Date:
December 19th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 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 1733)
---------------------------------------
Vector Time (GMT): 2008/352/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2702899
64 A = 6731717
98 meter
Y = -4615194
91 meter E =
0017661
Z = 4073815
37 I = 51
76287
XDOT = 6658
576653 Wp = 85
08259
YDOT = 491
845578 meter/sec RA = 157
23871 deg
ZDOT = -3844
929593 TA = 44
43402
MA = 44
29246
Ha = 196
420 n
mi
Hp = 184
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8867780
98 X = 2734516
87
Y = -15141715
59 feet Y = -4584793
15 meter
Z = 13365535
98 Z = 4087022
32
XDOT = 21845
723926 XDOT = 6671
259746
YDOT = 1613
666594 feet/sec YDOT = 566
376937 meter/sec
ZDOT = -12614
598403 ZDOT = -3812
551541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10680705
02 X = -3255478
89
Y = 13873241
54 feet Y = 4228564
02 meter
Z = 13416495
50 Z = 4089347
83
XDOT = -20511
760301 XDOT = -6251
984540
YDOT = -3664
364779 feet/sec YDOT = -1116
898385 meter/sec
ZDOT = -12488
723149 ZDOT = -3806
562816
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 08352
28270092
00010596 00000-0 82463-4 0 9008
2 25544 51
6407 158
0509 0007387 96
9632 263
2370 15
71610617 17346
Satellite: ISS
Catalog Number: 25544
Epoch time: 08352
28270092 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 158
0509 deg
Eccentricity:
0007387
Arg of perigee: 96
9632 deg
Mean anomaly: 263
2370 deg
Mean motion: 15
71610617 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1734
Checksum: 304
Coasting Arc #2 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2008/353/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6104488
20 A = 6735890
40 meter
Y = 810507
42 meter E =
0020668
Z = 2709921
66 I = 51
80396
XDOT = 1594
297800 Wp = 86
17710
YDOT = -5460
400197 meter/sec RA = 152
17915 deg
ZDOT = 5192
059681 TA = 304
65440
MA = 304
84905
Ha = 196
500 n
mi
Hp = 184
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20027848
44 X = -6126262
01
Y = 2659145
09 feet Y = 742121
53 meter
Z = 8890819
11 Z = 2680213
30
XDOT = 5230
635827 XDOT = 1630
016367
YDOT = -17914
698809 feet/sec YDOT = -5442
372563 meter/sec
ZDOT = 17034
316540 ZDOT = 5199
891062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20250427
25 X = 6172330
23
Y = -380442
14 feet Y = -115958
76 meter
Z = 8775413
96 Z = 2674746
17
XDOT = -7145
691349 XDOT = -2178
006723
YDOT = 15745
619311 feet/sec YDOT = 4799
264766 meter/sec
ZDOT = 17064
318855 ZDOT = 5201
204387
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 08353
30007649
00010596 00000-0 82463-4 0 9019
2 25544 51
6414 152
8444 0007345 100
1913 260
0078 15
71609599 17503
Satellite: ISS
Catalog Number: 25544
Epoch time: 08353
30007649 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 152
8444 deg
Eccentricity:
0007345
Arg of perigee: 100
1913 deg
Mean anomaly: 260
0078 deg
Mean motion: 15
71609599 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1750
Checksum: 292
Coasting Arc #3 (Orbit 1764)
---------------------------------------
Vector Time (GMT): 2008/354/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -81311
75 A = 6728565
16 meter
Y = 4639194
14 meter E =
0019489
Z = -4890836
09 I = 51
80555
XDOT = -6943
285720 Wp = 105
91126
YDOT = 2324
887522 meter/sec RA = 147
03250 deg
ZDOT = 2323
117118 TA = 186
70658
MA = 186
73270
Ha = 196
319 n
mi
Hp = 184
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -266770
84 X = -109423
10
Y = 15220453
22 feet Y = 4638128
08 meter
Z = -16046050
