Date:
December 12th 2006
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) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 2066)
---------------------------------------
Vector Time (GMT): 2006/342/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4549124
41 A = 6722329
52 meter
Y = 3479313
51 meter E =
0016253
Z = 3510364
52 I = 51
68160
XDOT = -5592
558428 Wp = 338
78432
YDOT = 2777
909699 meter/sec RA = 8
43762 deg
ZDOT = 4515
462712 TA = 62
97997
MA = 62
81414
Ha = 191
951 n
mi
Hp = 178
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14924948
86 X = 4492827
44
Y = 11415070
56 feet Y = 3529869
03 meter
Z = 11516943
97 Z = 3532327
95
XDOT = -18348
288805 XDOT = -5645
141036
YDOT = 9113
876965 feet/sec YDOT = 2715
075906 meter/sec
ZDOT = 14814
510210 ZDOT = 4488
166784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16007169
29 X = -4878985
20
Y = 9742733
79 feet Y = 2969585
26 meter
Z = 11599465
59 Z = 3535517
11
XDOT = -1141
570489 XDOT = -347
950685
YDOT = -19309
486188 feet/sec YDOT = -5885
531390 meter/sec
ZDOT = 14712
749538 ZDOT = 4484
446059
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
53518261
00020000 00000-0 20000-3 0 9005
2 25544 51
6341 8
6043 0023926 311
5507 48
3605 15
75545710 20678
Satellite: ISS
Catalog Number: 25544
Epoch time: 06342
53518261 = yrday
fracday
Element set: 900
Inclination: 51
6341 deg
RA of node: 8
6043 deg
Eccentricity:
0023926
Arg of perigee: 311
5507 deg
Mean anomaly: 48
3605 deg
Mean motion: 15
75545710 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2067
Checksum: 265
Coasting Arc #2 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2006/343/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5093724
48 A = 6722107
71 meter
Y = -2530489
16 meter E =
0020057
Z = -3557737
31 I = 51
65417
XDOT = 5008
221809 Wp = 324
21159
YDOT = 3816
648712 meter/sec RA = 3
24024 deg
ZDOT = 4459
212388 TA = 353
24248
MA = 353
26948
Ha = 192
222 n
mi
Hp = 178
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16711694
49 X = 5138924
99
Y = -8302129
79 feet Y = -2473275
11 meter
Z = -11672366
50 Z = -3532882
60
XDOT = 16431
173915 XDOT = 4943
509296
YDOT = 12521
813359 feet/sec YDOT = 3872
291014 meter/sec
ZDOT = 14629
961903 ZDOT = 4483
385591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2011972
21 X = 613249
13
Y = 18609477
19 feet Y = 5672168
65 meter
Z = -11579704
57 Z = -3529493
95
XDOT = -16032
249656 XDOT = -4886
629695
YDOT = 10886
259982 feet/sec YDOT = 3318
132042 meter/sec
ZDOT = 14720
790441 ZDOT = 4486
896927
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
48656892
00020000 00000-0 20000-3 0 9014
2 25544 51
6353 3
7067 0023914 315
1747 44
7484 15
75624314 20826
Satellite: ISS
Catalog Number: 25544
Epoch time: 06343
48656892 = yrday
fracday
Element set: 901
Inclination: 51
6353 deg
RA of node: 3
7067 deg
Eccentricity:
0023914
Arg of perigee: 315
1747 deg
Mean anomaly: 44
7484 deg
Mean motion: 15
75624314 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2082
Checksum: 292
Coasting Arc #3 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2006/344/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4116861
34 A = 6719577
73 meter
Y = -3219160
30 meter E =
0022389
Z = -4230441
20 I = 51
61768
XDOT = 6092
630119 Wp = 339
41869
YDOT = -3041
355373 meter/sec RA = 358
14294 deg
ZDOT = -3588
389144 TA = 253
96497
MA = 254
21166
Ha = 192
302 n
mi
Hp = 178
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13506762
93 X = -4060007
59
Y = -10561549
54 feet Y = -3264878
98 meter
Z = -13879400
