Date:
November 3rd 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5704 87 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 1482)
---------------------------------------
Vector Time (GMT): 2006/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 562671
22 A = 6710199
48 meter
Y = -4186331
73 meter E =
0014665
Z = 5209818
99 I = 51
51245
XDOT = 7428
759410 Wp = 154
17778
YDOT = 1931
431243 meter/sec RA = 198
94559 deg
ZDOT = 735
893878 TA = 288
73953
MA = 288
89862
Ha = 188
165 n
mi
Hp = 175
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1846034
19 X = 584132
77
Y = -13734684
14 feet Y = -4179919
50 meter
Z = 17092581
99 Z = 5212604
73
XDOT = 24372
570243 XDOT = 7403
034855
YDOT = 6336
716677 feet/sec YDOT = 2014
359938 meter/sec
ZDOT = 2414
349992 ZDOT = 771
920845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7468124
66 X = 2276284
40
Y = 11659387
85 feet Y = 3553781
42 meter
Z = 17102384
01 Z = 5212806
65
XDOT = -21900
183996 XDOT = -6675
176082
YDOT = 10222
360788 feet/sec YDOT = 3115
775568 meter/sec
ZDOT = 2549
007555 ZDOT = 776
937503
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 06305
54882443
00020000 00000-0 20000-3 0 9001
2 25544 51
6351 199
6524 0012177 162
4826 197
6761 15
77550379 14838
Satellite: ISS
Catalog Number: 25544
Epoch time: 06305
54882443 = yrday
fracday
Element set: 900
Inclination: 51
6351 deg
RA of node: 199
6524 deg
Eccentricity:
0012177
Arg of perigee: 162
4826 deg
Mean anomaly: 197
6761 deg
Mean motion: 15
77550379 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1483
Checksum: 311
Coasting Arc #2 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2006/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6392339
89 A = 6721941
75 meter
Y = -2011208
65 meter E =
0013431
Z = 543826
11 I = 51
57998
XDOT = 1914
777486 Wp = 104
63251
YDOT = -4429
578877 meter/sec RA = 193
77452 deg
ZDOT = 5998
916340 TA = 261
29332
MA = 261
44547
Ha = 188
002 n
mi
Hp = 176
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20972243
73 X = -6372017
05
Y = -6598453
57 feet Y = -2082577
69 meter
Z = 1784206
41 Z = 512820
88
XDOT = 6282
078367 XDOT = 1935
025052
YDOT = -14532
739098 feet/sec YDOT = -4408
053365 meter/sec
ZDOT = 19681
484055 ZDOT = 6008
267860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20180385
27 X = 6150981
43
Y = -8747967
52 feet Y = -2666380
50 meter
Z = 1668263
69 Z = 508486
77
XDOT = 4209
684513 XDOT = 1283
111840
YDOT = 13555
601237 feet/sec YDOT = 4131
747257 meter/sec
ZDOT = 19715
743825 ZDOT = 6009
358718
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 06306
56237257
00020000 00000-0 20000-3 0 9012
2 25544 51
6355 194
4190 0012065 166
4030 193
7462 15
77564467 14996
Satellite: ISS
Catalog Number: 25544
Epoch time: 06306
56237257 = yrday
fracday
Element set: 901
Inclination: 51
6355 deg
RA of node: 194
4190 deg
Eccentricity:
0012065
Arg of perigee: 166
4030 deg
Mean anomaly: 193
7462 deg
Mean motion: 15
77564467 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1499
Checksum: 300
Coasting Arc #3 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2006/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2784810
21 A = 6711126
30 meter
Y = 3568719
50 meter E =
0021063
Z = -4971664
12 I = 51
57197
XDOT = -6946
522683 Wp = 136
26823
YDOT = -2641
447314 meter/sec RA = 188
58534 deg
ZDOT = 1984
978211 TA = 153
01889
MA = 152
90923
Ha = 187
782 n
mi
Hp = 176
139
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9136516
43 X = -2800357
03
Y = 11708397
32 feet Y = 3537491
16 meter
Z = -16311234
