Date:
November 30th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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
333/23:14:55
710 5
3 11
6 11
6
N/A 10
0 0
0 188
5
000/00:19:51
420 2
5 -0
2 179
2
Coasting Arc #1 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2006/331/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3503599
71 A = 6718779
83 meter
Y = -5634695
50 meter E =
0008343
Z = 1021094
46 I = 51
94012
XDOT = 3599
859651 Wp = 177
86733
YDOT = -3316
372364 meter/sec RA = 65
04760 deg
ZDOT = -5955
407618 TA = 350
99440
MA = 351
00935
Ha = 180
920 n
mi
Hp = 179
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11494749
69 X = -3445291
68
Y = -18486533
79 feet Y = -5673548
77 meter
Z = 3350047
45 Z = 1004215
01
XDOT = 11810
563159 XDOT = 3665
606729
YDOT = -10880
486758 feet/sec YDOT = -3275
748616 meter/sec
ZDOT = -19538
738904 ZDOT = -5937
759963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21778513
80 X = 6638091
01
Y = 27554
36 feet Y = 8398
57 meter
Z = 3286274
09 Z = 1001656
34
XDOT = 2916
999508 XDOT = 889
101450
YDOT = 14284
344925 feet/sec YDOT = 4353
868333 meter/sec
ZDOT = -19473
175968 ZDOT = -5935
424035
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
51274219
00020000 00000-0 20000-3 0 9003
2 25544 51
6340 65
5069 0011103 267
1030 92
8865 15
78565776 18933
Satellite: ISS
Catalog Number: 25544
Epoch time: 06331
51274219 = yrday
fracday
Element set: 900
Inclination: 51
6340 deg
RA of node: 65
5069 deg
Eccentricity:
0011103
Arg of perigee: 267
1030 deg
Mean anomaly: 92
8865 deg
Mean motion: 15
78565776 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1893
Checksum: 288
Coasting Arc #2 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2006/332/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3899353
50 A = 6706988
02 meter
Y = 1494043
35 meter E =
0008645
Z = 5255861
60 I = 51
88859
XDOT = -3438
106028 Wp = 280
66826
YDOT = -6866
591395 meter/sec RA = 59
90021 deg
ZDOT = -598
095304 TA = 174
99973
MA = 174
99109
Ha = 180
697 n
mi
Hp = 179
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12793154
53 X = -3941302
55
Y = 4901717
01 feet Y = 1450203
73 meter
Z = 17243640
41 Z = 5236816
56
XDOT = -11279
875421 XDOT = -3358
161849
YDOT = -22528
186991 feet/sec YDOT = -6904
591177 meter/sec
ZDOT = -1962
254933 ZDOT = -614
604026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2436702
60 X = 742706
95
Y = -13571954
56 feet Y = -4136731
75 meter
Z = 17172632
21 Z = 5234218
30
XDOT = 24124
587676 XDOT = 7353
174324
YDOT = 1766
249632 feet/sec YDOT = 538
352888 meter/sec
ZDOT = -2024
792239 ZDOT = -617
156674
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
52560968
00020000 00000-0 20000-3 0 9015
2 25544 51
6346 60
2684 0011117 272
1931 87
7962 15
78657677 19096
Satellite: ISS
Catalog Number: 25544
Epoch time: 06332
52560968 = yrday
fracday
Element set: 901
Inclination: 51
6346 deg
RA of node: 60
2684 deg
Eccentricity:
0011117
Arg of perigee: 272
1931 deg
Mean anomaly: 87
7962 deg
Mean motion: 15
78657677 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1909
Checksum: 313
Coasting Arc #3 (Orbit 1924)
---------------------------------------
Vector Time (GMT): 2006/333/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2271834
34 A = 6717072
32 meter
Y = 5980263
61 meter E =
0006641
Z = 2033332
48 I = 51
90751
XDOT = -5296
712900 Wp = 19
79148
YDOT = 108
611451 meter/sec RA = 54
77127 deg
ZDOT = 5599
396008 TA = 2
84523
MA = 2
84146
Ha = 180
912 n
mi
Hp = 179
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7453524
73 X = 2194915
65
Y = 19620287
42 feet Y = 6005238
34 meter
Z = 6671038
33 Z = 2044182
67
XDOT = -17377
666995 XDOT = -5324
734963
YDOT = 356
336781 feet/sec YDOT = 49
223699 meter/sec
ZDOT = 18370
721811 ZDOT = 5573
596168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20698976
95 X = -6309048
17
Y = -3392733
