Date:
December 8th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 2035)
---------------------------------------
Vector Time (GMT): 2006/340/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4053540
28 A = 6723096
59 meter
Y = 4165437
00 meter E =
0015191
Z = 3372000
18 I = 51
73736
XDOT = -5828
569715 Wp = 329
92457
YDOT = 1919
082797 meter/sec RA = 18
54988 deg
ZDOT = 4657
855503 TA = 69
80114
MA = 69
63783
Ha = 191
652 n
mi
Hp = 179
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13299016
66 X = 3990279
80
Y = 13666131
87 feet Y = 4210411
61 meter
Z = 11062992
73 Z = 3391539
55
XDOT = -19122
604053 XDOT = -5872
223189
YDOT = 6296
203402 feet/sec YDOT = 1853
659574 meter/sec
ZDOT = 15281
678161 ZDOT = 4629
434372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15955874
46 X = -4863350
54
Y = 10363633
23 feet Y = 3158835
41 meter
Z = 11136516
02 Z = 3394410
08
XDOT = -1730
786131 XDOT = -527
543613
YDOT = -18895
478390 feet/sec YDOT = -5759
341813 meter/sec
ZDOT = 15175
626893 ZDOT = 4625
531077
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 06340
56887758
00020000 00000-0 20000-3 0 9006
2 25544 51
6339 18
7254 0024040 303
6819 56
2053 15
75427092 20360
Satellite: ISS
Catalog Number: 25544
Epoch time: 06340
56887758 = yrday
fracday
Element set: 900
Inclination: 51
6339 deg
RA of node: 18
7254 deg
Eccentricity:
0024040
Arg of perigee: 303
6819 deg
Mean anomaly: 56
2053 deg
Mean motion: 15
75427092 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2036
Checksum: 288
Coasting Arc #2 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2006/341/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5294785
39 A = 6721967
13 meter
Y = -1764484
62 meter E =
0018937
Z = -3723670
17 I = 51
70757
XDOT = 4527
250946 Wp = 314
46492
YDOT = 4549
337366 meter/sec RA = 13
35742 deg
ZDOT = 4281
441917 TA =
53221
MA =
53020
Ha = 191
957 n
mi
Hp = 178
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17371343
13 X = 5332211
55
Y = -5788991
52 feet Y = -1705065
49 meter
Z = -12216765
66 Z = -3697857
42
XDOT = 14853
185517 XDOT = 4455
244611
YDOT = 14925
647525 feet/sec YDOT = 4599
560255 meter/sec
ZDOT = 14046
725448 ZDOT = 4303
261250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2641853
32 X = 805236
89
Y = 18183531
85 feet Y = 5542340
51 meter
Z = -12120442
59 Z = -3694310
90
XDOT = -15958
851520 XDOT = -4864
257943
YDOT = 11736
900544 feet/sec YDOT = 3577
407286 meter/sec
ZDOT = 14128
822147 ZDOT = 4306
464990
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 06341
52033808
00020000 00000-0 20000-3 0 9013
2 25544 51
6350 13
8282 0024062 307
3104 52
5867 15
75491009 20510
Satellite: ISS
Catalog Number: 25544
Epoch time: 06341
52033808 = yrday
fracday
Element set: 901
Inclination: 51
6350 deg
RA of node: 13
8282 deg
Eccentricity:
0024062
Arg of perigee: 307
3104 deg
Mean anomaly: 52
5867 deg
Mean motion: 15
75491009 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2051
Checksum: 255
Coasting Arc #3 (Orbit 2066)
---------------------------------------
Vector Time (GMT): 2006/342/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3778403
69 A = 6720588
91 meter
Y = -3794988
63 meter E =
0021374
Z = -4063961
22 I = 51
67532
XDOT = 6317
541692 Wp = 328
78501
YDOT = -2149
212070 meter/sec RA = 8
26572 deg
ZDOT = -3839
729123 TA = 261
61989
MA = 261
86226
Ha = 192
047 n
mi
Hp = 178
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12396337
58 X = -3715944
81
Y = -12450750
09 feet Y = -3836890
99 meter
Z = -13333206
11 Z = -4082165
56
XDOT = 20726