16 Z = -4891299
01
XDOT = -22779
808794 XDOT = -6980
052254
YDOT = 7627
583732 feet/sec YDOT = 2247
037923 meter/sec
ZDOT = 7621
775320 ZDOT = 2289
297454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1627818
71 X = 496159
14
Y = -15133990
27 feet Y = -4612840
24 meter
Z = -16047480
59 Z = -4891272
08
XDOT = 22344
050750 XDOT = 6810
466669
YDOT = -5530
893463 feet/sec YDOT = -1685
816328 meter/sec
ZDOT = 7490
501089 ZDOT = 2283
104732
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 08354
25385702
00010596 00000-0 82463-4 0 9024
2 25544 51
6417 147
9635 0007192 103
7353 256
4609 15
71640938 17657
Satellite: ISS
Catalog Number: 25544
Epoch time: 08354
25385702 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 147
9635 deg
Eccentricity:
0007192
Arg of perigee: 103
7353 deg
Mean anomaly: 256
4609 deg
Mean motion: 15
71640938 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1765
Checksum: 321
Coasting Arc #4 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2008/355/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5776910
10 A = 6738246
11 meter
Y = -3195253
80 meter E =
0015431
Z = -1328861
86 I = 51
86174
XDOT = 1323
729525 Wp = 127
90107
YDOT = 4808
046097 meter/sec RA = 141
95897 deg
ZDOT = -5861
577256 TA = 66
62929
MA = 66
46705
Ha = 196
368 n
mi
Hp = 184
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18953117
12 X = 5818666
00
Y = -10483116
16 feet Y = -3130419
47 meter
Z = -4359783
01 Z = -1300696
32
XDOT = 4342
944636 XDOT = 1298
341419
YDOT = 15774
429451 feet/sec YDOT = 4822
707345 meter/sec
ZDOT = -19230
896508 ZDOT = -5855
207807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19741399
96 X = -6017178
71
Y = 8962927
47 feet Y = 2731900
29 meter
Z = -4250545
79 Z = -1295566
36
XDOT = -2549
448426 XDOT = -777
071880
YDOT = -14635
278123 feet/sec YDOT = -4460
832772 meter/sec
ZDOT = -19205
757886 ZDOT = -5853
915004
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 08355
27121593
00010596 00000-0 82463-4 0 9034
2 25544 51
6417 142
7570 0007160 108
7445 251
4494 15
71613016 17812
Satellite: ISS
Catalog Number: 25544
Epoch time: 08355
27121593 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 142
7570 deg
Eccentricity:
0007160
Arg of perigee: 108
7445 deg
Mean anomaly: 251
4494 deg
Mean motion: 15
71613016 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1781
Checksum: 296
Coasting Arc #5 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2008/356/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2303678
08 A = 6726802
35 meter
Y = -3499270
93 meter E =
0009310
Z = 5254891
72 I = 51
84633
XDOT = 5934
149916 Wp = 98
30511
YDOT = -4872
162338 meter/sec RA = 136
83860 deg
ZDOT = -643
306132 TA = 357
78781
MA = 357
79192
Ha = 196
254 n
mi
Hp = 184
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7557998
95 X = -2289904
97
Y = -11480547
66 feet Y = -3524955
48 meter
Z = 17240458
39 Z = 5243733
48
XDOT = 19468
995789 XDOT = 5991
315284
YDOT = -15984
784574 feet/sec YDOT = -4805
483548 meter/sec
ZDOT = -2110
584424 ZDOT = -614
339399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6939586
41 X = 2115185
94
Y = 11927768
19 feet Y = 3635583
75 meter
Z = 17196808
28 Z = 5241587
16
XDOT = -19553
451849 XDOT = -5959
892124
YDOT = 14255
651964 feet/sec YDOT = 4345
122719 meter/sec
ZDOT = -1998
350767 ZDOT = -609
097314
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 08356
28856375
00010596 00000-0 82463-4 0 9040
2 25544 51
6416 137
5504 0007065 111
0159 249
1759 15
71689550 17974
Satellite: ISS