07 feet Y = -1034105
04 meter
Z = 6712315
36 Z = 2045913
72
XDOT = 8187
698805 XDOT = 2495
610596
YDOT = -13803
766479 feet/sec YDOT = -4207
388023 meter/sec
ZDOT = 18274
296702 ZDOT = 5570
005635
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
53844851
00020000 00000-0 20000-3 0 9024
2 25544 51
6347 55
0304 0010989 276
4604 83
5310 15
78678653 19254
Satellite: ISS
Catalog Number: 25544
Epoch time: 06333
53844851 = yrday
fracday
Element set: 902
Inclination: 51
6347 deg
RA of node: 55
0304 deg
Eccentricity:
0010989
Arg of perigee: 276
4604 deg
Mean anomaly: 83
5310 deg
Mean motion: 15
78678653 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1925
Checksum: 300
Coasting Arc #4 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2006/333/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5243599
58 A = 6722341
79 meter
Y = 2962853
86 meter E =
0017479
Z = -2963866
51 I = 51
89191
XDOT = -451
716437 Wp = 292
24353
YDOT = 5837
151026 meter/sec RA = 52
17258 deg
ZDOT = 5019
113142 TA = 33
62099
MA = 33
51021
Ha = 188
485 n
mi
Hp = 179
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17203410
71 X = 5224476
98
Y = 9720649
13 feet Y = 3021383
93 meter
Z = -9723971
50 Z = -2938439
00
XDOT = -1482
009307 XDOT = -541
337038
YDOT = 19150
757959 feet/sec YDOT = 5831
598333 meter/sec
ZDOT = 16466
906634 ZDOT = 5016
701273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17188008
45 X = 5238904
98
Y = -9842103
13 feet Y = -2999873
03 meter
Z = -9628569
61 Z = -2934788
02
XDOT = 14924
170433 XDOT = 4548
887148
YDOT = 9906
990227 feet/sec YDOT = 3019
650621 meter/sec
ZDOT = 16458
591604 ZDOT = 5016
578721
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
98155864
00020000 00000-0 20000-3 0 9033
2 25544 51
6342 52
7413 0020942 283
6413 76
2419 15
76137117 19322
Satellite: ISS
Catalog Number: 25544
Epoch time: 06333
98155864 = yrday
fracday
Element set: 903
Inclination: 51
6342 deg
RA of node: 52
7413 deg
Eccentricity:
0020942
Arg of perigee: 283
6413 deg
Mean anomaly: 76
2419 deg
Mean motion: 15
76137117 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1932
Checksum: 287
Coasting Arc #5 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2006/334/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 686098
09 A = 6716197
86 meter
Y = -4716130
16 meter E =
0013587
Z = -4728708
23 I = 51
85419
XDOT = 6249
769564 Wp = 317
54537
YDOT = 3619
809562 meter/sec RA = 47
08224 deg
ZDOT = -2689
106508 TA = 286
04087
MA = 286
19047
Ha = 188
525 n
mi
Hp = 179
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2250977
98 X = 761755
21
Y = -15472867
98 feet Y = -4708034
52 meter
Z = -15514134
60 Z = -4725191
61
XDOT = 20504
493320 XDOT = 6221
891315
YDOT = 11876
015623 feet/sec YDOT = 3689
542246 meter/sec
ZDOT = -8822
527913 ZDOT = -2658
811982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12260985
93 X = -3737148
51
Y = -9722914
64 feet Y = -2963544
38 meter
Z = -15501550
66 Z = -4724872
64
XDOT = 19816
369934 XDOT = 6040
029556
YDOT = -11029
660530 feet/sec YDOT = -3361
840530 meter/sec
ZDOT = -8708
858538 ZDOT = -2654
460082
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
99600587
00020000 00000-0 20000-3 0 9043
2 25544 51
6350 47
5147 0020906 287
9749 71
9136 15
76192534 19485
Satellite: ISS
Catalog Number: 25544
Epoch time: 06334
99600587 = yrday
fracday
Element set: 904
Inclination: 51
6350 deg
RA of node: 47
5147 deg
Eccentricity:
0020906
Arg of perigee: 287
9749 deg
Mean anomaly: 71
9136 deg
Mean motion: 15
76192534 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1948
Checksum: 320
Coasting Arc #6 (Orbit 1963)
---------------------------------------
Vector Time (GMT): 2006/335/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5623941
47 A = 6724800
64 meter
Y = -3297243
33 meter E =
0006912
Z = 1659173
47 I = 51
86263
XDOT = 1222
365362 Wp = 280
89508
YDOT = -4968
