Date:
November 22nd 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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
333/23:12:24
637 6
8 12
0 12
0
N/A 9
8 0
1 188
8
000/00:20:49
273 0
7 -0
2 179
4
Coasting Arc #1 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2006/324/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1997795
57 A = 6713889
83 meter
Y = 5182318
21 meter E =
0008408
Z = -3775206
31 I = 51
94116
XDOT = -4317
432250 Wp = 206
35768
YDOT = 4763
596458 meter/sec RA = 101
07112 deg
ZDOT = 4243
415353 TA = 108
08480
MA = 107
99320
Ha = 183
693 n
mi
Hp = 179
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6554447
42 X = 1958037
52
Y = 17002356
34 feet Y = 5204436
74 meter
Z = -12385847
48 Z = -3765596
80
XDOT = -14164
803971 XDOT = -4390
992943
YDOT = 15628
597303 feet/sec YDOT = 4714
904826 meter/sec
ZDOT = 13921
966380 ZDOT = 4222
262398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17318376
54 X = -5278641
17
Y = -5746205
60 feet Y = -1751443
47 meter
Z = -12349294
52 Z = -3764064
97
XDOT = -3369
269777 XDOT = -1026
953428
YDOT = -19674
364849 feet/sec YDOT = -5996
746406 meter/sec
ZDOT = 13843
548904 ZDOT = 4219
513706
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 06324
48512288
00020000 00000-0 20000-3 0 9002
2 25544 51
6305 101
8321 0011410 237
8408 122
1651 15
78260541 17822
Satellite: ISS
Catalog Number: 25544
Epoch time: 06324
48512288 = yrday
fracday
Element set: 900
Inclination: 51
6305 deg
RA of node: 101
8321 deg
Eccentricity:
0011410
Arg of perigee: 237
8408 deg
Mean anomaly: 122
1651 deg
Mean motion: 15
78260541 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1782
Checksum: 256
Coasting Arc #2 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2006/325/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3913256
55 A = 6710877
44 meter
Y = -2960719
81 meter E =
0001750
Z = -4576666
26 I = 51
93616
XDOT = 1666
664363 Wp = 192
11800
YDOT = 6887
585206 meter/sec RA = 95
97328 deg
ZDOT = -3032
084636 TA = 47
91324
MA = 47
89836
Ha = 183
422 n
mi
Hp = 179
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12838768
20 X = 3968306
13
Y = -9713647
68 feet Y = -2916651
26 meter
Z = -15015309
25 Z = -4557521
75
XDOT = 5468
058935 XDOT = 1604
252288
YDOT = 22597
064324 feet/sec YDOT = 6905
874170 meter/sec
ZDOT = -9947
784240 ZDOT = -3024
138531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -484897
08 X = -147796
63
Y = 16158140
84 feet Y = 4925001
33 meter
Z = -14944155
75 Z = -4554978
67
XDOT = -19918
615339 XDOT = -6071
193955
YDOT = -9765
415726 feet/sec YDOT = -2976
498713 meter/sec
ZDOT = -9917
238765 ZDOT = -3022
774375
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 06325
49819684
00020000 00000-0 20000-3 0 9015
2 25544 51
6311 96
5960 0011350 242
4198 117
5815 15
78303943 17980
Satellite: ISS
Catalog Number: 25544
Epoch time: 06325
49819684 = yrday
fracday
Element set: 901
Inclination: 51
6311 deg
RA of node: 96
5960 deg
Eccentricity:
0011350
Arg of perigee: 242
4198 deg
Mean anomaly: 117
5815 deg
Mean motion: 15
78303943 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1798
Checksum: 307
Coasting Arc #3 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2006/326/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -929913
47 A = 6719153
59 meter
Y = -6517396
83 meter E =
0011844
Z = 1303692
23 I = 51
96603
XDOT = 4630
299505 Wp = 172
16912
YDOT = -1837
054544 meter/sec RA = 90
79103 deg
ZDOT = -5886
289846 TA = 353
55285
MA = 353
56808
Ha = 183
063 n
mi
Hp = 179
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3050897
21 X = -863299
17
Y = -21382535
54 feet Y = -6527423
36 meter
Z = 4277205
49 Z = 1299335
52
XDOT = 15191
271341 XDOT = 4679
092798
YDOT = -6027
081838 feet/sec YDOT = -1785
002344 meter/sec
ZDOT = -19311
974562 ZDOT = -5863
677027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18804742
25 X = 5731685
44
