ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16915 4846 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 3551)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6337894
40                 A    =         6789793
45  meter
 Y    =        2401781
42  meter          E    =           
0018976
 Z    =         173116
84                 I    =           51
79227
 XDOT =      -1529
649369                 Wp   =           41
96554
 YDOT =      -4497
262105  meter/sec      RA   =          158
09349  deg
 ZDOT =       6025
902551                 TA   =          319
89662
                                          MA   =          320
03654
                                          Ha   =            223
211  n
mi
                                          Hp   =            213
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20793616
81                 X    =        -6365121
61
 Y    =        7879860
31  feet           Y    =         2330754
57  meter
 Z    =         567968
63                 Z    =          142263
49
 XDOT =      -5018
534676                 XDOT =       -1508
516938
 YDOT =     -14754
796934  feet/sec       YDOT =       -4514
250086  meter/sec
 ZDOT =      19770
021493                 ZDOT =        6018
522909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10867656
70                 X    =        -3312461
76
 Y    =      -19403519
32  feet           Y    =        -5914192
69  meter
 Z    =         432160
65                 Z    =          131722
57
 XDOT =      12415
114269                 XDOT =        3784
126829
 YDOT =      -6478
698521  feet/sec       YDOT =       -1974
707309  meter/sec
 ZDOT =      19738
372912                 ZDOT =        6016
256064


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
56405832  
00016717  00000-0  10270-3 0  9001
2 25544  51
6392 158
9052 0006765  32
1293 328
0270 15
53968521 35524


Satellite: ISS
Catalog Number: 25544
Epoch time:      16365
56405832   =   yrday
fracday
Element set:     900
Inclination:       51
6392  deg
RA of node:       158
9052  deg
Eccentricity:     
0006765     
Arg of perigee:    32
1293  deg
Mean anomaly:     328
0270  deg
Mean motion:   15
53968521  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3552
Checksum:              309


Coasting Arc #2 (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    =        6340541
05                 A    =         6788388
81  meter
 Y    =       -1597543
09  meter          E    =           
0008622
 Z    =       -1831206
29                 I    =           51
81704
 XDOT =       -328
655364                 Wp   =           91
15291
 YDOT =       5154
314558  meter/sec      RA   =          153
13468  deg
 ZDOT =      -5657
764519                 TA   =          108
91216
                                          MA   =          108
81867
                                          Ha   =            223
337  n
mi
                                          Hp   =            213
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20802300
04                 X    =         6366829
00
 Y    =       -5241283
12  feet           Y    =        -1526491
77  meter
 Z    =       -6007894
65                 Z    =        -1800342
35
 XDOT =      -1078
265631                 XDOT =        -358
785315
 YDOT =      16910
480833  feet/sec       YDOT =        5150
471311  meter/sec
 ZDOT =     -18562
219551                 ZDOT =       -5659
433773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8605074
19                 X    =         2622826
61
 Y    =       19691928
77  feet           Y    =         6002099
89  meter
 Z    =       -5872152
37                 Z    =        -1789832
04
 XDOT =     -15399
403178                 XDOT =       -4693
738089
 YDOT =       1214
794622  feet/sec       YDOT =         370
269401  meter/sec
 ZDOT =     -18570
395895                 ZDOT =       -5660
256669


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
52869397  
00016717  00000-0  10270-3 0  9019
2 25544  51
6388 154
0976 0006959  35
4002 324
7611 15
53982710 35674


Satellite: ISS
Catalog Number: 25544
Epoch time:      16366
52869397   =   yrday
fracday
Element set:     901
Inclination:       51
6388  deg
RA of node:       154
0976  deg
Eccentricity:     
0006959     
Arg of perigee:    35
4002  deg
Mean anomaly:     324
7611  deg
Mean motion:   15
53982710  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3567
Checksum:              337