Date:
November 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6727 44 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
There are no maneuvers
Coasting Arc #1 (Orbit 1259)
---------------------------------------
Vector Time (GMT): 2008/322/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3277768
38 A = 6735139
33 meter
Y = 5639850
27 meter E =
0012711
Z = 1659169
52 I = 51
41272
XDOT = -5017
156479 Wp = 101
52077
YDOT = -1226
538670 meter/sec RA = 311
87398 deg
ZDOT = -5707
992741 TA = 60
09685
MA = 59
97065
Ha = 192
719 n
mi
Hp = 185
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10753833
25 X = -3348650
54
Y = 18503445
78 feet Y = 5602799
86 meter
Z = 5443469
55 Z = 1643074
36
XDOT = -16460
487137 XDOT = -4975
339460
YDOT = -4024
077000 feet/sec YDOT = -1282
408958 meter/sec
ZDOT = -18727
010305 ZDOT = -5732
264989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19568613
65 X = 5964513
44
Y = 8704192
03 feet Y = 2653037
73 meter
Z = 5381467
91 Z = 1640271
42
XDOT = -1583
455524 XDOT = -482
637244
YDOT = 15266
872840 feet/sec YDOT = 4653
342842 meter/sec
ZDOT = -18821
190085 ZDOT = -5736
698738
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 08322
14744810
00020000 00000-0 20000-3 0 9003
2 25544 51
6414 312
2896 0003669 357
3653 2
7490 15
72551350 12605
Satellite: ISS
Catalog Number: 25544
Epoch time: 08322
14744810 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 312
2896 deg
Eccentricity:
0003669
Arg of perigee: 357
3653 deg
Mean anomaly: 2
7490 deg
Mean motion: 15
72551350 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1260
Checksum: 270
Coasting Arc #2 (Orbit 1275)
---------------------------------------
Vector Time (GMT): 2008/323/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4684243
71 A = 6725916
44 meter
Y = 165451
70 meter E =
0005851
Z = 4818643
32 I = 51
36487
XDOT = -2700
996650 Wp = 88
45538
YDOT = 6806
031926 meter/sec RA = 306
76609 deg
ZDOT = 2389
630981 TA = 338
13089
MA = 338
15586
Ha = 192
545 n
mi
Hp = 185
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15368253
63 X = 4658637
11
Y = 542820
55 feet Y = 217690
02 meter
Z = 15809197
24 Z = 4841337
43
XDOT = -8861
537564 XDOT = -2788
510578
YDOT = 22329
501069 feet/sec YDOT = 6775
338291 meter/sec
ZDOT = 7839
996658 ZDOT = 2376
297434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1387244
91 X = -422832
25
Y = -15223780
20 feet Y = -4640208
21 meter
Z = 15897190
29 Z = 4845463
60
XDOT = 22164
052387 XDOT = 6755
603168
YDOT = 6121
623465 feet/sec YDOT = 1865
870832 meter/sec
ZDOT = 7788
786911 ZDOT = 2374
022251
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 08323
16420520
00020000 00000-0 20000-3 0 9016
2 25544 51
6425 307
0795 0003704
0558
0605 15
72613520 12767
Satellite: ISS
Catalog Number: 25544
Epoch time: 08323
16420520 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 307
0795 deg
Eccentricity:
0003704
Arg of perigee:
0558 deg
Mean anomaly:
0605 deg
Mean motion: 15
72613520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1276
Checksum: 235
Coasting Arc #3 (Orbit 1290)
---------------------------------------
Vector Time (GMT): 2008/324/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1403790
32 A = 6733519
60 meter
Y = -6091075
22 meter E =
0008529
Z = -2495685
29 I = 51
37370
XDOT = 5515
047830 Wp = 30
54014
YDOT = -892
262584 meter/sec RA = 301
58224 deg
ZDOT = 5294
985604 TA = 301
12438
MA = 301
20802
Ha = 192
849 n
mi
Hp = 185
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4605611
29 X = 1483921