Y = 10632417
31 feet Y = 3240760
80 meter
Z = 4260124
14 Z = 1298485
84
XDOT = -3801
823332 XDOT = -1158
795752
YDOT = 14421
062209 feet/sec YDOT = 4395
539761 meter/sec
ZDOT = -19227
712724 ZDOT = -5860
606838
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 06326
51124794
00020000 00000-0 20000-3 0 9021
2 25544 51
6311 91
3587 0011378 246
3680 113
6292 15
78329155 18145
Satellite: ISS
Catalog Number: 25544
Epoch time: 06326
51124794 = yrday
fracday
Element set: 902
Inclination: 51
6311 deg
RA of node: 91
3587 deg
Eccentricity:
0011378
Arg of perigee: 246
3680 deg
Mean anomaly: 113
6292 deg
Mean motion: 15
78329155 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1814
Checksum: 288
Coasting Arc #4 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2006/327/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4140253
31 A = 6707681
17 meter
Y = 128353
23 meter E =
0008917
Z = 5282835
64 I = 51
92817
XDOT = -450
611525 Wp = 247
97265
YDOT = -7687
365683 meter/sec RA = 85
65520 deg
ZDOT = -169
876599 TA = 203
61225
MA = 203
65320
Ha = 182
668 n
mi
Hp = 179
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13583508
24 X = -4167044
42
Y = 421106
38 feet Y = 81904
05 meter
Z = 17332137
91 Z = 5262656
83
XDOT = -1478
384267 XDOT = -363
791591
YDOT = -25221
016019 feet/sec YDOT = -7691
919211 meter/sec
ZDOT = -557
337924 ZDOT = -171
855944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7833731
70 X = 2387721
42
Y = -11221817
60 feet Y = -3420410
00 meter
Z = 17256751
98 Z = 5259858
00
XDOT = 20289
571638 XDOT = 6184
261435
YDOT = 13311
598343 feet/sec YDOT = 4057
375175 meter/sec
ZDOT = -565
672824 ZDOT = -172
417077
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 06327
52427586
00020000 00000-0 20000-3 0 9039
2 25544 51
6325 86
1221 0011276 251
1004 108
8939 15
78372325 18307
Satellite: ISS
Catalog Number: 25544
Epoch time: 06327
52427586 = yrday
fracday
Element set: 903
Inclination: 51
6325 deg
RA of node: 86
1221 deg
Eccentricity:
0011276
Arg of perigee: 251
1004 deg
Mean anomaly: 108
8939 deg
Mean motion: 15
78372325 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1830
Checksum: 278
Coasting Arc #5 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2006/328/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -183640
35 A = 6718501
86 meter
Y = 6519177
26 meter E =
0003835
Z = 1603367
23 I = 51
96261
XDOT = -4847
288409 Wp = 27
66039
YDOT = -1559
433938 meter/sec RA = 80
52438 deg
ZDOT = 5783
215774 TA = 349
98468
MA = 349
99232
Ha = 182
200 n
mi
Hp = 179
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -602494
60 X = -264314
03
Y = 21388376
85 feet Y = 6516672
39 meter
Z = 5260391
17 Z = 1602280
07
XDOT = -15903
177194 XDOT = -4857
584552
YDOT = -5116
253076 feet/sec YDOT = -1613
697407 meter/sec
ZDOT = 18973
805034 ZDOT = 5759
642073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17001628
93 X = -5182096
50
Y = -12992485
78 feet Y = -3960109
67 meter
Z = 5257119
56 Z = 1602370
04
XDOT = 12547
937573 XDOT = 3824
611372
YDOT = -8775
442274 feet/sec YDOT = -2674
754805 meter/sec
ZDOT = 18885
519796 ZDOT = 5756
306434
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 06328
53727954
00020000 00000-0 20000-3 0 9044
2 25544 51
6334 80
8853 0011225 254
7624 105
2301 15
78423682 18464
Satellite: ISS
Catalog Number: 25544
Epoch time: 06328
53727954 = yrday
fracday
Element set: 904
Inclination: 51
6334 deg
RA of node: 80
8853 deg
Eccentricity:
0011225
Arg of perigee: 254
7624 deg
Mean anomaly: 105
2301 deg
Mean motion: 15
78423682 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1846
Checksum: 290
Coasting Arc #6 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2006/329/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4271763
39 A = 6711226
40 meter
Y = 2744177
53 meter E =
0005913
Z = -4389821
38 I = 51
93221
XDOT = -935
464755 Wp = 204
66874
YDOT = 6864
603312 meter/sec RA = 75