457857 meter/sec RA = 41
90925 deg
ZDOT = -5749
225551 TA = 240
82976
MA = 240
89894
Ha = 188
715 n
mi
Hp = 179
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18451251
55 X = -5594713
41
Y = -10817727
46 feet Y = -3359970
08 meter
Z = 5443482
50 Z = 1631922
40
XDOT = 4010
385047 XDOT = 1305
761890
YDOT = -16300
714755 feet/sec YDOT = -4954
321903 meter/sec
ZDOT = -18862
288554 ZDOT = -5743
085005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18390758
88 X = -5605503
31
Y = 10970626
50 feet Y = 3343846
96 meter
Z = 5341231
59 Z = 1628007
39
XDOT = -11493
964155 XDOT = -3503
360274
YDOT = -10126
205954 feet/sec YDOT = -3086
467575 meter/sec
ZDOT = -18839
919139 ZDOT = -5742
407354
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
01042821
00020000 00000-0 20000-3 0 9050
2 25544 51
6350 42
2876 0020854 291
6706 68
2238 15
76187374 19649
Satellite: ISS
Catalog Number: 25544
Epoch time: 06336
01042821 = yrday
fracday
Element set: 905
Inclination: 51
6350 deg
RA of node: 42
2876 deg
Eccentricity:
0020854
Arg of perigee: 291
6706 deg
Mean anomaly: 68
2238 deg
Mean motion: 15
76187374 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1964
Checksum: 291
Coasting Arc #7 (Orbit 1979)
---------------------------------------
Vector Time (GMT): 2006/336/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1533517
36 A = 6714004
23 meter
Y = 3968389
92 meter E =
0017360
Z = 5206556
29 I = 51
80547
XDOT = -6559
248831 Wp = 293
89584
YDOT = -3885
156205 meter/sec RA = 36
79385 deg
ZDOT = 1038
889692 TA = 146
26656
MA = 146
15597
Ha = 188
903 n
mi
Hp = 179
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5031224
92 X = -1603071
63
Y = 13019651
97 feet Y = 3950851
77 meter
Z = 17081877
59 Z = 5198937
78
XDOT = -21519
845247 XDOT = -6520
363837
YDOT = -12746
575476 feet/sec YDOT = -3958
288072 meter/sec
ZDOT = 3408
430749 ZDOT = 1007
118038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9116141
65 X = 2778599
98
Y = 10614940
61 feet Y = 3235433
90 meter
Z = 17053858
82 Z = 5198016
17
XDOT = -20559
087600 XDOT = -6266
409901
YDOT = 12422
427561 feet/sec YDOT = 3786
355921 meter/sec
ZDOT = 3289
216049 ZDOT = 1002
553052
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 06337
02482267
00020000 00000-0 20000-3 0 9065
2 25544 51
6356 37
0598 0020928 295
8814 64
0192 15
76260058 19808
Satellite: ISS
Catalog Number: 25544
Epoch time: 06337
02482267 = yrday
fracday
Element set: 906
Inclination: 51
6356 deg
RA of node: 37
0598 deg
Eccentricity:
0020928
Arg of perigee: 295
8814 deg
Mean anomaly: 64
0192 deg
Mean motion: 15
76260058 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1980
Checksum: 305
Coasting Arc #8 (Orbit 1994)
---------------------------------------
Vector Time (GMT): 2006/337/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5768591
69 A = 6725656
58 meter
Y = 3430098
68 meter E =
0021428
Z = -135054
64 I = 51
82168
XDOT = -2326
107292 Wp = 332
42700
YDOT = 4164
801791 meter/sec RA = 31
64305 deg
ZDOT = 6061
184240 TA = 26
10641
MA = 25
99852
Ha = 189
114 n
mi
Hp = 178
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18925825
74 X = 5730463
19
Y = 11253604
59 feet Y = 3494393
10 meter
Z = -443092
65 Z = -107122
27
XDOT = -7631
585603 XDOT = -2401
950631
YDOT = 13664
047871 feet/sec YDOT = 4138
365009 meter/sec
ZDOT = 19885
775066 ZDOT = 6049
700133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18593281
09 X = 5667232
07
Y = -11798402
04 feet Y = -3596152
94 meter
Z = -338282
35 Z = -103108
46
XDOT = 7829
602528 XDOT = 2386
462851
YDOT = 11725
389860 feet/sec YDOT = 3573
898829 meter/sec
ZDOT = 19843
320274 ZDOT = 6048
244020
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 06337
97579531
00020000 00000-0 20000-3 0 9071
2 25544 51
6358 32
1588 0021007 299
7406 60
1668 15
76294560 19950
Satellite: ISS
Catalog Number: 25544
Epoch time: 06337
97579531 = yrday