00 Z = -4985230
96
XDOT = -22790
428749 XDOT = -6926
112302
YDOT = -8666
165727 feet/sec YDOT = -2719
013018 meter/sec
ZDOT = 6512
395705 ZDOT = 1951
280703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1080806
92 X = -329429
95
Y = -14756597
06 feet Y = -4497810
78 meter
Z = -16361343
30 Z = -4986937
44
XDOT = 21704
375993 XDOT = 6615
493803
YDOT = -8706
611732 feet/sec YDOT = -2653
775256 meter/sec
ZDOT = 6386
316485 ZDOT = 1946
549265
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 06307
51255411
00020000 00000-0 20000-3 0 9021
2 25544 51
6356 189
5127 0012004 170
4249 189
7147 15
77601408 15142
Satellite: ISS
Catalog Number: 25544
Epoch time: 06307
51255411 = yrday
fracday
Element set: 902
Inclination: 51
6356 deg
RA of node: 189
5127 deg
Eccentricity:
0012004
Arg of perigee: 170
4249 deg
Mean anomaly: 189
7147 deg
Mean motion: 15
77601408 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1514
Checksum: 275
Coasting Arc #4 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2006/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5510439
07 A = 6718531
01 meter
Y = 2580914
97 meter E =
0015187
Z = -2833371
37 I = 51
62475
XDOT = -4379
503542 Wp = 160
63461
YDOT = 3778
900869 meter/sec RA = 183
45935 deg
ZDOT = -5097
033985 TA = 51
94326
MA = 51
80633
Ha = 187
750 n
mi
Hp = 176
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18078868
35 X = 5494933
83
Y = 8467568
80 feet Y = 2642449
07 meter
Z = -9295837
84 Z = -2806638
44
XDOT = -14368
449940 XDOT = -4396
672960
YDOT = 12397
968731 feet/sec YDOT = 3729
830838 meter/sec
ZDOT = -16722
552445 ZDOT = -5118
352010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19048815
22 X = -5806078
88
Y = 6126884
52 feet Y = 1867474
40 meter
Z = -9195745
10 Z = -2802863
10
XDOT = 2476
266025 XDOT = 754
765884
YDOT = -17409
732114 feet/sec YDOT = -5306
486348 meter/sec
ZDOT = -16801
556002 ZDOT = -5121
114269
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 06308
52606122
00020000 00000-0 20000-3 0 9033
2 25544 51
6352 184
2795 0012063 175
1820 184
9463 15
77594056 15309
Satellite: ISS
Catalog Number: 25544
Epoch time: 06308
52606122 = yrday
fracday
Element set: 903
Inclination: 51
6352 deg
RA of node: 184
2795 deg
Eccentricity:
0012063
Arg of perigee: 175
1820 deg
Mean anomaly: 184
9463 deg
Mean motion: 15
77594056 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1530
Checksum: 284
Coasting Arc #5 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2006/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4711795
20 A = 6715719
19 meter
Y = -3048890
15 meter E =
0016018
Z = 3668805
76 I = 51
64458
XDOT = 5487
403565 Wp = 131
65277
YDOT = 3263
145188 meter/sec RA = 178
24568 deg
ZDOT = -4334
008774 TA = 4
09880
MA = 4
08570
Ha = 187
271 n
mi
Hp = 176
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15458645
68 X = 4727715
11
Y = -10002920
44 feet Y = -2996111
36 meter
Z = 12036764
30 Z = 3691735
01
XDOT = 18003
292535 XDOT = 5471
561339
YDOT = 10705
856917 feet/sec YDOT = 3324
419953 meter/sec
ZDOT = -14219
188891 ZDOT = -4307
388413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4169944
62 X = -1270999
12
Y = 17876888
49 feet Y = 5448875
61 meter
Z = 12121891
68 Z = 3694752
58
XDOT = -19152
789808 XDOT = -5837
770333
YDOT = 5110
040968 feet/sec YDOT = 1557
540487 meter/sec
ZDOT = -14119
417138 ZDOT = -4303
598344
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 06309
53954633
00020000 00000-0 20000-3 0 9049
2 25544 51
6349 179
0460 0011795 178
6062 181
5138 15
77689713 15467
Satellite: ISS
