Date:
November 24th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 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
329/00:06:45
257 1
2 -1
3 6
0
N/A 5
5 0
0 195
3
000/02:41:30
514 2
2 5
9 186
1
Coasting Arc #1 (Orbit 1333)
---------------------------------------
Vector Time (GMT): 2008/326/19:31:39
464
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -77924
93 A = 6736268
54 meter
Y = 6324164
94 meter E =
0015101
Z = 2309696
97 I = 51
34066
XDOT = -5142
093510 Wp = 81
47987
YDOT = 1918
709947 meter/sec RA = 287
69249 deg
ZDOT = -5394
800570 TA = 72
46142
MA = 72
29647
Ha = 195
097 n
mi
Hp = 186
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -255659
22 X = -159857
28
Y = 20748572
62 feet Y = 6322835
35 meter
Z = 7577745
98 Z = 2309119
59
XDOT = -16870
385530 XDOT = -5136
959217
YDOT = 6294
980142 feet/sec YDOT = 1861
236962 meter/sec
ZDOT = -17699
476936 ZDOT = -5419
768786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2708348
98 X = -825504
77
Y = 20573289
06 feet Y = 6270738
51 meter
Z = 7575980
77 Z = 2309158
94
XDOT = -15886
127447 XDOT = -4842
091646
YDOT = 4501
020520 feet/sec YDOT = 1371
911055 meter/sec
ZDOT = -17796
136928 ZDOT = -5424
262536
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 08326
85007084
00020000 00000-0 20000-3 0 9000
2 25544 51
6416 288
2010 0006545 14
3071 345
8275 15
71754600 13343
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
85007084 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 288
2010 deg
Eccentricity:
0006545
Arg of perigee: 14
3071 deg
Mean anomaly: 345
8275 deg
Mean motion: 15
71754600 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1334
Checksum: 265
Coasting Arc #2 (Orbit 1349)
---------------------------------------
Vector Time (GMT): 2008/327/19:31:39
464
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4217175
20 A = 6730404
93 meter
Y = -2925183
72 meter E =
0011316
Z = 4342830
61 I = 51
31159
XDOT = 1246
423752 Wp = 74
82149
YDOT = 6812
701701 meter/sec RA = 282
59517 deg
ZDOT = 3374
062250 TA = 341
02599
MA = 341
06811
Ha = 195
111 n
mi
Hp = 186
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13835876
64 X = 4228474
49
Y = -9597059
44 feet Y = -2877961
80 meter
Z = 14248131
93 Z = 4363345
45
XDOT = 4089
316772 XDOT = 1153
759419
YDOT = 22351
383533 feet/sec YDOT = 6826
121696 meter/sec
ZDOT = 11069
758039 ZDOT = 3379
892675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14637226
44 X = 4461426
62
Y = -8186579
37 feet Y = -2495269
39 meter
Z = 14327449
75 Z = 4367006
68
XDOT = 1193
663637 XDOT = 363
828677
YDOT = 21573
045523 feet/sec YDOT = 6575
464275 meter/sec
ZDOT = 11092
876005 ZDOT = 3381
108606
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 08327
86737427
00020000 00000-0 20000-3 0 9014
2 25544 51
6404 282
9931 0006492 18
4602 341
6795 15
71713519 13502
Satellite: ISS
Catalog Number: 25544
Epoch time: 08327
86737427 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 282
9931 deg
Eccentricity:
0006492
Arg of perigee: 18
4602 deg
Mean anomaly: 341
6795 deg
Mean motion: 15
71713519 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1350
Checksum: 298
Coasting Arc #3 (Orbit 1364)
---------------------------------------
Vector Time (GMT): 2008/328/19:31:39
464
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2154874
58 A = 6733115
57 meter
Y = -5317941
48 meter E =
0009263
Z = -3524436
91 I = 51
31520
XDOT = 4204
641695 Wp = 55
33268
YDOT = -4650
067975 meter/sec RA = 277
40249 deg
ZDOT = 4459
124326 TA = 262
56204
MA = 262
66730
Ha = 195
131 n
mi
Hp = 186
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7069798
50 X = -2078126
81
Y = -17447314
58 feet Y = -5341609
24 meter
Z = -11563113
22 Z = -3534719
40
XDOT = 13794
756217 XDOT = 4234
664829
YDOT = -15256
128526 feet/sec YDOT = -4602
881592 meter/sec
ZDOT = 14629
672985 ZDOT = 4479