28 Z = -4250303
14
XDOT = 19988
943960 XDOT = 6143
617871
YDOT = -9978
200044 feet/sec YDOT = -2972
938716 meter/sec
ZDOT = -11772
930261 ZDOT = -3558
667695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14386312
33 X = 4384948
00
Y = -9216042
40 feet Y = -2809049
72 meter
Z = -13954042
63 Z = -4253192
19
XDOT = 2166
319514 XDOT = 660
294188
YDOT = 21169
456457 feet/sec YDOT = 6452
450328 meter/sec
ZDOT = -11662
125587 ZDOT = -3554
615879
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
50135111
00020000 00000-0 20000-3 0 9025
2 25544 51
6352 358
4822 0023894 319
1427 40
7945 15
75664939 20982
Satellite: ISS
Catalog Number: 25544
Epoch time: 06344
50135111 = yrday
fracday
Element set: 902
Inclination: 51
6352 deg
RA of node: 358
4822 deg
Eccentricity:
0023894
Arg of perigee: 319
1427 deg
Mean anomaly: 40
7945 deg
Mean motion: 15
75664939 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2098
Checksum: 299
Coasting Arc #4 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2006/345/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5527865
50 A = 6724306
24 meter
Y = 2794158
50 meter E =
0016115
Z = 2642396
10 I = 51
60435
XDOT = -4332
288516 Wp = 356
35849
YDOT = -3627
019196 meter/sec RA = 352
94452 deg
ZDOT = -5213
710218 TA = 153
59715
MA = 153
51494
Ha = 192
523 n
mi
Hp = 178
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18136041
66 X = -5571535
61
Y = 9167186
68 feet Y = 2732098
42 meter
Z = 8669278
54 Z = 2615435
92
XDOT = -14213
544999 XDOT = -4266
081435
YDOT = -11899
669278 feet/sec YDOT = -3675
094580 meter/sec
ZDOT = -17105
348485 ZDOT = -5234
596000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3033362
91 X = -924569
01
Y = -20136646
84 feet Y = -6137649
96 meter
Z = 8568773
10 Z = 2611762
04
XDOT = 14243
542262 XDOT = 4341
431682
YDOT = -9477
765944 feet/sec YDOT = -2888
823060 meter/sec
ZDOT = -17183
868371 ZDOT = -5237
643079
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
51610149
00020000 00000-0 20000-3 0 9037
2 25544 51
6340 353
2568 0023902 323
3039 36
6488 15
75725611 21145
Satellite: ISS
Catalog Number: 25544
Epoch time: 06345
51610149 = yrday
fracday
Element set: 903
Inclination: 51
6340 deg
RA of node: 353
2568 deg
Eccentricity:
0023902
Arg of perigee: 323
3039 deg
Mean anomaly: 36
6488 deg
Mean motion: 15
75725611 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2114
Checksum: 274
Coasting Arc #5 (Orbit 2129)
---------------------------------------
Vector Time (GMT): 2006/346/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3417880
24 A = 6716975
75 meter
Y = 3183678
20 meter E =
0017901
Z = 4827102
13 I = 51
55148
XDOT = -6501
409707 Wp = 336
16887
YDOT = 3357
709456 meter/sec RA = 347
83190 deg
ZDOT = 2408
028295 TA = 90
40904
MA = 90
20391
Ha = 192
661 n
mi
Hp = 177
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11213517
86 X = 3358576
62
Y = 10445138
47 feet Y = 3221566
85 meter
Z = 15836949
24 Z = 4843562
47
XDOT = -21330
084342 XDOT = -6550
170689
YDOT = 11016
107138 feet/sec YDOT = 3284
734241 meter/sec
ZDOT = 7900
355298 ZDOT = 2376
326187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13268157
19 X = -4044134
31
Y = 7538886
38 feet Y = 2297852
57 meter
Z = 15898869
73 Z = 4845975
49
XDOT = -3652
413165 XDOT = -1113
255533
YDOT = -22707
821577 feet/sec YDOT = -6921
344017 meter/sec
ZDOT = 7782
182342 ZDOT = 2372
009178
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
53082107
00020000 00000-0 20000-3 0 9048
2 25544 51
6335 348
0307 0023829 327
2809 32
6878 15
75744135 21307
Satellite: ISS