Catalog Number: 25544
Epoch time: 06309
53954633 = yrday
fracday
Element set: 904
Inclination: 51
6349 deg
RA of node: 179
0460 deg
Eccentricity:
0011795
Arg of perigee: 178
6062 deg
Mean anomaly: 181
5138 deg
Mean motion: 15
77689713 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1546
Checksum: 318
Coasting Arc #6 (Orbit 1561)
---------------------------------------
Vector Time (GMT): 2006/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3855930
53 A = 6712953
88 meter
Y = -3132693
24 meter E =
0017090
Z = 4515950
04 I = 51
66214
XDOT = 6273
246854 Wp = 153
61630
YDOT = -3224
785969 meter/sec RA = 173
13176 deg
ZDOT = 3099
858470 TA = 265
42607
MA = 265
62130
Ha = 187
320 n
mi
Hp = 176
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12650690
73 X = -3842552
12
Y = -10277864
95 feet Y = -3175737
90 meter
Z = 14816109
04 Z = 4497249
59
XDOT = 20581
518549 XDOT = 6293
781569
YDOT = -10580
006461 feet/sec YDOT = -3154
520442 meter/sec
ZDOT = 10170
139338 ZDOT = 3130
384563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16275665
28 X = 4960822
78
Y = -1688987
66 feet Y = -514803
44 meter
Z = 14745901
50 Z = 4494550
78
XDOT = -7218
115760 XDOT = -2200
081684
YDOT = 20787
607079 feet/sec YDOT = 6336
062638 meter/sec
ZDOT = 10283
602743 ZDOT = 3134
442116
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 06310
55301271
00020000 00000-0 20000-3 0 9058
2 25544 51
6339 173
8116 0011793 182
4182 177
6928 15
77664763 15629
Satellite: ISS
Catalog Number: 25544
Epoch time: 06310
55301271 = yrday
fracday
Element set: 905
Inclination: 51
6339 deg
RA of node: 173
8116 deg
Eccentricity:
0011793
Arg of perigee: 182
4182 deg
Mean anomaly: 177
6928 deg
Mean motion: 15
77664763 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1562
Checksum: 299
Coasting Arc #7 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2006/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6022014
23 A = 6720506
32 meter
Y = 2550682
42 meter E =
0006286
Z = -1565046
37 I = 51
71553
XDOT = -3182
623947 Wp = 147
51796
YDOT = -3976
923603 meter/sec RA = 167
93231 deg
ZDOT = 5770
111476 TA = 195
23460
MA = 195
25354
Ha = 187
007 n
mi
Hp = 177
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19757264
54 X = -6042485
82
Y = 8368380
65 feet Y = 2483226
60 meter
Z = -5134666
57 Z = -1594351
63
XDOT = -10441
679615 XDOT = -3165
947838
YDOT = -13047
649616 feet/sec YDOT = -4012
420762 meter/sec
ZDOT = 18930
811929 ZDOT = 5754
689991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7747050
89 X = 2361301
11
Y = -19980767
73 feet Y = -6090138
00 meter
Z = -5243683
90 Z = -1598274
85
XDOT = 15250
060746 XDOT = 4648
218515
YDOT = 964
552082 feet/sec YDOT = 293
995475 meter/sec
ZDOT = 18872
721333 ZDOT = 5752
405462
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 06311
50311596
00020000 00000-0 20000-3 0 9066
2 25544 51
6329 168
9041 0011772 187
1470 172
9529 15
77712918 15776
Satellite: ISS
Catalog Number: 25544
Epoch time: 06311
50311596 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 168
9041 deg
Eccentricity:
0011772
Arg of perigee: 187
1470 deg
Mean anomaly: 172
9529 deg
Mean motion: 15
77712918 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1577
Checksum: 304
Coasting Arc #8 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2006/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1610166
36 A = 6709448
91 meter
Y = 3851613
86 meter E =
0016655
Z = -5262802
54 I = 51
70497
XDOT = -7254
982452 Wp = 130
52103
YDOT = 2549
185875 meter/sec RA = 162
79034 deg
ZDOT = -365