623705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5549412
01 X = -1691460
78
Y = -17962794
76 feet Y = -5475059
84 meter
Z = -11603381
18 Z = -3536710
58
XDOT = 13605
115831 XDOT = 4146
839305
YDOT = -13676
044761 feet/sec YDOT = -4168
458443 meter/sec
ZDOT = 14708
801474 ZDOT = 4483
242689
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 08328
82108060
00020000 00000-0 20000-3 0 9027
2 25544 51
6395 278
1106 0006311 22
3039 337
8397 15
71765546 13658
Satellite: ISS
Catalog Number: 25544
Epoch time: 08328
82108060 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 278
1106 deg
Eccentricity:
0006311
Arg of perigee: 22
3039 deg
Mean anomaly: 337
8397 deg
Mean motion: 15
71765546 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1365
Checksum: 287
Coasting Arc #4 (Orbit 1368)
---------------------------------------
Vector Time (GMT): 2008/329/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4066797
72 A = 6727039
03 meter
Y = -1283183
46 meter E =
0017752
Z = -5217236
96 I = 51
29313
XDOT = 1415
023389 Wp = 78
05579
YDOT = -7515
872180 meter/sec RA = 276
14721 deg
ZDOT = 751
311649 TA = 199
10807
MA = 199
17475
Ha = 195
295 n
mi
Hp = 186
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13342512
21 X = -4026801
63
Y = -4209919
50 feet Y = -1328436
84 meter
Z = -17116919
15 Z = -5236896
91
XDOT = 4642
465187 XDOT = 1495
312095
YDOT = -24658
373294 feet/sec YDOT = -7499
599693 meter/sec
ZDOT = 2464
933233 ZDOT = 758
380638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5459154
42 X = -1663950
27
Y = 12779869
70 feet Y = 3895304
28 meter
Z = -17193241
09 Z = -5240499
88
XDOT = -23169
807133 XDOT = -7062
157214
YDOT = -6570
515200 feet/sec YDOT = -2002
693033 meter/sec
ZDOT = 2491
774023 ZDOT = 759
492722
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 08329
07540598
00020000 00000-0 20000-3 0 9032
2 25544 51
6401 276
8047 0005833 27
7878 332
3594 15
71637158 13693
Satellite: ISS
Catalog Number: 25544
Epoch time: 08329
07540598 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 276
8047 deg
Eccentricity:
0005833
Arg of perigee: 27
7878 deg
Mean anomaly: 332
3594 deg
Mean motion: 15
71637158 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1369
Checksum: 317
Coasting Arc #5 (Orbit 1384)
---------------------------------------
Vector Time (GMT): 2008/330/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -51724
90 A = 6738908
87 meter
Y = 6735551
69 meter E =
0012537
Z = 83963
41 I = 51
33118
XDOT = -4808
132215 Wp = 107
19192
YDOT = 47
114259 meter/sec RA = 271
01155 deg
ZDOT = -6006
251782 TA = 71
89336
MA = 71
75685
Ha = 195
362 n
mi
Hp = 186
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -169701
11 X = -127446
98
Y = 22098266
69 feet Y = 6734549
88 meter
Z = 275470
51 Z = 83528
69
XDOT = -15774
711992 XDOT = -4779
123591
YDOT = 154
574341 feet/sec YDOT = -6
490418 meter/sec
ZDOT = -19705
550465 ZDOT = -6029
539883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22016366
15 X = 6710588
40
Y = 1908522
62 feet Y = 581717
70 meter
Z = 274292
45 Z = 83604
34
XDOT = -938
486114 XDOT = -286
050567
YDOT = 14019
439283 feet/sec YDOT = 4273
125093 meter/sec
ZDOT = -19795
842122 ZDOT = -6033
772679
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 08330
09277322
00020000 00000-0 20000-3 0 9049
2 25544 51
6400 271
5979 0005756 31
9382 328
2128 15
71635951 13853
Satellite: ISS
Catalog Number: 25544
Epoch time: 08330
09277322 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 271
5979 deg
Eccentricity:
0005756
Arg of perigee: 31
9382 deg
Mean anomaly: 328
2128 deg
Mean motion: 15
71635951 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1385
Checksum: 294
Coasting Arc #6 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2008/331/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4061146
66 A = 6726974
63 meter
Y = -1373872
20 meter E =
0006904
Z = 5177977