09
Y = -19983842
59 feet Y = -6074929
03 meter
Z = -8187943
85 Z = -2488671
36
XDOT = 18093
988944 XDOT = 5498
893025
YDOT = -2927
370683 feet/sec YDOT = -830
680800 meter/sec
ZDOT = 17372
000014 ZDOT = 5321
738677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20444034
94 X = -6231341
85
Y = -1744835
17 feet Y = -531825
76 meter
Z = -8161190
50 Z = -2487530
86
XDOT = -5599
386718 XDOT = -1706
693072
YDOT = -15899
002168 feet/sec YDOT = -4846
015861 meter/sec
ZDOT = 17475
656514 ZDOT = 5326
580105
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 08324
11740452
00020000 00000-0 20000-3 0 9022
2 25544 51
6427 302
1955 0003849 4
9568 355
1632 15
72583426 12919
Satellite: ISS
Catalog Number: 25544
Epoch time: 08324
11740452 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 302
1955 deg
Eccentricity:
0003849
Arg of perigee: 4
9568 deg
Mean anomaly: 355
1632 deg
Mean motion: 15
72583426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1291
Checksum: 283
Coasting Arc #4 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2008/325/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4794174
20 A = 6727601
21 meter
Y = 1706925
44 meter E =
0011761
Z = -4412389
26 I = 51
33985
XDOT = 537
068672 Wp = 53
02028
YDOT = -6938
927265 meter/sec RA = 296
48266 deg
ZDOT = -3266
885587 TA = 184
00756
MA = 184
01699
Ha = 192
847 n
mi
Hp = 185
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15728917
97 X = -4791470
16
Y = 5600149
08 feet Y = 1653329
53 meter
Z = -14476342
71 Z = -4435672
99
XDOT = 1762
036325 XDOT = 630
491097
YDOT = -22765
509400 feet/sec YDOT = -6932
398953 meter/sec
ZDOT = -10718
128565 ZDOT = -3264
049865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8032788
77 X = 2448394
02
Y = 14547051
83 feet Y = 4433941
40 meter
Z = -14566489
49 Z = -4439866
00
XDOT = -21703
086264 XDOT = -6615
100693
YDOT = 1259
201101 feet/sec YDOT = 383
804496 meter/sec
ZDOT = -10707
643388 ZDOT = -3263
689705
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 08325
13413552
00020000 00000-0 20000-3 0 9034
2 25544 51
6428 296
9852 0003733 8
3774 351
7450 15
72609313 13077
Satellite: ISS
Catalog Number: 25544
Epoch time: 08325
13413552 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 296
9852 deg
Eccentricity:
0003733
Arg of perigee: 8
3774 deg
Mean anomaly: 351
7450 deg
Mean motion: 15
72609313 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1307
Checksum: 283
Coasting Arc #5 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2008/326/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 448264
71 A = 6731641
34 meter
Y = 5900704
71 meter E =
0014148
Z = 3200073
26 I = 51
34136
XDOT = -5256
363290 Wp = 77
94076
YDOT = 2993
940322 meter/sec RA = 291
28785 deg
ZDOT = -4763
637942 TA = 64
53173
MA = 64
38542
Ha = 192
934 n
mi
Hp = 185
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1470684
74 X = 366703
13
Y = 19359267
43 feet Y = 5905261
33 meter
Z = 10498928
02 Z = 3202053
05
XDOT = -17245
286384 XDOT = -5266
310106
YDOT = 9822
638852 feet/sec YDOT = 2935
105174 meter/sec
ZDOT = -15628
733406 ZDOT = -4789
197805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18803730
72 X = 5731377
12
Y = -4815953
46 feet Y = -1467902
61 meter
Z = 10507042
50 Z = 3202546
55
XDOT = 12353
725442 XDOT = 3765
415515
YDOT = 13773
744843 feet/sec YDOT = 4198
237428 meter/sec
ZDOT = -15727
608086 ZDOT = -4793
774945
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
15085271
00020000 00000-0 20000-3 0 9041
2 25544 51
6426 291
7750 0003758 14