Catalog Number: 25544
Epoch time: 08356
28856375 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 137
5504 deg
Eccentricity:
0007065
Arg of perigee: 111
0159 deg
Mean anomaly: 249
1759 deg
Mean motion: 15
71689550 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1797
Checksum: 334
Coasting Arc #6 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2008/357/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4357241
35 A = 6738718
37 meter
Y = 5131726
72 meter E =
0015546
Z = -210751
78 I = 51
90672
XDOT = -3735
838025 Wp = 68
89948
YDOT = -2938
352043 meter/sec RA = 131
74012 deg
ZDOT = 6051
448777 TA = 288
82191
MA = 288
99046
Ha = 196
114 n
mi
Hp = 184
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14295411
25 X = -4413277
51
Y = 16836373
76 feet Y = 5082688
23 meter
Z = -691442
83 Z = -232055
00
XDOT = -12256
686433 XDOT = -3732
100359
YDOT = -9640
262607 feet/sec YDOT = -2980
108127 meter/sec
ZDOT = 19853
834571 ZDOT = 6033
308647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15019240
79 X = 4577864
59
Y = -16190240
17 feet Y = -4934785
20 meter
Z = -773877
63 Z = -235877
90
XDOT = 10753
292914 XDOT = 3277
603680
YDOT = 9080
599857 feet/sec YDOT = 2767
766836 meter/sec
ZDOT = 19783
083545 ZDOT = 6029
883864
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 08357
24232133
00010596 00000-0 82463-4 0 9058
2 25544 51
6412 132
6690 0007029 114
2543 245
9354 15
71693752 18126
Satellite: ISS
Catalog Number: 25544
Epoch time: 08357
24232133 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 132
6690 deg
Eccentricity:
0007029
Arg of perigee: 114
2543 deg
Mean anomaly: 245
9354 deg
Mean motion: 15
71693752 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1812
Checksum: 294
Coasting Arc #7 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2008/358/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3998109
50 A = 6727055
67 meter
Y = 1485801
20 meter E =
0020423
Z = -5219263
64 I = 51
88543
XDOT = -3836
877151 Wp = 93
26054
YDOT = 6568
356113 meter/sec RA = 126
65067 deg
ZDOT = -1074
033667 TA = 166
53132
MA = 166
47673
Ha = 196
047 n
mi
Hp = 185
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13117157
14 X = 4006552
35
Y = 4874675
86 feet Y = 1530558
27 meter
Z = -17123568
39 Z = -5199819
94
XDOT = -12588
179628 XDOT = -3904
822910
YDOT = 21549
724779 feet/sec YDOT = 6525
070167 meter/sec
ZDOT = -3523
732503 ZDOT = -1092
837574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13079700
49 X = -3986692
71
Y = -5227900
02 feet Y = -1593463
93 meter
Z = -17047855
20 Z = -5196186
26
XDOT = 12761
094993 XDOT = 3889
581754
YDOT = -20250
345929 feet/sec YDOT = -6172
305439 meter/sec
ZDOT = -3596
357616 ZDOT = -1096
169801
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 08358
25965299
00010596 00000-0 82463-4 0 9067
2 25544 51
6405 127
4615 0006920 117
4551 242
7316 15
71704113 18284
Satellite: ISS
Catalog Number: 25544
Epoch time: 08358
25965299 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 127
4615 deg
Eccentricity:
0006920
Arg of perigee: 117
4551 deg
Mean anomaly: 242
7316 deg
Mean motion: 15
71704113 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1828
Checksum: 311
Coasting Arc #8 (Orbit 1843)
---------------------------------------
Vector Time (GMT): 2008/359/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2234738
60 A = 6737522
17 meter
Y = -6124938
38 meter E =
0021061
Z = 1657574
11 I = 51
93781
XDOT = 5109
167563 Wp = 117
80453
YDOT = 293
578232 meter/sec RA = 121
52775 deg
ZDOT = -5757
728221 TA = 43