fracday
Element set: 907
Inclination: 51
6358 deg
RA of node: 32
1588 deg
Eccentricity:
0021007
Arg of perigee: 299
7406 deg
Mean anomaly: 60
1668 deg
Mean motion: 15
76294560 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1995
Checksum: 323
Coasting Arc #9 (Orbit 2010)
---------------------------------------
Vector Time (GMT): 2006/338/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2554936
69 A = 6713587
47 meter
Y = -3335009
33 meter E =
0010530
Z = -5233147
71 I = 51
75625
XDOT = 6593
569959 Wp = 344
31707
YDOT = 3926
496233 meter/sec RA = 26
49529 deg
ZDOT = 726
437082 TA = 292
51880
MA = 292
63023
Ha = 189
359 n
mi
Hp = 178
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8382338
22 X = 2617461
50
Y = -10941631
66 feet Y = -3306088
12 meter
Z = -17169119
79 Z = -5220584
29
XDOT = 21632
447373 XDOT = 6545
644313
YDOT = 12882
205488 feet/sec YDOT = 3999
961101 meter/sec
ZDOT = 2383
323759 ZDOT = 758
353502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6143219
71 X = -1872453
37
Y = -12403284
33 feet Y = -3780521
07 meter
Z = -17122527
88 Z = -5218946
50
XDOT = 20123
042924 XDOT = 6133
503483
YDOT = -13378
555637 feet/sec YDOT = -4077
783758 meter/sec
ZDOT = 2503
087397 ZDOT = 762
941039
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 06338
99014093
00020000 00000-0 20000-3 0 9082
2 25544 51
6354 26
9312 0021018 303
7597 56
1564 15
76350157 20116
Satellite: ISS
Catalog Number: 25544
Epoch time: 06338
99014093 = yrday
fracday
Element set: 908
Inclination: 51
6354 deg
RA of node: 26
9312 deg
Eccentricity:
0021018
Arg of perigee: 303
7597 deg
Mean anomaly: 56
1564 deg
Mean motion: 15
76350157 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2011
Checksum: 280
Coasting Arc #10 (Orbit 2026)
---------------------------------------
Vector Time (GMT): 2006/339/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5631250
62 A = 6724628
54 meter
Y = -3397245
18 meter E =
0012995
Z = -1410968
04 I = 51
76723
XDOT = 3595
145531 Wp = 296
57744
YDOT = -3520
796714 meter/sec RA = 21
37068 deg
ZDOT = -5824
451414 TA = 258
91138
MA = 259
05754
Ha = 189
563 n
mi
Hp = 178
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18475231
69 X = -5585989
31
Y = -11145817
51 feet Y = -3459963
62 meter
Z = -4629160
22 Z = -1438215
66
XDOT = 11795
096885 XDOT = 3662
542845
YDOT = -11551
170321 feet/sec YDOT = -3480
215910 meter/sec
ZDOT = -19109
092565 ZDOT = -5806
822908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17877127
67 X = -5448948
52
Y = 12042199
81 feet Y = 3670462
50 meter
Z = -4731415
03 Z = -1442135
30
XDOT = -4589
124510 XDOT = -1398
765151
YDOT = -14354
046320 feet/sec YDOT = -4375
113318 meter/sec
ZDOT = -19043
577493 ZDOT = -5804
482420
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
00446210
00020000 00000-0 20000-3 0 9098
2 25544 51
6353 21
7038 0020994 307
2951 52
6299 15
76336520 20279
Satellite: ISS
Catalog Number: 25544
Epoch time: 06340
00446210 = yrday
fracday
Element set: 909
Inclination: 51
6353 deg
RA of node: 21
7038 deg
Eccentricity:
0020994
Arg of perigee: 307
2951 deg
Mean anomaly: 52
6299 deg
Mean motion: 15
76336520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2027
Checksum: 269
Coasting Arc #11 (Orbit 2042)
---------------------------------------
Vector Time (GMT): 2006/340/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3741525
40 A = 6715299
64 meter
Y = 2861044
97 meter E =
0020010
Z = 4801587
41 I = 51
70949
XDOT = -6171
577579 Wp = 331
30993
YDOT = -3849
123614 meter/sec RA = 16
18932 deg
ZDOT = -2502
621501 TA = 143
24825
MA = 143
11089
Ha = 189
758 n
mi
Hp = 178
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12275345
78 X = -3796565
30
Y = 9386630
48 feet Y = 2818896
56 meter
Z = 15753239
52 Z = 4783277
78
XDOT = -20247
957935 XDOT = -6115
920101
YDOT = -12628
358315 feet/sec YDOT = -3917
825977 meter/sec
ZDOT = -8210