9140 345
2132 15
72626289 13236
Satellite: ISS
Catalog Number: 25544
Epoch time: 08326
15085271 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 291
7750 deg
Eccentricity:
0003758
Arg of perigee: 14
9140 deg
Mean anomaly: 345
2132 deg
Mean motion: 15
72626289 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1323
Checksum: 279
Coasting Arc #6 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2008/327/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4245490
62 A = 6729260
81 meter
Y = -3478147
46 meter E =
0012262
Z = 3881948
38 I = 51
32501
XDOT = 1519
066127 Wp = 82
01219
YDOT = 6378
677512 meter/sec RA = 286
19113 deg
ZDOT = 4044
628850 TA = 325
69094
MA = 325
77008
Ha = 192
784 n
mi
Hp = 185
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13928775
00 X = 4265210
12
Y = -11411244
96 feet Y = -3430561
80 meter
Z = 12736051
11 Z = 3902621
16
XDOT = 4983
812754 XDOT = 1427
977353
YDOT = 20927
419659 feet/sec YDOT = 6395
155155 meter/sec
ZDOT = 13269
779692 ZDOT = 4051
787564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13881932
93 X = -4231213
16
Y = -11378835
46 feet Y = -3468269
05 meter
Z = 12815940
24 Z = 3906298
59
XDOT = 18748
402786 XDOT = 5714
513169
YDOT = -7861
315567 feet/sec YDOT = -2396
128985 meter/sec
ZDOT = 13298
013036 ZDOT = 4053
234373
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
16755302
00020000 00000-0 20000-3 0 9053
2 25544 51
6430 286
5638 0003792 17
7320 342
3974 15
72695555 13398
Satellite: ISS
Catalog Number: 25544
Epoch time: 08327
16755302 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 286
5638 deg
Eccentricity:
0003792
Arg of perigee: 17
7320 deg
Mean anomaly: 342
3974 deg
Mean motion: 15
72695555 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1339
Checksum: 303
Coasting Arc #7 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2008/328/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2135315
62 A = 6729480
70 meter
Y = -5105324
66 meter E =
0007755
Z = -3834023
81 I = 51
31867
XDOT = 4299
822205 Wp = 75
68236
YDOT = -4878
520854 meter/sec RA = 280
99199 deg
ZDOT = 4110
259923 TA = 237
47039
MA = 237
54534
Ha = 192
924 n
mi
Hp = 185
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7005628
67 X = -2059442
91
Y = -16749752
83 feet Y = -5128778
62 meter
Z = -12578818
26 Z = -3844213
32
XDOT = 14107
028232 XDOT = 4334
087672
YDOT = -16005
645847 feet/sec YDOT = -4830
246330 meter/sec
ZDOT = 13485
104735 ZDOT = 4131
231996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14911786
25 X = -4545112
45
Y = 10308566
33 feet Y = 3142051
02 meter
Z = -12618708
84 Z = -3846182
45
XDOT = -17851
705892 XDOT = -5441
199956
YDOT = -9252
448882 feet/sec YDOT = -2820
146419 meter/sec
ZDOT = 13566
048078 ZDOT = 4134
931454
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
12069919
00020000 00000-0 20000-3 0 9063
2 25544 51
6429 281
6796 0003860 20
3100 339
8216 15
72691957 13548
Satellite: ISS
Catalog Number: 25544
Epoch time: 08328
12069919 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 281
6796 deg
Eccentricity:
0003860
Arg of perigee: 20
3100 deg
Mean anomaly: 339
8216 deg
Mean motion: 15
72691957 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1354
Checksum: 303
Coasting Arc #8 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2008/329/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3166589
70 A = 6731093
54 meter
Y = 4944556
60 meter E =
0007131
Z = -3300099
63 I = 51
31951
XDOT = -3227
280399 Wp = 63
03107
YDOT = -5183
804787 meter/sec RA = 275