95862
MA = 43
79129
Ha = 196
043 n
mi
Hp = 185
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7331819
56 X = 2295010
32
Y = -20094942
18 feet Y = -6099611
49 meter
Z = 5438235
28 Z = 1668576
05
XDOT = 16762
360770 XDOT = 5133
475202
YDOT = 963
183177 feet/sec YDOT = 350
848662 meter/sec
ZDOT = -18890
184451 ZDOT = -5732
848611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7494512
02 X = -2284327
26
Y = 20023294
29 feet Y = 6103100
10 meter
Z = 5480570
92 Z = 1670478
02
XDOT = -15400
567166 XDOT = -4694
092872
YDOT = -579
668269 feet/sec YDOT = -176
682888 meter/sec
ZDOT = -18793
414453 ZDOT = -5728
232725
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 08359
27697699
00010596 00000-0 82463-4 0 9077
2 25544 51
6411 122
2553 0006986 120
9344 239
2505 15
71701375 18442
Satellite: ISS
Catalog Number: 25544
Epoch time: 08359
27697699 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 122
2553 deg
Eccentricity:
0006986
Arg of perigee: 120
9344 deg
Mean anomaly: 239
2505 deg
Mean motion: 15
71701375 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1844
Checksum: 329
Coasting Arc #9 (Orbit 1859)
---------------------------------------
Vector Time (GMT): 2008/360/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4660682
12 A = 6729150
51 meter
Y = 1040945
06 meter E =
0014622
Z = 4733370
64 I = 51
92310
XDOT = 1173
389135 Wp = 120
97598
YDOT = -7115
157904 meter/sec RA = 116
46538 deg
ZDOT = 2706
617016 TA = 302
44067
MA = 302
58199
Ha = 196
125 n
mi
Hp = 185
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15290951
84 X = -4694969
70
Y = 3415174
07 feet Y = 988634
15 meter
Z = 15529431
22 Z = 4710645
83
XDOT = 3849
701886 XDOT = 1239
716479
YDOT = -23343
693912 feet/sec YDOT = -7101
665964 meter/sec
ZDOT = 8879
977085 ZDOT = 2712
477340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15353941
66 X = 4679881
42
Y = -3530995
48 feet Y = -1076247
42 meter
Z = 15441126
99 Z = 4706455
51
XDOT = -3880
240519 XDOT = -1182
697310
YDOT = 22251
886951 feet/sec YDOT = 6782
375143 meter/sec
ZDOT = 8902
258751 ZDOT = 2713
408467
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 08360
29429210
00010596 00000-0 82463-4 0 9084
2 25544 51
6404 117
0479 0006900 124
1735 236
0082 15
71683939 18607
Satellite: ISS
Catalog Number: 25544
Epoch time: 08360
29429210 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 117
0479 deg
Eccentricity:
0006900
Arg of perigee: 124
1735 deg
Mean anomaly: 236
0082 deg
Mean motion: 15
71683939 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1860
Checksum: 301
Coasting Arc #10 (Orbit 1874)
---------------------------------------
Vector Time (GMT): 2008/361/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 178191
64 A = 6734707
33 meter
Y = 6026657
09 meter E =
0009966
Z = -3012338
90 I = 51
95380
XDOT = -5220
260900 Wp = 106
42139
YDOT = 2641
433479 meter/sec RA = 111
32273 deg
ZDOT = 4986
599841 TA = 219
00027
MA = 219
07218
Ha = 195
844 n
mi
Hp = 185
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 584618
25 X = 125420
73
Y = 19772497
00 feet Y = 6028355
17 meter
Z = -9883001
64 Z = -3011600
43
XDOT = -17126
840223 XDOT = -5273
633862
YDOT = 8666
120338 feet/sec YDOT = 2582
758252 meter/sec
ZDOT = 16360
235700 ZDOT = 4961
110598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1130170
16 X = -344475
87
Y = -19750475
60 feet Y = -6019944
96 meter
Z = -9879704
78 Z = -3011334
02
XDOT = 15560
960257 XDOT = 4742
980686
YDOT = -9007
029905 feet/sec YDOT = -2745
342715 meter/sec
ZDOT = 16261
280683 ZDOT = 4956