842820 XDOT = 6359
757642
YDOT = -7051
220703 feet/sec YDOT = -2078
329182 meter/sec
ZDOT = -12597
536494 ZDOT = -3808
936314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14244948
57 X = 4341860
32
Y = -10195119
20 feet Y = -3107472
33 meter
Z = -13401706
35 Z = -4084840
10
XDOT = 2925
390813 XDOT = 891
659120
YDOT = 20611
722655 feet/sec YDOT = 6282
453065 meter/sec
ZDOT = -12482
628700 ZDOT = -3804
705228
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 06342
53520791
00020000 00000-0 20000-3 0 9028
2 25544 51
6348 8
6041 0024056 311
3017 48
6076 15
75523049 20678
Satellite: ISS
Catalog Number: 25544
Epoch time: 06342
53520791 = yrday
fracday
Element set: 902
Inclination: 51
6348 deg
RA of node: 8
6041 deg
Eccentricity:
0024056
Arg of perigee: 311
3017 deg
Mean anomaly: 48
6076 deg
Mean motion: 15
75523049 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2067
Checksum: 268
Coasting Arc #4 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2006/343/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5724726
69 A = 6724080
76 meter
Y = 2007928
03 meter E =
0015593
Z = 2922639
40 I = 51
65777
XDOT = -4038
856116 Wp = 346
09293
YDOT = -4193
504362 meter/sec RA = 3
07022 deg
ZDOT = -5020
753381 TA = 160
30884
MA = 160
24856
Ha = 192
298 n
mi
Hp = 178
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18781911
72 X = -5760951
77
Y = 6587690
39 feet Y = 1943708
03 meter
Z = 9588711
94 Z = 2894741
02
XDOT = -13250
840274 XDOT = -3967
273737
YDOT = -13758
216410 feet/sec YDOT = -4238
268196 meter/sec
ZDOT = -16472
287994 ZDOT = -5040
200775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3859118
91 X = -1176259
44
Y = -19576788
91 feet Y = -5967005
26 meter
Z = 9484608
90 Z = 2890908
79
XDOT = 14052
555087 XDOT = 4283
218790
YDOT = -10801
115937 feet/sec YDOT = -3292
180137 meter/sec
ZDOT = -16545
486447 ZDOT = -5043
064269
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 06343
55005482
00020000 00000-0 20000-3 0 9037
2 25544 51
6337 3
3793 0024077 315
4702 44
4527 15
75570795 20834
Satellite: ISS
Catalog Number: 25544
Epoch time: 06343
55005482 = yrday
fracday
Element set: 903
Inclination: 51
6337 deg
RA of node: 3
3793 deg
Eccentricity:
0024077
Arg of perigee: 315
4702 deg
Mean anomaly: 44
4527 deg
Mean motion: 15
75570795 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2083
Checksum: 283
Coasting Arc #5 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2006/344/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3237790
84 A = 6718134
34 meter
Y = 3586520
02 meter E =
0016971
Z = 4668692
63 I = 51
60911
XDOT = -6738
924569 Wp = 328
68566
YDOT = 2460
738755 meter/sec RA = 357
96647 deg
ZDOT = 2801
937371 TA = 93
75605
MA = 93
56197
Ha = 192
495 n
mi
Hp = 178
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10622673
36 X = 3174765
62
Y = 11766797
97 feet Y = 3622373
89 meter
Z = 15317233
05 Z = 4684269
10
XDOT = -22109
332577 XDOT = -6779
551320
YDOT = 8073
289877 feet/sec YDOT = 2385
152894 meter/sec
ZDOT = 9192
707911 ZDOT = 2769
101330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12985329
23 X = -3957928
35
Y = 8993306
40 feet Y = 2741159
79 meter
Z = 15375890
77 Z = 4686571
51
XDOT = -4600
234770 XDOT = -1402
151558
YDOT = -22044
663001 feet/sec YDOT = -6719
213283 meter/sec
ZDOT = 9070
189823 ZDOT = 2764
593858
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 06344
56488015
00020000 00000-0 20000-3 0 9047
2 25544 51
6333 358
1538 0024024 319
4726 40
4649 15
75571643 20991
Satellite: ISS
Catalog Number: 25544
Epoch time: 06344
56488015 = yrday