89474 deg
ZDOT = -4674
788329 TA = 155
84470
MA = 155
81124
Ha = 193
005 n
mi
Hp = 185
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10389073
83 X = -3205613
47
Y = 16222298
55 feet Y = 4908927
95 meter
Z = -10827098
52 Z = -3315577
86
XDOT = -10588
190284 XDOT = -3146
364502
YDOT = -17007
233552 feet/sec YDOT = -5219
441422 meter/sec
ZDOT = -15337
232051 ZDOT = -4690
270612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18146797
92 X = 5531144
01
Y = 6363533
62 feet Y = 1939605
05 meter
Z = -10886737
47 Z = -3318277
58
XDOT = -13707
206289 XDOT = -4177
956477
YDOT = 12771
915662 feet/sec YDOT = 3892
879894 meter/sec
ZDOT = -15397
650696 ZDOT = -4693
203932
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
13737361
00020000 00000-0 20000-3 0 9079
2 25544 51
6426 276
4686 0003855 25
0001 335
1348 15
72703759 13708
Satellite: ISS
Catalog Number: 25544
Epoch time: 08329
13737361 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 276
4686 deg
Eccentricity:
0003855
Arg of perigee: 25
0001 deg
Mean anomaly: 335
1348 deg
Mean motion: 15
72703759 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1370
Checksum: 289
Coasting Arc #9 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2008/330/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3414204
47 A = 6727540
45 meter
Y = 3858302
02 meter E =
0012828
Z = 4320815
37 I = 51
30669
XDOT = -2804
907597 Wp = 58
43574
YDOT = 6312
086127 meter/sec RA = 270
69565 deg
ZDOT = -3405
996990 TA = 66
14729
MA = 66
01290
Ha = 192
962 n
mi
Hp = 184
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11201458
23 X = 3349816
22
Y = 12658471
19 feet Y = 3896121
29 meter
Z = 14175903
44 Z = 4337245
93
XDOT = -9202
452745 XDOT = -2858
735719
YDOT = 20708
943986 feet/sec YDOT = 6280
419314 meter/sec
ZDOT = -11174
530807 ZDOT = -3419
753898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9558249
57 X = 2913354
47
Y = -13875550
08 feet Y = -4229267
67 meter
Z = 14239900
73 Z = 4340321
74
XDOT = 21302
036413 XDOT = 6492
860699
YDOT = 3104
711269 feet/sec YDOT = 946
315995 meter/sec
ZDOT = -11227
395158 ZDOT = -3422
110044
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
15403297
00020000 00000-0 20000-3 0 9082
2 25544 51
6430 271
2574 0004024 28
1522 331
9857 15
72754169 13860
Satellite: ISS
Catalog Number: 25544
Epoch time: 08330
15403297 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 271
2574 deg
Eccentricity:
0004024
Arg of perigee: 28
1522 deg
Mean anomaly: 331
9857 deg
Mean motion: 15
72754169 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1386
Checksum: 284
Coasting Arc #10 (Orbit 1401)
---------------------------------------
Vector Time (GMT): 2008/331/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1654088
72 A = 6732672
53 meter
Y = -5961775
87 meter E =
0016728
Z = 2632593
95 I = 51
32480
XDOT = 4447
962163 Wp = 68
08359
YDOT = 3539
548966 meter/sec RA = 265
59370 deg
ZDOT = 5200
730798 TA = 322
01679
MA = 322
13464
Ha = 193
013 n
mi
Hp = 184
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5426800
25 X = 1707842
30
Y = -19559632
13 feet Y = -5942978
60 meter
Z = 8637119
27 Z = 2640759
74
XDOT = 14593
051715 XDOT = 4382
786844
YDOT = 11612
693459 feet/sec YDOT = 3588
923739 meter/sec
ZDOT = 17062
765085 ZDOT = 5222
181632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20285011
59 X = -6182871
53
Y = -86539
48 feet Y = -26377
23 meter
Z = 8668334
03 Z = 2642108
21
XDOT = 7421
613035 XDOT = 2262
107653
YDOT = -15543
815587 feet/sec YDOT = -4737
754991 meter/sec