06 I = 51
29306
XDOT = 1317
950778 Wp = 65
64023
YDOT = 7527
557211 meter/sec RA = 265
87927 deg
ZDOT = 965
402932 TA = 15
12788
MA = 15
10724
Ha = 195
193 n
mi
Hp = 185
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13323971
97 X = 4051053
30
Y = -4507454
71 feet Y = -1328515
03 meter
Z = 16988113
72 Z = 5197682
02
XDOT = 4323
985491 XDOT = 1228
988566
YDOT = 24696
710010 feet/sec YDOT = 7541
797794 meter/sec
ZDOT = 3167
332454 ZDOT = 971
590335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3685642
92 X = -1123383
96
Y = -13478245
44 feet Y = -4108169
21 meter
Z = 17064416
80 Z = 5201234
24
XDOT = 23931
884034 XDOT = 7294
438253
YDOT = -2510
489600 feet/sec YDOT = -765
197230 meter/sec
ZDOT = 3191
890354 ZDOT = 972
888180
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 08331
11012470
00020000 00000-0 20000-3 0 9055
2 25544 51
6407 266
3912 0005780 34
9784 325
1756 15
71698062 14019
Satellite: ISS
Catalog Number: 25544
Epoch time: 08331
11012470 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 266
3912 deg
Eccentricity:
0005780
Arg of perigee: 34
9784 deg
Mean anomaly: 325
1756 deg
Mean motion: 15
71698062 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1401
Checksum: 276
Coasting Arc #7 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2008/332/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2286557
31 A = 6737771
19 meter
Y = -6130861
27 meter E =
0013986
Z = -1583933
75 I = 51
33233
XDOT = 4154
685474 Wp = 37
47097
YDOT = -3020
976057 meter/sec RA = 260
71582 deg
ZDOT = 5732
934891 TA = 304
99165
MA = 305
12286
Ha = 195
459 n
mi
Hp = 185
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7501828
45 X = -2210136
41
Y = -20114374
26 feet Y = -6156003
41 meter
Z = -5196633
03 Z = -1594857
20
XDOT = 13630
857855 XDOT = 4160
307435
YDOT = -9911
338770 feet/sec YDOT = -2974
485179 meter/sec
ZDOT = 18808
841506 ZDOT = 5753
132204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20425685
85 X = -6225749
05
Y = 6573429
12 feet Y = 2003581
20 meter
Z = -5239452
65 Z = -1596985
17
XDOT = -8823
024356 XDOT = -2689
257824
YDOT = -12458
907547 feet/sec YDOT = -3797
475020 meter/sec
ZDOT = 18886
935617 ZDOT = 5756
737976
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 08332
06388155
00020000 00000-0 20000-3 0 9067
2 25544 51
6407 261
5110 0005953 37
3709 322
7866 15
71646837 14166
Satellite: ISS
Catalog Number: 25544
Epoch time: 08332
06388155 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 261
5110 deg
Eccentricity:
0005953
Arg of perigee: 37
3709 deg
Mean anomaly: 322
7866 deg
Mean motion: 15
71646837 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1416
Checksum: 295
Coasting Arc #8 (Orbit 1431)
---------------------------------------
Vector Time (GMT): 2008/333/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2965852
92 A = 6728949
43 meter
Y = 3750478
09 meter E =
0016794
Z = -4750624
75 I = 51
30822
XDOT = -3722
876742 Wp = 61
91700
YDOT = -6208
217616 meter/sec RA = 255
61053 deg
ZDOT = -2576
138576 TA = 182
63927
MA = 182
64814
Ha = 195
455 n
mi
Hp = 185
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9730488
57 X = -2984492
73
Y = 12304718
16 feet Y = 3717208
60 meter
Z = -15586039
21 Z = -4765078
00
XDOT = -12214
162540 XDOT = -3640
664035
YDOT = -20368
168030 feet/sec YDOT = -6249
388970 meter/sec
ZDOT = -8451
898214 ZDOT = -2594
025836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12038682
48 X = 3669390
42
Y = 9970810
13 feet Y = 3039102
93 meter
Z = -15641808
86 Z = -4767623
34
XDOT = -19963
484324 XDOT = -6084
870022
YDOT = 10730
875750 feet/sec YDOT = 3270
770929 meter/sec
ZDOT = -8521
734570 ZDOT = -2597
424697
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 08333
08120772
00020000 00000-0 20000-3 0 9070
2 25544 51
6400 256
3048 0005802 42
2383 317
9225 15
71685889 14320
Satellite: ISS
Catalog Number: 25544
