Date:
December 28th 2010
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 1388)
---------------------------------------
Vector Time (GMT): 2010/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5831227
12 A = 6734914
68 meter
Y = -2467249
36 meter E =
0018853
Z = 2269888
23 I = 51
44100
XDOT = 184
330378 Wp = 72
83574
YDOT = 5460
423720 meter/sec RA = 320
46182 deg
ZDOT = 5430
088301 TA = 312
73084
MA = 312
88939
Ha = 194
511 n
mi
Hp = 184
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19131322
59 X = 5847356
31
Y = -8094650
12 feet Y = -2401951
01 meter
Z = 7447139
88 Z = 2298255
26
XDOT = 604
758457 XDOT = 96
878911
YDOT = 17914
775984 feet/sec YDOT = 5461
995723 meter/sec
ZDOT = 17815
250331 ZDOT = 5430
771680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9753249
82 X = 2972790
54
Y = 18294563
23 feet Y = 5576182
87 meter
Z = 7561337
92 Z = 2304695
80
XDOT = -16466
846381 XDOT = -5019
094777
YDOT = 1372
398799 feet/sec YDOT = 418
307154 meter/sec
ZDOT = 17817
809236 ZDOT = 5430
868255
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 10361
55899264
00016717 00000-0 10270-3 0 9006
2 25544 51
6445 320
7104 0004881 74
6861 285
4840 15
72231701 13898
Satellite: ISS
Catalog Number: 25544
Epoch time: 10361
55899264 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 320
7104 deg
Eccentricity:
0004881
Arg of perigee: 74
6861 deg
Mean anomaly: 285
4840 deg
Mean motion: 15
72231701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1389
Checksum: 308
Coasting Arc #2 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2010/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1193489
23 A = 6726572
77 meter
Y = -4396868
86 meter E =
0017329
Z = -4964178
06 I = 51
38992
XDOT = 6273
869960 Wp = 96
86563
YDOT = -3960
205449 meter/sec RA = 315
28713 deg
ZDOT = 2003
214567 TA = 192
59937
MA = 192
64274
Ha = 194
608 n
mi
Hp = 184
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3915647
09 X = -1120118
84
Y = -14425422
77 feet Y = -4409804
60 meter
Z = -16286673
41 Z = -4969798
11
XDOT = 20583
562861 XDOT = 6307
956174
YDOT = -12992
800029 feet/sec YDOT = -3889
856804 meter/sec
ZDOT = 6572
226269 ZDOT = 2033
775558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13941642
46 X = 4249412
62
Y = -5322005
13 feet Y = -1622147
16 meter
Z = -16309129
71 Z = -4971022
74
XDOT = 14703
208325 XDOT = 4481
537897
YDOT = 18038
958874 feet/sec YDOT = 5498
274665 meter/sec
ZDOT = 6695
297741 ZDOT = 2040
726752
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 10362
51241867
00016717 00000-0 10270-3 0 9014
2 25544 51
6446 315
8273 0004922 76
0457 284
1252 15
72215135 14048
Satellite: ISS
Catalog Number: 25544
Epoch time: 10362
51241867 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 315
8273 deg
Eccentricity:
0004922
Arg of perigee: 76
0457 deg
Mean anomaly: 284
1252 deg
Mean motion: 15
72215135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 286
Coasting Arc #3 (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 = -4976604
50 A = 6736440
88 meter
Y = 4364939
14 meter E =
0012092
Z = -1235878
89 I = 51
40340
XDOT = -2406
090395 Wp = 120
99269
YDOT = -4385
238434 meter/sec RA = 310
17600 deg
ZDOT = -5847
581603 TA = 72
58855
MA = 72
45638
Ha = 194
529 n
mi
Hp = 184
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16327442
59 X = -5019040
50
Y = 14320666
46 feet Y = 4309050
58 meter
Z = -4054720
77 Z = -1260158
00
XDOT = -7893
997358 XDOT = -2328
468443
YDOT = -14387
265203 feet/sec YDOT = -4411
710271 meter/sec
ZDOT = -19184
979011 ZDOT = -5859
082258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16213998
47 X = -4942026
73
Y = -14421176