ZDOT = 17146
207555 ZDOT = 5226
164063
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
17067847
00020000 00000-0 20000-3 0 9093
2 25544 51
6429 266
0466 0003964 32
5803 327
5604 15
72764052 14025
Satellite: ISS
Catalog Number: 25544
Epoch time: 08331
17067847 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 266
0466 deg
Eccentricity:
0003964
Arg of perigee: 32
5803 deg
Mean anomaly: 327
5604 deg
Mean motion: 15
72764052 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1402
Checksum: 290
Coasting Arc #11 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2008/332/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224143
86 A = 6725842
90 meter
Y = -2271361
32 meter E =
0013257
Z = -4726909
76 I = 51
30491
XDOT = 921
686406 Wp = 91
43216
YDOT = -7167
517576 meter/sec RA = 260
40209 deg
ZDOT = 2626
488852 TA = 204
49118
MA = 204
55421
Ha = 193
079 n
mi
Hp = 184
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13858739
69 X = -4175468
10
Y = -7451972
82 feet Y = -2318325
43 meter
Z = -15508234
11 Z = -4747313
22
XDOT = 3023
905533 XDOT = 989
006911
YDOT = -23515
477611 feet/sec YDOT = -7156
834638 meter/sec
ZDOT = 8617
089410 ZDOT = 2631
129230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3338026
16 X = -1017430
37
Y = 15296683
13 feet Y = 4662429
02 meter
Z = -15587525
67 Z = -4751077
82
XDOT = -22301
675629 XDOT = -6797
550732
YDOT = 3912
021999 feet/sec YDOT = 1192
384305 meter/sec
ZDOT = 8634
545337 ZDOT = 2631
809419
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
12377121
00020000 00000-0 20000-3 0 9100
2 25544 51
6421 261
1618 0004108 36
1154 324
0285 15
72789323 14173
Satellite: ISS
Catalog Number: 25544
Epoch time: 08332
12377121 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 261
1618 deg
Eccentricity:
0004108
Arg of perigee: 36
1154 deg
Mean anomaly: 324
0285 deg
Mean motion: 15
72789323 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1417
Checksum: 255
Coasting Arc #12 (Orbit 1432)
---------------------------------------
Vector Time (GMT): 2008/333/02:41:54
689
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 62295
02 A = 6733919
73 meter
Y = 6439946
59 meter E =
0007341
Z = -1968418
94 I = 51
33803
XDOT = -5041
791363 Wp = 106
95155
YDOT = -1648
498091 meter/sec RA = 255
29151 deg
ZDOT = -5572
090728 TA = 95
03148
MA = 94
94767
Ha = 193
159 n
mi
Hp = 184
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 204379
97 X = -159
70
Y = 21128433
69 feet Y = 6440294
26 meter
Z = -6458067
39 Z = -1968267
18
XDOT = -16541
310247 XDOT = -4995
914028
YDOT = -5408
458304 feet/sec YDOT = -1704
621086 meter/sec
ZDOT = -18281
137558 ZDOT = -5596
473101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20123547
34 X = 6133657
23
Y = -6442762
10 feet Y = -1963753
89 meter
Z = -6456994
26 Z = -1968091
85
XDOT = -807
052696 XDOT = -245
989662
YDOT = 15832
332275 feet/sec YDOT = 4825
694878 meter/sec
ZDOT = -18375
820355 ZDOT = -5600
950044
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
14038991
00020000 00000-0 20000-3 0 9113
2 25544 51
6419 255
9505 0004140 40
2478 319
8991 15
72796343 14331
Satellite: ISS
Catalog Number: 25544
Epoch time: 08333
14038991 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 255
9505 deg
Eccentricity:
0004140
Arg of perigee: 40
2478 deg
Mean anomaly: 319
8991 deg
Mean motion: 15
72796343 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1433
Checksum: 296
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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