Epoch time: 08333
08120772 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 256
3048 deg
Eccentricity:
0005802
Arg of perigee: 42
2383 deg
Mean anomaly: 317
9225 deg
Mean motion: 15
71685889 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1432
Checksum: 282
Coasting Arc #9 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2008/334/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4058393
39 A = 6734971
78 meter
Y = 4528374
26 meter E =
0017699
Z = 2883153
56 I = 51
33745
XDOT = -2366
260621 Wp = 82
70521
YDOT = 5335
549866 meter/sec RA = 250
42607 deg
ZDOT = -5020
814387 TA = 64
01921
MA = 63
83700
Ha = 195
457 n
mi
Hp = 185
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13314938
94 X = 3993448
62
Y = 14856870
94 feet Y = 4573394
04 meter
Z = 9459165
22 Z = 2902712
50
XDOT = -7763
322249 XDOT = -2401
357055
YDOT = 17505
084862 feet/sec YDOT = 5308
893428 meter/sec
ZDOT = -16472
488145 ZDOT = -5032
394427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14987657
19 X = 4568237
91
Y = -13112471
97 feet Y = -3996681
46 meter
Z = 9535367
35 Z = 2906379
97
XDOT = 16471
882299 XDOT = 5020
629725
YDOT = 6748
738047 feet/sec YDOT = 2057
015357 meter/sec
ZDOT = -16516
998557 ZDOT = -5034
381160
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 08334
09851987
00020000 00000-0 20000-3 0 9082
2 25544 51
6399 251
0982 0006000 45
9942 314
1713 15
71735596 14487
Satellite: ISS
Catalog Number: 25544
Epoch time: 08334
09851987 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 251
0982 deg
Eccentricity:
0006000
Arg of perigee: 45
9942 deg
Mean anomaly: 314
1713 deg
Mean motion: 15
71735596 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1448
Checksum: 311
Coasting Arc #10 (Orbit 1463)
---------------------------------------
Vector Time (GMT): 2008/335/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1005777
12 A = 6731801
85 meter
Y = -5356829
65 meter E =
0015438
Z = 3936410
77 I = 51
33763
XDOT = 5303
911755 Wp = 83
57568
YDOT = 3926
500508 meter/sec RA = 245
33585 deg
ZDOT = 3976
523253 TA = 324
99902
MA = 325
10040
Ha = 195
415 n
mi
Hp = 185
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3299793
71 X = 1046480
64
Y = -17574900
44 feet Y = -5345355
44 meter
Z = 12914733
49 Z = 3941395
03
XDOT = 17401
285287 XDOT = 5240
293251
YDOT = 12882
219516 feet/sec YDOT = 3985
455646 meter/sec
ZDOT = 13046
336131 ZDOT = 4002
136088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17597820
82 X = -5363815
79
Y = -3097299
47 feet Y = -944056
88 meter
Z = 12933659
33 Z = 3942179
36
XDOT = 12529
823956 XDOT = 3819
090342
YDOT = -16136
241744 feet/sec YDOT = -4918
326484 meter/sec
ZDOT = 13145
985987 ZDOT = 4006
896529
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 08335
11581750
00020000 00000-0 20000-3 0 9095
2 25544 51
6396 245
8914 0005886 49
6646 310
5030 15
71762960 14648
Satellite: ISS
Catalog Number: 25544
Epoch time: 08335
11581750 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 245
8914 deg
Eccentricity:
0005886
Arg of perigee: 49
6646 deg
Mean anomaly: 310
5030 deg
Mean motion: 15
71762960 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1464
Checksum: 305
Coasting Arc #11 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2008/336/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4953509
17 A = 6731484
31 meter
Y = -2221579
18 meter E =
0011777
Z = -3989113
79 I = 51
34931
XDOT = -181
495442 Wp = 83
74212
YDOT = -6612
595278 meter/sec RA = 240
14563 deg
ZDOT = 3919
180961 TA = 226
95215
MA = 227
05083
Ha = 195
479 n
mi
Hp = 185
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16251670
50 X = -4908920
32
Y = -7288645
59 feet Y = -2276722
32 meter
Z = -13087643
66 Z = -4013070
23
XDOT = -595
457487 XDOT = -126
577734
YDOT = -21694
866396 feet/sec YDOT = -6614
318342 meter/sec
ZDOT = 12858
205251 ZDOT = 3918