407450 TA = 136
07800
MA = 135
94549
Ha = 186
796 n
mi
Hp = 177
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5282698
03 X = 1592543
72
Y = 12636528
41 feet Y = 3869521
64 meter
Z = -17266412
52 Z = -5255022
58
XDOT = -23802
435865 XDOT = -7281
173471
YDOT = 8363
470718 feet/sec YDOT = 2467
910236 meter/sec
ZDOT = -1198
843340 ZDOT = -400
716303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12893865
23 X = -3930050
12
Y = -4728298
19 feet Y = -1441185
29 meter
Z = -17236855
46 Z = -5253793
54
XDOT = 9844
586836 XDOT = 3000
630068
YDOT = -22132
425814 feet/sec YDOT = -6745
963388 meter/sec
ZDOT = -1330
285846 ZDOT = -405
471126
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 06312
51654050
00020000 00000-0 20000-3 0 9074
2 25544 51
6317 163
6688 0011770 191
0605 169
0303 15
77763552 15939
Satellite: ISS
Catalog Number: 25544
Epoch time: 06312
51654050 = yrday
fracday
Element set: 907
Inclination: 51
6317 deg
RA of node: 163
6688 deg
Eccentricity:
0011770
Arg of perigee: 191
0605 deg
Mean anomaly: 169
0303 deg
Mean motion: 15
77763552 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1593
Checksum: 285
Coasting Arc #9 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2006/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6386941
73 A = 6721152
89 meter
Y = -1822105
90 meter E =
0019619
Z = -945373
79 I = 51
77139
XDOT = 511
625910 Wp = 170
93461
YDOT = 4868
773998 meter/sec RA = 157
63953 deg
ZDOT = -5963
104849 TA = 19
39946
MA = 19
32489
Ha = 186
711 n
mi
Hp = 177
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20954533
24 X = 6411434
61
Y = -5978037
73 feet Y = -1750546
54 meter
Z = -3101620
04 Z = -914286
19
XDOT = 1678
562696 XDOT = 486
112746
YDOT = 15973
667974 feet/sec YDOT = 4874
353232 meter/sec
ZDOT = -19563
992287 ZDOT = -5960
680811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9660709
28 X = -2944584
19
Y = 19550064
75 feet Y = 5958859
74 meter
Z = -2985818
11 Z = -910077
36
XDOT = -11606
866958 XDOT = -3537
773049
YDOT = -8703
487306 feet/sec YDOT = -2652
822931 meter/sec
ZDOT = -19554
289403 ZDOT = -5960
147410
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 06313
52994530
00020000 00000-0 20000-3 0 9087
2 25544 51
6319 158
4352 0011858 195
1976 164
8834 15
77757317 16096
Satellite: ISS
Catalog Number: 25544
Epoch time: 06313
52994530 = yrday
fracday
Element set: 908
Inclination: 51
6319 deg
RA of node: 158
4352 deg
Eccentricity:
0011858
Arg of perigee: 195
1976 deg
Mean anomaly: 164
8834 deg
Mean motion: 15
77757317 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1609
Checksum: 325
Coasting Arc #10 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2006/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 672590
79 A = 6711186
89 meter
Y = -4625981
64 meter E =
0007803
Z = 4810759
64 I = 51
76420
XDOT = 7141
671006 Wp = 164
77321
YDOT = -1526
970293 meter/sec RA = 152
45467 deg
ZDOT = -2473
284204 TA = 309
29507
MA = 309
36424
Ha = 186
402 n
mi
Hp = 177
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2206662
69 X = 700899
08
Y = -15177105
11 feet Y = -4618302
50 meter
Z = 15783332
15 Z = 4814095
48
XDOT = 23430
679154 XDOT = 7170
229933
YDOT = -5009
745055 feet/sec YDOT = -1446
948268 meter/sec
ZDOT = -8114
449488 ZDOT = -2438
520289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10019240
73 X = 3053864
57
Y = 11595474
29 feet Y = 3534300
56 meter
Z = 15795165
23 Z = 4814366
36
XDOT = -10855
724962 XDOT = -3308
824968
YDOT = 20227
927450 feet/sec YDOT = 6165
472287 meter/sec
ZDOT = -7984
868023 ZDOT = -2433