700461 ZDOT = -2532
468700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3569912
28 X = 1088109
26
Y = 15105990
14 feet Y = 4604305
80 meter
Z = 15685097
69 Z = 4780817
78
XDOT = -18631
572029 XDOT = -5678
903155
YDOT = 13089
097360 feet/sec YDOT = 3989
556875 meter/sec
ZDOT = -8322
732794 ZDOT = -2536
768956
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
01875545
00020000 00000-0 20000-3 0 9109
2 25544 51
6352 16
4747 0021130 311
6187 48
3167 15
76444633 20438
Satellite: ISS
Catalog Number: 25544
Epoch time: 06341
01875545 = yrday
fracday
Element set: 910
Inclination: 51
6352 deg
RA of node: 16
4747 deg
Eccentricity:
0021130
Arg of perigee: 311
6187 deg
Mean anomaly: 48
3167 deg
Mean motion: 15
76444633 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2043
Checksum: 269
Coasting Arc #12 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2006/341/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5048836
54 A = 6721476
70 meter
Y = 3331228
52 meter E =
0016878
Z = 2910723
87 I = 51
70185
XDOT = -4940
438384 Wp = 354
27639
YDOT = 3094
019130 meter/sec RA = 11
08259 deg
ZDOT = 5047
472947 TA = 39
26365
MA = 39
14137
Ha = 189
951 n
mi
Hp = 178
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16564424
35 X = 4997071
25
Y = 10929227
41 feet Y = 3387397
50 meter
Z = 9549618
99 Z = 2935125
95
XDOT = -16208
787349 XDOT = -4999
188688
YDOT = 10150
981397 feet/sec YDOT = 3038
443088 meter/sec
ZDOT = 16559
950614 ZDOT = 5023
330073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16497854
19 X = 5028545
96
Y = -10949460
45 feet Y = -3337395
54 meter
Z = 9641240
16 Z = 2938650
00
XDOT = 2200
736002 XDOT = 670
784333
YDOT = 17763
838690 feet/sec YDOT = 5414
418033 meter/sec
ZDOT = 16470
017964 ZDOT = 5020
061475
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
03302655
00020000 00000-0 20000-3 0 9110
2 25544 51
6342 11
2452 0021124 315
7214 44
2259 15
76438790 20593
Satellite: ISS
Catalog Number: 25544
Epoch time: 06342
03302655 = yrday
fracday
Element set: 911
Inclination: 51
6342 deg
RA of node: 11
2452 deg
Eccentricity:
0021124
Arg of perigee: 315
7214 deg
Mean anomaly: 44
2259 deg
Mean motion: 15
76438790 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2059
Checksum: 255
Coasting Arc #13 (Orbit 2073)
---------------------------------------
Vector Time (GMT): 2006/342/23:24:51
420
Vector Time (MET): N/A
Weight (LBS) : 469621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4815894
58 A = 6718582
11 meter
Y = -2592208
55 meter E =
0015984
Z = -3884678
78 I = 51
66343
XDOT = 5331
458422 Wp = 331
57935
YDOT = 3795
556563 meter/sec RA = 5
88034 deg
ZDOT = 4083
729839 TA = 340
83759
MA = 340
89764
Ha = 190
233 n
mi
Hp = 178
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15800179
07 X = 4863394
12
Y = -8504621
22 feet Y = -2538088
40 meter
Z = -12745009
13 Z = -3861168
20
XDOT = 17491
661491 XDOT = 5268
781750
YDOT = 12452
613396 feet/sec YDOT = 3854
824862 meter/sec
ZDOT = 13398
063777 ZDOT = 4109
478323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1958467
76 X = -596940
97
Y = -17898731
69 feet Y = -5455533
42 meter
Z = -12657381
49 Z = -3857969
88
XDOT = 16753
391186 XDOT = 5106
433633
YDOT = -11359
894819 feet/sec YDOT = -3462
495941 meter/sec
ZDOT = 13494
778086 ZDOT = 4113
208361
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
98388095
00020000 00000-0 20000-3 0 9127
2 25544 51
6335 6
3429 0021057 319
1251 40
8333 15
76490152 20740
Satellite: ISS
Catalog Number: 25544
Epoch time: 06342
98388095 = yrday
fracday
Element set: 912
Inclination: 51
6335 deg
RA of node: 6
3429 deg
Eccentricity:
0021057
Arg of perigee: 319
1251 deg
Mean anomaly: 40
8333 deg
Mean motion: 15
76490152 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2074
Checksum: 279
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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