RA   =          204
80909  deg
 ZDOT =       5855
626256                 TA   =          286
11102
                                          MA   =          286
21815
                                          Ha   =            223
881  n
mi
                                          Hp   =            216
853

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18499071
58                 X    =        -5603307
53
 Y    =      -11835857
84  feet           Y    =        -3670426
22  meter
 Z    =        3748624
13                 Z    =         1115274
95
 XDOT =      11337
861588                 XDOT =        3466
587927
 YDOT =     -11591
901893  feet/sec       YDOT =       -3494
506784  meter/sec
 ZDOT =      19211
372232                 ZDOT =        5872
439962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9136095
55                 X    =         2784681
92
 Y    =      -19992270
31  feet           Y    =        -6093643
99  meter
 Z    =        3632664
20                 Z    =         1107236
05
 XDOT =      11583
512166                 XDOT =        3530
654508
 YDOT =       8823
562472  feet/sec       YDOT =        2689
421842  meter/sec
 ZDOT =      19283
746454                 ZDOT =        5877
685919


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   14364
56220917  
00016717  00000-0  10270-3 0  9018
2 25544  51
6429 205
5803 0006934 194
7163 165
3788 15
52863109  1802


Satellite: ISS
Catalog Number: 25544
Epoch time:      14364
56220917   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:       205
5803  deg
Eccentricity:     
0006934     
Arg of perigee:   194
7163  deg
Mean anomaly:     165
3788  deg
Mean motion:   15
52863109  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             180
Checksum:              314