fracday
Element set: 904
Inclination: 51
6333 deg
RA of node: 358
1538 deg
Eccentricity:
0024024
Arg of perigee: 319
4726 deg
Mean anomaly: 40
4649 deg
Mean motion: 15
75571643 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2099
Checksum: 300
Coasting Arc #6 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2006/345/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5985211
81 A = 6725901
89 meter
Y = -2316874
09 meter E =
0026533
Z = -1951247
23 I = 51
60805
XDOT = 3401
690959 Wp = 337
50317
YDOT = 4055
764900 meter/sec RA = 352
77824 deg
ZDOT = 5617
659315 TA =
71178
MA =
70801
Ha = 192
680 n
mi
Hp = 178
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19636521
70 X = 6020153
40
Y = -7601292
94 feet Y = -2249748
58 meter
Z = -6401729
75 Z = -1922086
41
XDOT = 11160
403408 XDOT = 3328
796434
YDOT = 13306
315290 feet/sec YDOT = 4093
396399 meter/sec
ZDOT = 18430
640798 ZDOT = 5634
008050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5448268
75 X = 1660632
31
Y = 20373268
11 feet Y = 6209772
12 meter
Z = -6292940
25 Z = -1918088
19
XDOT = -12929
495321 XDOT = -3940
910174
YDOT = 9170
461090 feet/sec YDOT = 2795
156540 meter/sec
ZDOT = 18492
242269 ZDOT = 5636
435444
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 06345
51625675
00020000 00000-0 20000-3 0 9059
2 25544 51
6340 353
2568 0023944 323
0768 36
8747 15
75643953 21145
Satellite: ISS
Catalog Number: 25544
Epoch time: 06345
51625675 = yrday
fracday
Element set: 905
Inclination: 51
6340 deg
RA of node: 353
2568 deg
Eccentricity:
0023944
Arg of perigee: 323
0768 deg
Mean anomaly: 36
8747 deg
Mean motion: 15
75643953 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2114
Checksum: 306
Coasting Arc #7 (Orbit 2129)
---------------------------------------
Vector Time (GMT): 2006/346/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2656709
99 A = 6716276
49 meter
Y = -3533440
54 meter E =
0023039
Z = -5061868
89 I = 51
54659
XDOT = 6960
084926 Wp =
27945
YDOT = -2854
413229 meter/sec RA = 347
65693 deg
ZDOT = -1637
826598 TA = 253
83103
MA = 254
08472
Ha = 192
876 n
mi
Hp = 177
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8716240
12 X = -2592411
39
Y = -11592652
68 feet Y = -3562789
41 meter
Z = -16607181
41 Z = -5074619
35
XDOT = 22834
924299 XDOT = 6999
442378
YDOT = -9364
872798 feet/sec YDOT = -2776
361496 meter/sec
ZDOT = -5373
446844 ZDOT = -1603
919033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12322436
78 X = 3755878
73
Y = -7544568
34 feet Y = -2299584
43 meter
Z = -16655268
02 Z = -5076525
69
XDOT = 6716
504025 XDOT = 2047
190427
YDOT = 22716
544876 feet/sec YDOT = 6924
002878 meter/sec
ZDOT = -5246
968700 ZDOT = -1599
276060
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 06346
53103691
00020000 00000-0 20000-3 0 9062
2 25544 51
6329 348
0318 0024044 326
9916 32
9746 15
75646310 21300
Satellite: ISS
Catalog Number: 25544
Epoch time: 06346
53103691 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 348
0318 deg
Eccentricity:
0024044
Arg of perigee: 326
9916 deg
Mean anomaly: 32
9746 deg
Mean motion: 15
75646310 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2130
Checksum: 284
Coasting Arc #8 (Orbit 2145)
---------------------------------------
Vector Time (GMT): 2006/347/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6131942
26 A = 6727012
69 meter
Y = 2651600
81 meter E =
0013138
Z = 859887
89 I = 51
55531
XDOT = -2615
490287 Wp = 356
21920
YDOT = -4119
534843 meter/sec RA = 342
47987 deg
ZDOT = -5940
339879 TA = 174
40001
MA = 174
38531
Ha = 193