787774
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 06314
54332787
00020000 00000-0 20000-3 0 9091
2 25544 51
6317 153
1999 0011788 199
5660 160
5055 15
77818241 16253
Satellite: ISS
Catalog Number: 25544
Epoch time: 06314
54332787 = yrday
fracday
Element set: 909
Inclination: 51
6317 deg
RA of node: 153
1999 deg
Eccentricity:
0011788
Arg of perigee: 199
5660 deg
Mean anomaly: 160
5055 deg
Mean motion: 15
77818241 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1625
Checksum: 316
Coasting Arc #11 (Orbit 1640)
---------------------------------------
Vector Time (GMT): 2006/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5836356
62 A = 6716672
45 meter
Y = 699855
23 meter E =
0013088
Z = 3254029
64 I = 51
80671
XDOT = 1980
510423 Wp = 141
76707
YDOT = -5719
181458 meter/sec RA = 147
34383 deg
ZDOT = 4762
021272 TA = 256
27499
MA = 256
42071
Ha = 186
178 n
mi
Hp = 177
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19148151
64 X = -5859556
38
Y = 2296112
95 feet Y = 634459
90 meter
Z = 10675950
27 Z = 3225620
02
XDOT = 6497
737608 XDOT = 2021
182636
YDOT = -18763
718693 feet/sec YDOT = -5696
807220 meter/sec
ZDOT = 15623
429370 ZDOT = 4771
741079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10653583
02 X = 3247212
10
Y = -16145484
81 feet Y = -4921143
77 meter
Z = 10569969
21 Z = 3221726
61
XDOT = 9005
594760 XDOT = 2744
905283
YDOT = 16237
656209 feet/sec YDOT = 4949
237612 meter/sec
ZDOT = 15658
953160 ZDOT = 4772
848923
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 06315
55669004
00020000 00000-0 20000-3 0 9100
2 25544 51
6308 147
9642 0011839 203
7602 156
3018 15
77867752 16411
Satellite: ISS
Catalog Number: 25544
Epoch time: 06315
55669004 = yrday
fracday
Element set: 910
Inclination: 51
6308 deg
RA of node: 147
9642 deg
Eccentricity:
0011839
Arg of perigee: 203
7602 deg
Mean anomaly: 156
3018 deg
Mean motion: 15
77867752 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1641
Checksum: 293
Coasting Arc #12 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2006/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2644039
52 A = 6716568
70 meter
Y = 5269536
77 meter E =
0010009
Z = -3228105
72 I = 51
82951
XDOT = -6026
312731 Wp = 184
11747
YDOT = -83
512340 meter/sec RA = 142
13944 deg
ZDOT = 4788
942951 TA = 138
22926
MA = 138
15282
Ha = 185
976 n
mi
Hp = 177
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8674670
33 X = -2687085
99
Y = 17288506
47 feet Y = 5239729
14 meter
Z = -10590898
02 Z = -3241054
87
XDOT = -19771
367229 XDOT = -6048
195045
YDOT = -273
990616 feet/sec YDOT = -151
024513 meter/sec
ZDOT = 15711
755089 ZDOT = 4759
613675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7936749
79 X = -2419121
34
Y = -17610760
04 feet Y = -5367759
66 meter
Z = -10638543
87 Z = -3242628
17
XDOT = 11492
306575 XDOT = 3502
855044
YDOT = -14625
611108 feet/sec YDOT = -4457
886266 meter/sec
ZDOT = 15602
225237 ZDOT = 4755
558252
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 06316
50669966
00020000 00000-0 20000-3 0 9114
2 25544 51
6303 143
0554 0011779 206
6068 153
4494 15
77880338 16563
Satellite: ISS
Catalog Number: 25544
Epoch time: 06316
50669966 = yrday
fracday
Element set: 911
Inclination: 51
6303 deg
RA of node: 143
0554 deg
Eccentricity:
0011779
Arg of perigee: 206
6068 deg
Mean anomaly: 153
4494 deg
Mean motion: 15
77880338 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1656
Checksum: 309
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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