ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 ET - UTC (sec) : 66 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 1419)
---------------------------------------
Vector Time (GMT): 2010/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4976418
53 A = 6736419
48 meter
Y = 4365372
29 meter E =
0012046
Z = -1235118
53 I = 51
40297
XDOT = -2406
821235 Wp = 120
86628
YDOT = -4384
602184 meter/sec RA = 310
17749 deg
ZDOT = -5847
736092 TA = 72
70652
MA = 72
57476
Ha = 194
509 n
mi
Hp = 184
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16326832
46 X = -5018863
09
Y = 14322087
55 feet Y = 4309485
76 meter
Z = -4052226
16 Z = -1259396
76
XDOT = -7896
395127 XDOT = -2329
205593
YDOT = -14385
177770 feet/sec YDOT = -4411
082229 meter/sec
ZDOT = -19185
485866 ZDOT = -5859
240313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16215335
82 X = -4942434
36
Y = -14420411
39 feet Y = -4395341
39 meter
Z = -4150036
91 Z = -1264931
25
XDOT = 12269
989774 XDOT = 3739
892883
YDOT = -8307
070485 feet/sec YDOT = -2531
995084 meter/sec
ZDOT = -19231
612880 ZDOT = -5861
795606
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 10363
52938888
00016717 00000-0 10270-3 0 9001
2 25544 51
6447 310
6199 0004895 78
7936 281
3777 15
72265029 14205
Satellite: ISS
Catalog Number: 25544
Epoch time: 10363
52938888 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 310
6199 deg
Eccentricity:
0004895
Arg of perigee: 78
7936 deg
Mean anomaly: 281
3777 deg
Mean motion: 15
72265029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1420
Checksum: 340
Coasting Arc #2 (Orbit 1435)
---------------------------------------
Vector Time (GMT): 2010/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2904383
16 A = 6725166
15 meter
Y = 3107074
37 meter E =
0007952
Z = 5203168
43 I = 51
34676
XDOT = -4896
891723 Wp = 73
21338
YDOT = 5895
904036 meter/sec RA = 305
01831 deg
ZDOT = -784
067811 TA = 24
29331
MA = 24
25584
Ha = 194
390 n
mi
Hp = 184
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9528816
14 X = 2844147
29
Y = 10193813
55 feet Y = 3139215
56 meter
Z = 17070762
58 Z = 5217132
00
XDOT = -16065
917725 XDOT = -4958
648006
YDOT = 19343
517179 feet/sec YDOT = 5840
798831 meter/sec
ZDOT = -2572
400954 ZDOT = -808
006339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8776037
57 X = -2674936
25
Y = 10759928
23 feet Y = 3279626
12 meter
Z = 17126827
37 Z = 5220256
98
XDOT = -20613
252528 XDOT = -6282
919371
YDOT = -12547
549612 feet/sec YDOT = -3824
493122 meter/sec
ZDOT = -2668
898267 ZDOT = -813
480192
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 10364
54633479
00016717 00000-0 10270-3 0 9013
2 25544 51
6449 305
4119 0004861 82
4330 277
7384 15
72296902 14368
Satellite: ISS
Catalog Number: 25544
Epoch time: 10364
54633479 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 305
4119 deg
Eccentricity:
0004861
Arg of perigee: 82
4330 deg
Mean anomaly: 277
7384 deg
Mean motion: 15
72296902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1436
Checksum: 315
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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