ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
364/11:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 1211)
---------------------------------------
Vector Time (GMT): 2017/363/12:14:56
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5388107
16 A = 6789027
23 meter
Y = 4117190
90 meter E =
0011623
Z = -131479
56 I = 51
87837
XDOT = -2964
546327 Wp = 30
79588
YDOT = -3694
842794 meter/sec RA = 143
48741 deg
ZDOT = 6032
223543 TA = 327
79213
MA = 327
86306
Ha = 220
115 n
mi
Hp = 215
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17677516
92 X = -5433107
57
Y = 13507844
16 feet Y = 4056685
80 meter
Z = -431363
38 Z = -157762
33
XDOT = -9726
201859 XDOT = -2952
310913
YDOT = -12122
187643 feet/sec YDOT = -3727
926457 meter/sec
ZDOT = 19790
759654 ZDOT = 6017
852081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16633949
36 X = -5070027
76
Y = -14770003
69 feet Y = -4501897
12 meter
Z = -548864
69 Z = -167293
96
XDOT = 8938
556515 XDOT = 2724
472026
YDOT = -10776
206225 feet/sec YDOT = -3284
587657 meter/sec
ZDOT = 19727
342646 ZDOT = 6012
894039
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 17363
51069519
00016717 00000-0 10270-3 0 9003
2 25544 51
6386 144
5998 0002796 304
1420 55
9467 15
54228265 12121
Satellite: ISS
Catalog Number: 25544
Epoch time: 17363
51069519 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 144
5998 deg
Eccentricity:
0002796
Arg of perigee: 304
1420 deg
Mean anomaly: 55
9467 deg
Mean motion: 15
54228265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1212
Checksum: 318
Coasting Arc #2 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3512433
44 A = 6777341
93 meter
Y = -2417358
17 meter E =
0000703
Z = 5267380
18 I = 51
86363
XDOT = 5208
211625 Wp = 95
54724
YDOT = -5553
584426 meter/sec RA = 138
63010 deg
ZDOT = 924
100226 TA = 345
63998
MA = 345
64198
Ha = 220
269 n
mi
Hp = 215
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11523731
77 X = -3510727
21
Y = -7930965
13 feet Y = -2456627
61 meter
Z = 17281431
03 Z = 5250321
75
XDOT = 17087
308482 XDOT = 5265
437386
YDOT = -18220
421346 feet/sec YDOT = -5495
022769 meter/sec
ZDOT = 3031
824888 ZDOT = 949
538541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6994305
99 X = 2131864
47
Y = -12222192
14 feet Y = -3725324
16 meter
Z = 17205875
84 Z = 5244350
96
XDOT = 18608
855729 XDOT = 5671
979226
YDOT = 15078
470205 feet/sec YDOT = 4595
917718 meter/sec
ZDOT = 3145
795587 ZDOT = 958
838495
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 17364
53946259
00016717 00000-0 10270-3 0 9012
2 25544 51
6376 139
4703 0002915 307
9709 52
1180 15
54234994 12285
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
53946259 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 139
4703 deg
Eccentricity:
0002915
Arg of perigee: 307
9709 deg
Mean anomaly: 52
1180 deg
Mean motion: 15
54234994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 321
Coasting Arc #3 (Orbit 1242)
---------------------------------------
Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2165117
17 A = 6777355
64 meter
Y = 3704244
58 meter E =
0012084
Z = -5256703
18 I = 51
88910
XDOT = -5803
939874 Wp = 90
52974
YDOT = 4886
259391 meter/sec RA = 133
64631 deg
ZDOT = 1054
674130 TA = 189
53708
MA = 189
56004
Ha = 220
232 n
mi
Hp = 215
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7103402
78 X = 2149068
79
Y = 12153033
39 feet Y = 3728367
31 meter
Z = -17246401
50 Z = -5246224
27
XDOT = -19041
797488 XDOT = -5863
271052
YDOT = 16031
034749 feet/sec YDOT = 4821
023897 meter/sec
ZDOT = 3460
216962 ZDOT = 1026
336975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11407588
68 X = -3477033
03
Y = 8343225
72 feet Y = 2543015
20 meter
Z = -17200302
95 Z = -5242652
34
XDOT = -17168
672187 XDOT = -5233
011283
YDOT = -16615
820335 feet/sec YDOT = -5064
502038 meter/sec
ZDOT = 3333
415630 ZDOT = 1016
025084
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 17365
50393062
00016717 00000-0 10270-3 0 9029
2 25544 51
6389 134
6625 0002856 311
9875 48
1034 15
54245641 12433
Satellite: ISS
Catalog Number: 25544
Epoch time: 17365
50393062 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 134
6625 deg
Eccentricity:
0002856
Arg of perigee: 311
9875 deg
Mean anomaly: 48
1034 deg
Mean motion: 15
54245641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1243
Checksum: 306
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