33824 deg
ZDOT = 3374
034347 TA = 99
15467
MA = 99
08777
Ha = 181
767 n
mi
Hp = 179
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14014971
74 X = 4262085
29
Y = 9003207
11 feet Y = 2791893
22 meter
Z = -14402301
11 Z = -4369092
09
XDOT = -3069
110087 XDOT = -1028
546789
YDOT = 22521
664410 feet/sec YDOT = 6853
621535 meter/sec
ZDOT = 11069
666494 ZDOT = 3369
264620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15426773
28 X = -4702080
50
Y = 6459638
37 feet Y = 1968897
77 meter
Z = -14324496
04 Z = -4366106
39
XDOT = -16260
326372 XDOT = -4956
147478
YDOT = -14272
530194 feet/sec YDOT = -4350
267203 meter/sec
ZDOT = 11052
670643 ZDOT = 3368
854012
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 06329
48695093
00020000 00000-0 20000-3 0 9058
2 25544 51
6334 75
9765 0011261 259
1717 100
8181 15
78442665 18619
Satellite: ISS
Catalog Number: 25544
Epoch time: 06329
48695093 = yrday
fracday
Element set: 905
Inclination: 51
6334 deg
RA of node: 75
9765 deg
Eccentricity:
0011261
Arg of perigee: 259
1717 deg
Mean anomaly: 100
8181 deg
Mean motion: 15
78442665 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1861
Checksum: 309
Coasting Arc #7 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2006/330/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1527036
89 A = 6712358
59 meter
Y = -5129298
60 meter E =
0004300
Z = -4048640
27 I = 51
92825
XDOT = 4870
184759 Wp = 284
14138
YDOT = 4528
979780 meter/sec RA = 70
23895 deg
ZDOT = -3896
498526 TA = 305
88740
MA = 305
92732
Ha = 181
416 n
mi
Hp = 179
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5009963
55 X = 1603947
63
Y = -16828407
48 feet Y = -5111791
95 meter
Z = -13282940
52 Z = -4041035
62
XDOT = 15978
296453 XDOT = 4838
107727
YDOT = 14858
857545 feet/sec YDOT = 4583
261967 meter/sec
ZDOT = -12783
787815 ZDOT = -3872
916415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11174203
91 X = 3405897
35
Y = 13570926
67 feet Y = 4136418
45 meter
Z = -13255137
06 Z = -4040165
78
XDOT = -20279
069586 XDOT = -6181
060410
YDOT = 4283
660929 feet/sec YDOT = 1305
659851 meter/sec
ZDOT = -12695
098964 ZDOT = -3869
466164
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 06330
49991090
00020000 00000-0 20000-3 0 9068
2 25544 51
6338 70
7392 0011242 263
2377 96
7509 15
78465297 18779
Satellite: ISS
Catalog Number: 25544
Epoch time: 06330
49991090 = yrday
fracday
Element set: 906
Inclination: 51
6338 deg
RA of node: 70
7392 deg
Eccentricity:
0011242
Arg of perigee: 263
2377 deg
Mean anomaly: 96
7509 deg
Mean motion: 15
78465297 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1877
Checksum: 319
Coasting Arc #8 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2006/331/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4097041
00 A = 6717497
94 meter
Y = -4880298
06 meter E =
0005840
Z = 2114014
19 I = 51
93479
XDOT = 2648
402311 Wp = 158
15904
YDOT = -4632
395178 meter/sec RA = 65
04515 deg
ZDOT = -5561
821890 TA = 358
26575
MA = 358
26778
Ha = 181
021 n
mi
Hp = 179
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13441735
58 X = -4052433
89
Y = -16011476
58 feet Y = -4925864
22 meter
Z = 6935742
10 Z = 2094218
56
XDOT = 8688
983959 XDOT = 2727
024073
YDOT = -15198
146909 feet/sec YDOT = -4602
339201 meter/sec
ZDOT = -18247
447146 ZDOT = -5548
765286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20758060
65 X = 6327056
89
Y = -2679470
18 feet Y = -816702
51 meter
Z = 6861159
80 Z = 2091281
51
XDOT = 7834
818267 XDOT = 2388
052608
YDOT = 14098
991062 feet/sec YDOT = 4297
372476 meter/sec
ZDOT = -18199
203791 ZDOT = -5547
117315
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 06331
51284831
00020000 00000-0 20000-3 0 9071
2 25544 51
6337 65
5022 0011090 267
4018 92
5878 15
78497768 18938
Satellite: ISS
Catalog Number: 25544
Epoch time: 06331
51284831 = yrday
fracday
Element set: 907
Inclination: 51
6337 deg