Catalog Number: 25544
Epoch time: 06346
53082107 = yrday
fracday
Element set: 904
Inclination: 51
6335 deg
RA of node: 348
0307 deg
Eccentricity:
0023829
Arg of perigee: 327
2809 deg
Mean anomaly: 32
6878 deg
Mean motion: 15
75744135 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2130
Checksum: 287
Coasting Arc #6 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2006/347/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5756718
81 A = 6725976
06 meter
Y = -3078741
67 meter E =
0028095
Z = -1538458
45 I = 51
55551
XDOT = 3525
960090 Wp = 346
19569
YDOT = 3706
581072 meter/sec RA = 342
64420 deg
ZDOT = 5781
447670 TA = 356
77458
MA = 356
79266
Ha = 192
770 n
mi
Hp = 177
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18886872
73 X = 5798191
48
Y = -10100858
50 feet Y = -3014134
83 meter
Z = -5047435
84 Z = -1510391
63
XDOT = 11568
110532 XDOT = 3456
165103
YDOT = 12160
699054 feet/sec YDOT = 3745
619595 meter/sec
ZDOT = 18968
004168 ZDOT = 5798
407677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4416683
74 X = 1346205
20
Y = 20982832
85 feet Y = 6395567
45 meter
Z = -4942827
42 Z = -1506573
80
XDOT = -13347
889461 XDOT = -4068
436708
YDOT = 7288
659209 feet/sec YDOT = 2221
583327 meter/sec
ZDOT = 19031
853001 ZDOT = 5800
908795
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
48209037
00020000 00000-0 20000-3 0 9057
2 25544 51
6341 343
1330 0023702 330
8531 29
1308 15
75835458 21452
Satellite: ISS
Catalog Number: 25544
Epoch time: 06347
48209037 = yrday
fracday
Element set: 905
Inclination: 51
6341 deg
RA of node: 343
1330 deg
Eccentricity:
0023702
Arg of perigee: 330
8531 deg
Mean anomaly: 29
1308 deg
Mean motion: 15
75835458 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2145
Checksum: 271
Coasting Arc #7 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2006/348/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2697806
14 A = 6715228
12 meter
Y = -3337286
81 meter E =
0023910
Z = -5172250
35 I = 51
49147
XDOT = 6670
423784 Wp = 9
63127
YDOT = -3688
819077 meter/sec RA = 337
50970 deg
ZDOT = -1076
623139 TA = 249
94441
MA = 250
20195
Ha = 192
958 n
mi
Hp = 177
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8851070
01 X = -2635161
50
Y = -10949103
70 feet Y = -3367104
45 meter
Z = -16969325
28 Z = -5185204
56
XDOT = 21884
592466 XDOT = 6716
407010
YDOT = -12102
424794 feet/sec YDOT = -3613
969492 meter/sec
ZDOT = -3532
228147 ZDOT = -1044
106509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12864962
14 X = 3921240
46
Y = -5572934
47 feet Y = -1698630
43 meter
Z = -17018150
99 Z = -5187132
42
XDOT = 5516
528518 XDOT = 1681
437892
YDOT = 23375
747801 feet/sec YDOT = 7124
927930 meter/sec
ZDOT = -3411
049329 ZDOT = -1039
687835
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
49674690
00020000 00000-0 20000-3 0 9061
2 25544 51
6329 337
9071 0023802 334
7246 25
2751 15
75841198 21613
Satellite: ISS
Catalog Number: 25544
Epoch time: 06348
49674690 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 337
9071 deg
Eccentricity:
0023802
Arg of perigee: 334
7246 deg
Mean anomaly: 25
2751 deg
Mean motion: 15
75841198 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2161
Checksum: 306
Coasting Arc #8 (Orbit 2176)
---------------------------------------
Vector Time (GMT): 2006/349/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5849891
41 A = 6726685
22 meter
Y = 3326631
60 meter E =
0013701
Z = 289764
85 I = 51
50443
XDOT = -2593
383003 Wp = 2
91557
YDOT = -4034
941730 meter/sec RA = 332
33706 deg
ZDOT = -6007