438352
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 08361
24801498
00010596 00000-0 82463-4 0 9093
2 25544 51
6399 112
1659 0006810 128
9804 231
1966 15
71731691 18757
Satellite: ISS
Catalog Number: 25544
Epoch time: 08361
24801498 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 112
1659 deg
Eccentricity:
0006810
Arg of perigee: 128
9804 deg
Mean anomaly: 231
1966 deg
Mean motion: 15
71731691 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1875
Checksum: 330
Coasting Arc #11 (Orbit 1890)
---------------------------------------
Vector Time (GMT): 2008/362/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4217616
99 A = 6732028
65 meter
Y = -3494336
91 meter E =
0011716
Z = -3921895
60 I = 51
95374
XDOT = 1474
837176 Wp = 103
39377
YDOT = 6347
544651 meter/sec RA = 106
27630 deg
ZDOT = -4082
297122 TA = 124
27593
MA = 124
16494
Ha = 195
833 n
mi
Hp = 185
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13837326
07 X = 4275429
55
Y = -11464359
93 feet Y = -3446849
18 meter
Z = -12867111
55 Z = -3901266
65
XDOT = 4838
704645 XDOT = 1423
579254
YDOT = 20825
277726 feet/sec YDOT = 6363
751210 meter/sec
ZDOT = -13393
363262 ZDOT = -4075
255848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13418377
96 X = -4089921
60
Y = 12037553
02 feet Y = 3669046
16 meter
Z = -12787108
79 Z = -3897510
76
XDOT = -4906
545072 XDOT = -1495
514938
YDOT = -19622
279518 feet/sec YDOT = -5980
870797 meter/sec
ZDOT = -13365
531662 ZDOT = -4073
814051
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 08362
26531255
00010596 00000-0 82463-4 0 9109
2 25544 51
6393 106
9592 0006811 132
2506 227
9234 15
71741407 18911
Satellite: ISS
Catalog Number: 25544
Epoch time: 08362
26531255 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 106
9592 deg
Eccentricity:
0006811
Arg of perigee: 132
2506 deg
Mean anomaly: 227
9234 deg
Mean motion: 15
71741407 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1891
Checksum: 300
Coasting Arc #12 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2008/363/05:48:17
221
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2300320
72 A = 6731353
40 meter
Y = -4826265
17 meter E =
0015163
Z = 4075322
25 I = 51
95956
XDOT = 4116
836026 Wp = 99
32485
YDOT = -5238
567588 meter/sec RA = 101
12904 deg
ZDOT = -3870
379788 TA = 30
34588
MA = 30
25819
Ha = 195
724 n
mi
Hp = 185
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7546983
98 X = -2265978
68
Y = -15834203
31 feet Y = -4851797
32 meter
Z = 13370479
82 Z = 4064230
03
XDOT = 13506
679875 XDOT = 4193
910027
YDOT = -17186
901537 feet/sec YDOT = -5192
099188 meter/sec
ZDOT = -12698
096418 ZDOT = -3850
193976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8546259
01 X = 2604899
75
Y = 15355824
96 feet Y = 4680455
45 meter
Z = 13326994
75 Z = 4062068
00
XDOT = -11420
351566 XDOT = -3480
923157
YDOT = 17336
322836 feet/sec YDOT = 5284
111200 meter/sec
ZDOT = -12619
927059 ZDOT = -3846
553768
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 08363
28260039
00010596 00000-0 82463-4 0 9112
2 25544 51
6400 101
7520 0006693 136
7760 223
3928 15
71770978 19076
Satellite: ISS
Catalog Number: 25544
Epoch time: 08363
28260039 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 101
7520 deg
Eccentricity:
0006693
Arg of perigee: 136
7760 deg
Mean anomaly: 223
3928 deg
Mean motion: 15
71770978 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1907
Checksum: 308
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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