RA of node: 65
5022 deg
Eccentricity:
0011090
Arg of perigee: 267
4018 deg
Mean anomaly: 92
5878 deg
Mean motion: 15
78497768 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1893
Checksum: 311
Coasting Arc #9 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2006/332/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3146658
21 A = 6707248
86 meter
Y = 2771646
45 meter E =
0008495
Z = 5242153
09 I = 51
88847
XDOT = -4334
860043 Wp = 262
74954
YDOT = -6323
519752 meter/sec RA = 59
91878 deg
ZDOT = 741
311075 TA = 180
22417
MA = 180
22455
Ha = 180
833 n
mi
Hp = 179
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10323681
79 X = -3202882
94
Y = 9093328
25 feet Y = 2736144
07 meter
Z = 17198664
99 Z = 5226730
09
XDOT = -14221
981769 XDOT = -4267
428571
YDOT = -20746
455879 feet/sec YDOT = -6371
617583 meter/sec
ZDOT = 2432
122948 ZDOT = 720
415522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2249292
40 X = -685584
32
Y = -13644629
31 feet Y = -4158883
01 meter
Z = 17141349
90 Z = 5224683
45
XDOT = 24137
657493 XDOT = 7357
158004
YDOT = -1022
589474 feet/sec YDOT = -311
685272 meter/sec
ZDOT = 2353
253636 ZDOT = 717
271708
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 06332
52576098
00020000 00000-0 20000-3 0 9083
2 25544 51
6344 60
2639 0011146 272
2165 87
7724 15
78581398 19098
Satellite: ISS
Catalog Number: 25544
Epoch time: 06332
52576098 = yrday
fracday
Element set: 908
Inclination: 51
6344 deg
RA of node: 60
2639 deg
Eccentricity:
0011146
Arg of perigee: 272
2165 deg
Mean anomaly: 87
7724 deg
Mean motion: 15
78581398 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1909
Checksum: 313
Coasting Arc #10 (Orbit 1924)
---------------------------------------
Vector Time (GMT): 2006/333/11:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3250962
35 A = 6718835
58 meter
Y = 5805889
85 meter E =
0009210
Z = 885144
84 I = 51
91225
XDOT = -4574
232571 Wp =
94480
YDOT = 1650
529250 meter/sec RA = 54
76934 deg
ZDOT = 5982
149929 TA = 8
69970
MA = 8
68374
Ha = 181
126 n
mi
Hp = 179
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10665886
97 X = 3181498
52
Y = 19048195
04 feet Y = 5841855
48 meter
Z = 2904018
52 Z = 900769
80
XDOT = -15007
324708 XDOT = -4621
409645
YDOT = 5415
122211 feet/sec YDOT = 1599
113553 meter/sec
ZDOT = 19626
476145 ZDOT = 5959
813497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21815040
72 X = -6649224
41
Y = -593386
34 feet Y = -180864
16 meter
Z = 2963122
34 Z = 903159
69
XDOT = 3036
349559 XDOT = 925
479346
YDOT = -14167
453737 feet/sec YDOT = -4318
239899 meter/sec
ZDOT = 19543
182601 ZDOT = 5956
762057
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 06333
53865425
00020000 00000-0 20000-3 0 9091
2 25544 51
6346 55
0263 0011029 276
9503 83
0408 15
78577286 19259
Satellite: ISS
Catalog Number: 25544
Epoch time: 06333
53865425 = yrday
fracday
Element set: 909
Inclination: 51
6346 deg
RA of node: 55
0263 deg
Eccentricity:
0011029
Arg of perigee: 276
9503 deg
Mean anomaly: 83
0408 deg
Mean motion: 15
78577286 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1925
Checksum: 302
Coasting Arc #11 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2006/333/23:22:49
273
Vector Time (MET): N/A
Weight (LBS) : 469585
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5238920
37 A = 6721022
62 meter
Y = 2097697
13 meter E =
0015843
Z = -3635092
83 I = 51
88518
XDOT = 533
303516 Wp = 277
74230
YDOT = 6311
686276 meter/sec RA = 52
17564 deg
ZDOT = 4396
768726 TA = 38
76341
MA = 38
64984
Ha = 188
785 n
mi
Hp = 179
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17188058
96 X = 5232733
16
Y = 6882208
42 feet Y = 2156247
23 meter
Z = -11926157
58 Z = -3609656
67
XDOT = 1749
683452 XDOT = 441
326671
YDOT = 20707
632138 feet/sec YDOT = 6317
135480 meter/sec
ZDOT = 14425
094244 ZDOT = 4399
136461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14848592