431733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6890421
84 X = -2100200
58
Y = 16349845
97 feet Y = 4983433
05 meter
Z = -13180750
70 Z = -4017492
81
XDOT = -20479
587029 XDOT = -6242
178127
YDOT = 1702
924100 feet/sec YDOT = 519
051266 meter/sec
ZDOT = 12854
789657 ZDOT = 3918
139887
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 08336
06952348
00020000 00000-0 20000-3 0 9107
2 25544 51
6385 241
0106 0006061 53
6532 306
5189 15
71788765 14799
Satellite: ISS
Catalog Number: 25544
Epoch time: 08336
06952348 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 241
0106 deg
Eccentricity:
0006061
Arg of perigee: 53
6532 deg
Mean anomaly: 306
5189 deg
Mean motion: 15
71788765 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1479
Checksum: 298
Coasting Arc #12 (Orbit 1494)
---------------------------------------
Vector Time (GMT): 2008/337/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1346358
01 A = 6734918
36 meter
Y = 5942582
24 meter E =
0009367
Z = -2878849
70 I = 51
37610
XDOT = -5700
589172 Wp = 82
24246
YDOT = -1139
768434 meter/sec RA = 235
05617 deg
ZDOT = -5031
490449 TA = 130
90498
MA = 130
82382
Ha = 195
589 n
mi
Hp = 185
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4417185
08 X = 1293792
08
Y = 19496660
88 feet Y = 5957344
45 meter
Z = -9445044
93 Z = -2872435
96
XDOT = -18702
720381 XDOT = -5662
978118
YDOT = -3739
397748 feet/sec YDOT = -1203
304784 meter/sec
ZDOT = -16507
514596 ZDOT = -5059
092958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19293237
80 X = 5880578
88
Y = -5280195
05 feet Y = -1609403
45 meter
Z = -9419697
39 Z = -2871123
76
XDOT = -3345
724619 XDOT = -1019
776864
YDOT = 17340
357819 feet/sec YDOT = 5285
341063 meter/sec
ZDOT = -16614
695297 ZDOT = -5064
159126
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 08337
08679653
00020000 00000-0 20000-3 0 9116
2 25544 51
6382 235
8030 0006127 57
0535 303
1216 15
71783552 14958
Satellite: ISS
Catalog Number: 25544
Epoch time: 08337
08679653 = yrday
fracday
Element set: 911
Inclination: 51
6382 deg
RA of node: 235
8030 deg
Eccentricity:
0006127
Arg of perigee: 57
0535 deg
Mean anomaly: 303
1216 deg
Mean motion: 15
71783552 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1495
Checksum: 286
Coasting Arc #13 (Orbit 1510)
---------------------------------------
Vector Time (GMT): 2008/338/01:27:30
514
Vector Time (MET): N/A
Weight (LBS) : 611735
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4760195
97 A = 6728450
17 meter
Y = -232143
51 meter E =
0013377
Z = 4742339
73 I = 51
37284
XDOT = 2907
422130 Wp = 60
08296
YDOT = 6649
620074 meter/sec RA = 229
87496 deg
ZDOT = -2580
850415 TA = 55
37713
MA = 55
25106
Ha = 195
368 n
mi
Hp = 185
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15617440
86 X = 4739400
45
Y = -761625
70 feet Y = -179029
05 meter
Z = 15558857
40 Z = 4765414
41
XDOT = 9538
786515 XDOT = 2845
386305
YDOT = 21816
338825 feet/sec YDOT = 6681
785978 meter/sec
ZDOT = -8467
357004 ZDOT = -2566
875992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1674171
42 X = -510287
45
Y = -15456007
22 feet Y = -4710991
00 meter
Z = 15648372
67 Z = 4769623
99
XDOT = 20087
012681 XDOT = 6122
521465
YDOT = -10732
776356 feet/sec YDOT = -3271
350233 meter/sec
ZDOT = -8412
607458 ZDOT = -2564
162753
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 08338
10405414
00020000 00000-0 20000-3 0 9123
2 25544 51
6382 230
5958 0006024 59
1190 301
0564 15
71838452 15117
Satellite: ISS
Catalog Number: 25544
Epoch time: 08338
10405414 = yrday
fracday
Element set: 912
Inclination: 51
6382 deg
RA of node: 230
5958 deg
Eccentricity:
0006024
Arg of perigee: 59
1190 deg
Mean anomaly: 301
0564 deg
Mean motion: 15
71838452 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1511
Checksum: 262
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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