123 n
mi
Hp = 177
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20117920
78 X = -6165314
30
Y = 8699477
73 feet Y = 2582843
36 meter
Z = 2821154
50 Z = 830017
86
XDOT = -8581
004877 XDOT = -2540
373382
YDOT = -13515
534261 feet/sec YDOT = -4148
362217 meter/sec
ZDOT = -19489
304064 ZDOT = -5952
863901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7207442
07 X = -2196828
34
Y = -20714260
19 feet Y = -6313706
51 meter
Z = 2709753
83 Z = 825932
97
XDOT = 12587
038178 XDOT = 3836
529237
YDOT = -6938
761170 feet/sec YDOT = -2114
934405 meter/sec
ZDOT = -19536
611015 ZDOT = -5954
759037
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 06347
54579336
00020000 00000-0 20000-3 0 9078
2 25544 51
6324 342
8062 0024158 331
1461 28
8366 15
75707681 21460
Satellite: ISS
Catalog Number: 25544
Epoch time: 06347
54579336 = yrday
fracday
Element set: 907
Inclination: 51
6324 deg
RA of node: 342
8062 deg
Eccentricity:
0024158
Arg of perigee: 331
1461 deg
Mean anomaly: 28
8366 deg
Mean motion: 15
75707681 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2146
Checksum: 300
Coasting Arc #9 (Orbit 2161)
---------------------------------------
Vector Time (GMT): 2006/348/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1907770
34 A = 6715248
54 meter
Y = 3732628
82 meter E =
0022709
Z = 5252185
73 I = 51
48829
XDOT = -7002
916278 Wp = 339
22257
YDOT = 3184
792044 meter/sec RA = 337
33269 deg
ZDOT = 301
608798 TA = 108
03152
MA = 107
78395
Ha = 193
296 n
mi
Hp = 177
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6259089
04 X = 1840375
33
Y = 12246157
56 feet Y = 3753585
28 meter
Z = 17231580
47 Z = 5261290
40
XDOT = -22975
447107 XDOT = -7039
473774
YDOT = 10448
792794 feet/sec YDOT = 3106
277113 meter/sec
ZDOT = 989
530176 ZDOT = 267
499750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12570840
43 X = -3831592
16
Y = 5470761
89 feet Y = 1667488
22 meter
Z = 17266055
46 Z = 5262693
70
XDOT = -8751
504884 XDOT = -2667
458689
YDOT = -22611
036393 feet/sec YDOT = -6891
843893 meter/sec
ZDOT = 862
338658 ZDOT = 262
840823
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 06348
56052710
00020000 00000-0 20000-3 0 9084
2 25544 51
6318 337
5803 0024129 334
8260 25
1726 15
75712604 21621
Satellite: ISS
Catalog Number: 25544
Epoch time: 06348
56052710 = yrday
fracday
Element set: 908
Inclination: 51
6318 deg
RA of node: 337
5803 deg
Eccentricity:
0024129
Arg of perigee: 334
8260 deg
Mean anomaly: 25
1726 deg
Mean motion: 15
75712604 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2162
Checksum: 277
Coasting Arc #10 (Orbit 2177)
---------------------------------------
Vector Time (GMT): 2006/349/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6040167
18 A = 6727028
26 meter
Y = -2895810
13 meter E =
0030789
Z = 324867
94 I = 51
50292
XDOT = 1817
306021 Wp = 1
39281
YDOT = 4465
173115 meter/sec RA = 332
17509 deg
ZDOT = 6031
498021 TA = 2
15581
MA = 2
14257
Ha = 193
277 n
mi
Hp = 177
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19816821
45 X = 6070521
44
Y = -9500689
40 feet Y = -2828095
94 meter
Z = 1065839
69 Z = 354284
90
XDOT = 5962
290095 XDOT = 1737
940441
YDOT = 14649
518095 feet/sec YDOT = 4485
050866 meter/sec
ZDOT = 19788
379334 ZDOT = 6040
134291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8728790
90 X = 2660535
47
Y = 20162636
02 feet Y = 6145571
46 meter
Z = 1175518
46 Z = 358298
03
XDOT = -13394
144654 XDOT = -4082
535291
YDOT = 4646
162137 feet/sec YDOT = 1416
150219 meter/sec
ZDOT = 19821
185129 ZDOT = 6041
497227
