ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9149 32 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 1827)
---------------------------------------

Vector Time (GMT): 2015/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4446645
99                 A    =         6781499
99  meter
 Y    =       -3816597
35  meter          E    =           
0011342
 Z    =        3397993
86                 I    =           51
55159
 XDOT =       5625
101835                 Wp   =           47
59850
 YDOT =      -2442
293868  meter/sec      RA   =          193
22719  deg
 ZDOT =       4615
553647                 TA   =          352
23181
                                          MA   =          352
24936
                                          Ha   =            220
285  n
mi
                                          Hp   =            213
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14588733
57                 X    =        -4420143
27
 Y    =      -12521644
83  feet           Y    =        -3866174
73  meter
 Z    =       11148273
81                 Z    =         3376457
39
 XDOT =      18455
058513                 XDOT =        5629
573863
 YDOT =      -8012
775156  feet/sec       YDOT =       -2379
365585  meter/sec
 ZDOT =      15142
892544                 ZDOT =        4642
889509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10976221
68                 X    =         3345552
37
 Y    =      -15849289
54  feet           Y    =        -4830863
45  meter
 Z    =       11055737
15                 Z    =         3369788
68
 XDOT =       8668
402070                 XDOT =        2642
128951
 YDOT =      16654
401312  feet/sec       YDOT =        5076
261520  meter/sec
 ZDOT =      15261
617458                 ZDOT =        4651
741001


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   15362
55724360  
00016717  00000-0  10270-3 0  9006
2 25544  51
6379 194
0437 0008652 331
2741  28
7935 15
55161675 18288


Satellite: ISS
Catalog Number: 25544
Epoch time:      15362
55724360   =   yrday
fracday
Element set:     900
Inclination:       51
6379  deg
RA of node:       194
0437  deg
Eccentricity:     
0008652     
Arg of perigee:   331
2741  deg
Mean anomaly:      28
7935  deg
Mean motion:   15
55161675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1828
Checksum:              318


Coasting Arc #2 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2015/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2614554
82                 A    =         6777045
13  meter
 Y    =        4141911
12  meter          E    =           
0013149
 Z    =       -4694666
54                 I    =           51
56753
 XDOT =      -7018
642661                 Wp   =           30
44171
 YDOT =       1237
769323  meter/sec      RA   =          188
22475  deg
 ZDOT =      -2809
153802                 TA   =          211
60612
                                          MA   =          211
68515
                                          Ha   =            220
404  n
mi
                                          Hp   =            213
553

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8577935
76                 X    =         2590849
16
 Y    =       13588947
24  feet           Y    =         4171016
50  meter
 Z    =      -15402449
28                 Z    =        -4682023
13
 XDOT =     -23027
042850                 XDOT =       -7018
316487
 YDOT =       4060
922977  feet/sec       YDOT =        1159
284191  meter/sec
 ZDOT =      -9216
383864                 ZDOT =       -2843
247549

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12467920
84                 X    =        -3800222
27
 Y    =       10220182
68  feet           Y    =         3115111
68  meter
 Z    =      -15348443
86                 Z    =        -4678205
69
 XDOT =      -5998
359199                 XDOT =       -1828
299884
 YDOT =     -21418
240510  feet/sec       YDOT =       -6528
279708  meter/sec
 ZDOT =      -9364
162464                 ZDOT =       -2854
196719


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   15363
52113948  
00016717  00000-0  10270-3 0  9019
2 25544  51
6373 189
2304 0008569 336
2634  23
8122 15
55166188 18439


Satellite: ISS
Catalog Number: 25544
Epoch time:      15363
52113948   =   yrday
fracday
Element set:     901
Inclination:       51
6373  deg
RA of node:       189
2304  deg
Eccentricity:     
0008569     
Arg of perigee:   336
2634  deg
Mean anomaly:      23
8122  deg
Mean motion:   15
55166188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1843
Checksum:              312


Coasting Arc #3 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2015/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922656
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -411355
10                 A    =         6774566
75  meter
 Y    =       -4219069
05  meter          E    =           
0006830
 Z    =        5284006
88                 I    =           51
59103
 XDOT =       7649
054510                 Wp   =          358
38463
 YDOT =        -29
992674  meter/sec      RA   =          183
21137  deg
 ZDOT =        578
225387                 TA   =           86
13426
                                          MA   =           86
05617
                                          Ha   =            220
580  n
mi
                                          Hp   =            213
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1349590
22                 X    =         -389813
16
 Y    =      -13842090
05  feet           Y    =        -4223548
84  meter
 Z    =       17335980
58                 Z    =         5282060
80
 XDOT =      25095
323195                 XDOT =        7646
012646
 YDOT =        -98
401161  feet/sec       YDOT =          55
527081  meter/sec
 ZDOT =       1897
064919                 ZDOT =         615
375013

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13516078
76                 X    =         4119700
80
 Y    =       -3317717
36  feet           Y    =        -1011240
25  meter
 Z    =       17328284
39                 Z    =         5281661
08
 XDOT =       3245
122722                 XDOT =         989
113406
 YDOT =      23853
662591  feet/sec       YDOT =        7270
596358  meter/sec
 ZDOT =       2057
880111                 ZDOT =         627
241858


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
54928679  
00016717  00000-0  10270-3 0  9028
2 25544  51
6375 184
0954 0008571 340
3501  19
7321 15
55128037 18590


Satellite: ISS
Catalog Number: 25544
Epoch time:      15364
54928679   =   yrday
fracday
Element set:     902
Inclination:       51
6375  deg
RA of node:       184
0954  deg
Eccentricity:     
0008571     
Arg of perigee:   340
3501  deg
Mean anomaly:      19
7321  deg
Mean motion:   15
55128037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              322