65 feet Y = -4395574
64 meter
Z = -4152535
06 Z = -1265692
69
XDOT = 12272
299636 XDOT = 3740
596929
YDOT = -8305
047739 feet/sec YDOT = -2531
378551 meter/sec
ZDOT = -19231
091660 ZDOT = -5861
636738
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
52938767
00016717 00000-0 10270-3 0 9029
2 25544 51
6451 310
6185 0004913 79
4072 280
7643 15
72257237 14202
Satellite: ISS
Catalog Number: 25544
Epoch time: 10363
52938767 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 310
6185 deg
Eccentricity:
0004913
Arg of perigee: 79
4072 deg
Mean anomaly: 280
7643 deg
Mean motion: 15
72257237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1420
Checksum: 305
Coasting Arc #4 (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 = 2905976
32 A = 6725186
96 meter
Y = 3105116
76 meter E =
0007957
Z = 5203449
02 I = 51
34719
XDOT = -4895
561075 Wp = 73
62750
YDOT = 5897
305262 meter/sec RA = 305
01694 deg
ZDOT = -781
940181 TA = 23
85839
MA = 23
82153
Ha = 194
409 n
mi
Hp = 184
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9534043
05 X = 2845760
86
Y = 10187390
94 feet Y = 3137275
88 meter
Z = 17071683
14 Z = 5217420
37
XDOT = -16061
552084 XDOT = -4957
343462
YDOT = 19348
114376 feet/sec YDOT = 5842
214791 meter/sec
ZDOT = -2565
420540 ZDOT = -805
872308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8768947
93 X = -2672775
33
Y = 10764200
09 feet Y = 3280928
19 meter
Z = 17127779
33 Z = 5220547
14
XDOT = -20616
888643 XDOT = -6284
027659
YDOT = -12543
142189 feet/sec YDOT = -3823
149739 meter/sec
ZDOT = -2661
892149 ZDOT = -811
344727
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
54633864
00016717 00000-0 10270-3 0 9033
2 25544 51
6453 305
4105 0004878 83
0497 277
1220 15
72289143 14369
Satellite: ISS
Catalog Number: 25544
Epoch time: 10364
54633864 = yrday
fracday
Element set: 903
Inclination: 51
6453 deg
RA of node: 305
4105 deg
Eccentricity:
0004878
Arg of perigee: 83
0497 deg
Mean anomaly: 277
1220 deg
Mean motion: 15
72289143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1436
Checksum: 306
Coasting Arc #5 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2010/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828620
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3442489
55 A = 6736982
90 meter
Y = -5782304
85 meter E =
0016562
Z = 130074
62 I = 51
37036
XDOT = 4065
834216 Wp = 57
40134
YDOT = 2568
133845 meter/sec RA = 299
88235 deg
ZDOT = 6012
461105 TA = 304
01620
MA = 304
17340
Ha = 194
466 n
mi
Hp = 184
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11294257
04 X = 3506260
63
Y = -18970816
42 feet Y = -5743452
31 meter
Z = 426754
00 Z = 146952
39
XDOT = 13339
351102 XDOT = 4007
607210
YDOT = 8425
635976 feet/sec YDOT = 2613
274099 meter/sec
ZDOT = 19725
922259 ZDOT = 6032
071849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20507110
35 X = 6250567
23
Y = 8176049
76 feet Y = 2492059
97 meter
Z = 494845
82 Z = 150829
01
XDOT = -5652
057638 XDOT = -1722
747168
YDOT = 12884
225291 feet/sec YDOT = 3927
111869 meter/sec
ZDOT = 19804
725294 ZDOT = 6036
480269
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 10365
56327170
00016717 00000-0 10270-3 0 9047
2 25544 51
6452 300
2013 0004859 86
9371 273
2347 15
72310511 14520
Satellite: ISS
Catalog Number: 25544
Epoch time: 10365
56327170 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 300
2013 deg
Eccentricity:
0004859
Arg of perigee: 86
9371 deg
Mean anomaly: 273
2347 deg
Mean motion: 15
72310511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 281
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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