84 X = 4525851
10
Y = -11161461
22 feet Y = -3402013
38 meter
Z = -11830827
19 Z = -3606036
13
XDOT = 17743
755777 XDOT = 5408
296761
YDOT = 8255
494750 feet/sec YDOT = 2516
274800 meter/sec
ZDOT = 14434
702010 ZDOT = 4399
697173
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 06333
98179283
00020000 00000-0 20000-3 0 9102
2 25544 51
6341 52
7375 0021364 278
3300 81
5442 15
75925819 19321
Satellite: ISS
Catalog Number: 25544
Epoch time: 06333
98179283 = yrday
fracday
Element set: 910
Inclination: 51
6341 deg
RA of node: 52
7375 deg
Eccentricity:
0021364
Arg of perigee: 278
3300 deg
Mean anomaly: 81
5442 deg
Mean motion: 15
75925819 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1932
Checksum: 295
Coasting Arc #12 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2006/334/23:22:49
273
Vector Time (MET): N/A
Weight (LBS) : 469585
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -283652
75 A = 6718736
75 meter
Y = -5197510
52 meter E =
0015002
Z = -4241818
54 I = 51
86035
XDOT = 6291
627461 Wp = 300
09140
YDOT = 2611
897289 meter/sec RA = 47
09301 deg
ZDOT = -3604
294949 TA = 293
34481
MA = 293
50257
Ha = 188
770 n
mi
Hp = 179
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -930619
24 X = -204905
95
Y = -17052199
87 feet Y = -5200241
93 meter
Z = -13916727
48 Z = -4243005
59
XDOT = 20641
822379 XDOT = 6279
462631
YDOT = 8569
216829 feet/sec YDOT = 2682
185966 meter/sec
ZDOT = -11825
114662 ZDOT = -3573
758967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15148376
66 X = -4617225
21
Y = -7875882
45 feet Y = -2400568
97 meter
Z = -13921782
80 Z = -4243359
40
XDOT = 17280
202580 XDOT = 5267
005746
YDOT = -12438
852370 feet/sec YDOT = -3791
362202 meter/sec
ZDOT = -11710
662609 ZDOT = -3569
409963
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 06334
99638020
00020000 00000-0 20000-3 0 9114
2 25544 51
6349 47
5119 0021369 282
5884 77
2891 15
75964035 19486
Satellite: ISS
Catalog Number: 25544
Epoch time: 06334
99638020 = yrday
fracday
Element set: 911
Inclination: 51
6349 deg
RA of node: 47
5119 deg
Eccentricity:
0021369
Arg of perigee: 282
5884 deg
Mean anomaly: 77
2891 deg
Mean motion: 15
75964035 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1948
Checksum: 322
Coasting Arc #13 (Orbit 1963)
---------------------------------------
Vector Time (GMT): 2006/335/23:22:49
273
Vector Time (MET): N/A
Weight (LBS) : 469585
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5724454
15 A = 6723775
28 meter
Y = -2410975
82 meter E =
0007523
Z = 2584374
45 I = 51
85655
XDOT = -23
677817 Wp = 290
65517
YDOT = -5595
594086 meter/sec RA = 41
91089 deg
ZDOT = -5282
317902 TA = 220
10667
MA = 220
16222
Ha = 188
928 n
mi
Hp = 179
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18781017
56 X = -5709623
56
Y = -7910025
67 feet Y = -2474907
15 meter
Z = 8478918
80 Z = 2556600
18
XDOT = -77
683126 XDOT = 64
555837
YDOT = -18358
248314 feet/sec YDOT = -5595
365073 meter/sec
ZDOT = -17330
439310 ZDOT = -5282
219087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16123173
64 X = -4914343
33
Y = 12533671
21 feet Y = 3820262
98 meter
Z = 8374816
33 Z = 2552644
02
XDOT = -15078
697734 XDOT = -4595
987069
YDOT = -7838
486098 feet/sec YDOT = -2389
170563 meter/sec
ZDOT = -17330
727368 ZDOT = -5282
405702
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 06336
01094986
00020000 00000-0 20000-3 0 9127
2 25544 51
6347 42
2858 0021293 286
3582 73
5241 15
75956944 19645
Satellite: ISS
Catalog Number: 25544
Epoch time: 06336
01094986 = yrday
fracday
Element set: 912
Inclination: 51
6347 deg
RA of node: 42
2858 deg
Eccentricity:
0021293
Arg of perigee: 286
3582 deg
Mean anomaly: 73
5241 deg
Mean motion: 15
75956944 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1964
Checksum: 314
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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