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 06349
57523475
00020000 00000-0 20000-3 0 9098
2 25544 51
6317 332
3555 0023915 338
7207 21
2961 15
75800549 21784
Satellite: ISS
Catalog Number: 25544
Epoch time: 06349
57523475 = yrday
fracday
Element set: 909
Inclination: 51
6317 deg
RA of node: 332
3555 deg
Eccentricity:
0023915
Arg of perigee: 338
7207 deg
Mean anomaly: 21
2961 deg
Mean motion: 15
75800549 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2178
Checksum: 304
Coasting Arc #11 (Orbit 2192)
---------------------------------------
Vector Time (GMT): 2006/350/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1274273
93 A = 6715409
16 meter
Y = -4090417
93 meter E =
0022048
Z = -5173947
48 I = 51
43895
XDOT = 6816
846360 Wp = 18
24231
YDOT = -3426
759031 meter/sec RA = 327
00096 deg
ZDOT = 1052
051233 TA = 261
69318
MA = 261
94325
Ha = 193
593 n
mi
Hp = 176
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4180688
76 X = -1203305
12
Y = -13420006
34 feet Y = -4104270
13 meter
Z = -16974893
30 Z = -5179966
11
XDOT = 22364
981495 XDOT = 6849
547465
YDOT = -11242
647738 feet/sec YDOT = -3350
346555 meter/sec
ZDOT = 3451
611658 ZDOT = 1085
246989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13504335
37 X = 4116121
42
Y = -3798316
70 feet Y = -1157726
93 meter
Z = -16997865
97 Z = -5180949
55
XDOT = 10484
639942 XDOT = 3195
718254
YDOT = 21596
379925 feet/sec YDOT = 6582
576601 meter/sec
ZDOT = 3575
364452 ZDOT = 1089
771085
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 06350
52650484
00020000 00000-0 20000-3 0 9108
2 25544 51
6316 327
4562 0024114 342
4673 17
5657 15
75779746 21938
Satellite: ISS
Catalog Number: 25544
Epoch time: 06350
52650484 = yrday
fracday
Element set: 910
Inclination: 51
6316 deg
RA of node: 327
4562 deg
Eccentricity:
0024114
Arg of perigee: 342
4673 deg
Mean anomaly: 17
5657 deg
Mean motion: 15
75779746 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2193
Checksum: 298
Coasting Arc #12 (Orbit 2208)
---------------------------------------
Vector Time (GMT): 2006/351/12:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5823916
85 A = 6725846
68 meter
Y = 3017994
87 meter E =
0017069
Z = -1534917
33 I = 51
45222
XDOT = -1064
659370 Wp = 356
99596
YDOT = -4988
559060 meter/sec RA = 321
86071 deg
ZDOT = -5749
343070 TA = 199
94166
MA = 200
00845
Ha = 193
775 n
mi
Hp = 176
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19107338
75 X = -5849775
19
Y = 9901557
98 feet Y = 2952724
24 meter
Z = -5035818
00 Z = -1563272
71
XDOT = -3492
976937 XDOT = -980
867794
YDOT = -16366
663582 feet/sec YDOT = -4999
995340 meter/sec
ZDOT = -18862
674115 ZDOT = -5754
312451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9821138
60 X = -2993483
05
Y = -19120688
03 feet Y = -5827985
71 meter
Z = -5141520
53 Z = -1567135
46
XDOT = 14986
382724 XDOT = 4567
849454
YDOT = -2603
310034 feet/sec YDOT = -793
488898 meter/sec
ZDOT = -18881
823239 ZDOT = -5755
179723
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 06351
54116743
00020000 00000-0 20000-3 0 9117
2 25544 51
6321 322
2299 0024215 346
4397 13
6114 15
75847500 22090
Satellite: ISS
Catalog Number: 25544
Epoch time: 06351
54116743 = yrday
fracday
Element set: 911
Inclination: 51
6321 deg
RA of node: 322
2299 deg
Eccentricity:
0024215
Arg of perigee: 346
4397 deg
Mean anomaly: 13
6114 deg
Mean motion: 15
75847500 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2209
Checksum: 269
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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