411101 TA = 173
93361
MA = 173
91700
Ha = 193
153 n
mi
Hp = 177
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19192557
11 X = -5888063
13
Y = 10914145
67 feet Y = 3261001
41 meter
Z = 950672
06 Z = 261253
31
XDOT = -8508
474419 XDOT = -2518
887665
YDOT = -13237
997802 feet/sec YDOT = -4063
525242 meter/sec
ZDOT = -19709
354006 ZDOT = -6019
829387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5854495
28 X = -1784450
16
Y = -21292919
64 feet Y = -6490081
91 meter
Z = 844428
48 Z = 257381
80
XDOT = 13344
953122 XDOT = 4067
541712
YDOT = -4456
482383 feet/sec YDOT = -1358
335830 meter/sec
ZDOT = -19756
254170 ZDOT = -6021
706271
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
51137041
00020000 00000-0 20000-3 0 9070
2 25544 51
6323 332
6805 0023873 338
8837 21
1340 15
75916548 21771
Satellite: ISS
Catalog Number: 25544
Epoch time: 06349
51137041 = yrday
fracday
Element set: 907
Inclination: 51
6323 deg
RA of node: 332
6805 deg
Eccentricity:
0023873
Arg of perigee: 338
8837 deg
Mean anomaly: 21
1340 deg
Mean motion: 15
75916548 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2177
Checksum: 293
Coasting Arc #9 (Orbit 2192)
---------------------------------------
Vector Time (GMT): 2006/350/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1841491
11 A = 6714646
79 meter
Y = 3782275
66 meter E =
0024135
Z = 5239166
73 I = 51
43881
XDOT = -6641
805190 Wp = 348
41271
YDOT = 3870
503650 meter/sec RA = 327
17254 deg
ZDOT = -436
769815 TA = 105
88054
MA = 105
61439
Ha = 193
261 n
mi
Hp = 176
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6041637
51 X = 1773609
01
Y = 12409040
88 feet Y = 3802488
05 meter
Z = 17188867
22 Z = 5247948
40
XDOT = -21790
699441 XDOT = -6682
470290
YDOT = 12698
502790 feet/sec YDOT = 3796
003979 meter/sec
ZDOT = -1432
971833 ZDOT = -469
134500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13442012
68 X = -4097125
47
Y = 2941614
97 feet Y = 896604
24 meter
Z = 17222137
85 Z = 5249307
62
XDOT = -7149
299426 XDOT = -2179
106465
YDOT = -23134
119949 feet/sec YDOT = -7051
279760 meter/sec
ZDOT = -1553
566099 ZDOT = -473
526947
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
52596121
00020000 00000-0 20000-3 0 9082
2 25544 51
6317 327
4535 0023824 342
4901 17
5439 15
75945097 21932
Satellite: ISS
Catalog Number: 25544
Epoch time: 06350
52596121 = yrday
fracday
Element set: 908
Inclination: 51
6317 deg
RA of node: 327
4535 deg
Eccentricity:
0023824
Arg of perigee: 342
4901 deg
Mean anomaly: 17
5439 deg
Mean motion: 15
75945097 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2193
Checksum: 296
Coasting Arc #10 (Orbit 2208)
---------------------------------------
Vector Time (GMT): 2006/351/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5689849
70 A = 6725881
80 meter
Y = -3391605
75 meter E =
0031072
Z = 1038967
75 I = 51
45450
XDOT = 1696
674283 Wp = 10
55756
YDOT = 4659
174614 meter/sec RA = 322
02284 deg
ZDOT = 5920
006679 TA =
86965
MA =
86426
Ha = 193
167 n
mi
Hp = 176
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18667485
90 X = 5722305
04
Y = -11127315
46 feet Y = -3327797
37 meter
Z = 3408686
83 Z = 1066687
80
XDOT = 5566
516678 XDOT = 1615
689892
YDOT = 15286
005951 feet/sec YDOT = 4677
694111 meter/sec
ZDOT = 19422
594090 ZDOT = 5928
053201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6908532
98 X = 2105720
85
Y = 20587606
90 feet Y = 6275102
58 meter
Z = 3511970
84 Z = 1070448
71
XDOT = -14595
709973 XDOT = -4448
772400
YDOT = 1580
660915 feet/sec YDOT = 481
785447 meter/sec
ZDOT = 19453
213926 ZDOT = 5929
339605
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
54051671
00020000 00000-0 20000-3 0 9092
2 25544 51
6318 322
2275 0023592 346
3458 13
7065 15
76046863 22094
Satellite: ISS
Catalog Number: 25544
Epoch time: 06351
54051671 = yrday
fracday
Element set: 909
Inclination: 51
6318 deg
RA of node: 322
2275 deg
Eccentricity:
0023592
Arg of perigee: 346
3458 deg
Mean anomaly: 13
7065 deg
Mean motion: 15
76046863 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2209
Checksum: 288
Coasting Arc #11 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2006/352/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1143358
00 A = 6715586
48 meter
Y = -4369277
12 meter E =
0021851
Z = -4971349
44 I = 51
39797
XDOT = 6378
932671 Wp = 22
64329
YDOT = -3855
671075 meter/sec RA = 316
82965 deg
ZDOT = 1944
320835 TA = 266
07503
MA = 266
32487
Ha = 193
475 n
mi
Hp = 176
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3751174
54 X = -1070264
93
Y = -14334898
67 feet Y = -4381653
27 meter
Z = -16310201
56 Z = -4976727
12
XDOT = 20928
256794 XDOT = 6412
127951
YDOT = -12649
839485 feet/sec YDOT = -3784
153025 meter/sec
ZDOT = 6379
005364 ZDOT = 1975
390083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14774083
59 X = 4503140
68
Y = -783899
95 feet Y = -238932
71 meter
Z = -16330807
10 Z = -4977630
00
XDOT = 8258
246815 XDOT = 2517
113629
YDOT = 21887
282004 feet/sec YDOT = 6671
243555 meter/sec
ZDOT = 6494
769602 ZDOT = 1979
605775
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 06352
49163552
00020000 00000-0 20000-3 0 9101
2 25544 51
6318 317
3273 0023781 350
1043 9
9650 15
76031449 22248
Satellite: ISS
Catalog Number: 25544
Epoch time: 06352
49163552 = yrday
fracday
Element set: 910
Inclination: 51
6318 deg
RA of node: 317
3273 deg
Eccentricity:
0023781
Arg of perigee: 350
1043 deg
Mean anomaly: 9
9650 deg
Mean motion: 15
76031449 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2224
Checksum: 271
Coasting Arc #12 (Orbit 2239)
---------------------------------------
Vector Time (GMT): 2006/353/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5412288
44 A = 6723659
09 meter
Y = 3239821
23 meter E =
0019902
Z = -2363186
81 I = 51
40688
XDOT = -899
255252 Wp = 4
19121
YDOT = -5428
282151 meter/sec RA = 311
69763 deg
ZDOT = -5365
707449 TA = 202
47948
MA = 202
56680
Ha = 193
586 n
mi
Hp = 175
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17756851
84 X = -5436634
29
Y = 10629334
74 feet Y = 3179162
32 meter
Z = -7753237
58 Z = -2389538
49
XDOT = -2950
312507 XDOT = -812
422745
YDOT = -17809
324642 feet/sec YDOT = -5437
851639 meter/sec
ZDOT = -17604
027065 ZDOT = -5369
866142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7289850
29 X = -2221946
37
Y = -19329104
73 feet Y = -5891511
12 meter
Z = -7851434
93 Z = -2393117
37
XDOT = 16622
795137 XDOT = 5066
627958
YDOT = 910
074243 feet/sec YDOT = 277
390629 meter/sec
ZDOT = -17620
193352 ZDOT = -5370
634934
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 06353
50612743
00020000 00000-0 20000-3 0 9116
2 25544 51
6323 312
0998 0023826 354
1046 5
9834 15
76119372 22407
Satellite: ISS
Catalog Number: 25544
Epoch time: 06353
50612743 = yrday
fracday
Element set: 911
Inclination: 51
6323 deg
RA of node: 312
0998 deg
Eccentricity:
0023826
Arg of perigee: 354
1046 deg
Mean anomaly: 5
9834 deg
Mean motion: 15
76119372 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2240
Checksum: 275
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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