Date:
October 16th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 746)
---------------------------------------
Vector Time (GMT): 2008/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2487283
55 A = 6726200
40 meter
Y = -3690762
80 meter E =
0001546
Z = 5042117
43 I = 51
91006
XDOT = 4783
793554 Wp = 66
46474
YDOT = -5743
821516 meter/sec RA = 118
64376 deg
ZDOT = -1843
502356 TA = 41
25329
MA = 41
24162
Ha = 192
163 n
mi
Hp = 187
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8160379
11 X = -2470322
49
Y = -12108801
83 feet Y = -3718481
97 meter
Z = 16542380
02 Z = 5030075
18
XDOT = 15694
860742 XDOT = 4856
622046
YDOT = -18844
558778 feet/sec YDOT = -5689
919252 meter/sec
ZDOT = -6048
236076 ZDOT = -1820
084755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12417171
09 X = 3784753
75
Y = 7783418
36 feet Y = 2372385
92 meter
Z = 16495377
12 Z = 5027790
95
XDOT = -6287
190253 XDOT = -1916
335589
YDOT = 22664
434577 feet/sec YDOT = 6908
119659 meter/sec
ZDOT = -5958
085348 ZDOT = -1816
024414
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 08289
54459184
00020000 00000-0 20000-3 0 9006
2 25544 51
6386 119
3079 0003956 230
8121 129
2690 15
72243818 7479
Satellite: ISS
Catalog Number: 25544
Epoch time: 08289
54459184 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 119
3079 deg
Eccentricity:
0003956
Arg of perigee: 230
8121 deg
Mean anomaly: 129
2690 deg
Mean motion: 15
72243818 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 747
Checksum: 307
Coasting Arc #2 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2008/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3400003
32 A = 6736641
25 meter
Y = 5712025
18 meter E =
0009840
Z = 1064286
86 I = 51
95749
XDOT = -3638
908563 Wp = 57
30247
YDOT = -3278
766412 meter/sec RA = 113
56567 deg
ZDOT = 5937
885908 TA = 314
27776
MA = 314
35845
Ha = 191
943 n
mi
Hp = 187
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11154866
54 X = -3468793
70
Y = 18740240
11 feet Y = 5673619
77 meter
Z = 3491754
81 Z = 1047601
92
XDOT = -11938
676388 XDOT = -3630
820560
YDOT = -10757
107652 feet/sec YDOT = -3319
413488 meter/sec
ZDOT = 19481
252980 ZDOT = 5920
227186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2351293
33 X = 716674
21
Y = -21691992
56 feet Y = -6611719
33 meter
Z = 3427663
50 Z = 1044751
84
XDOT = 13854
323755 XDOT = 4222
797880
YDOT = 4587
310506 feet/sec YDOT = 1398
212242 meter/sec
ZDOT = 19412
537598 ZDOT = 5916
941460
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 08290
56154606
00020000 00000-0 20000-3 0 9012
2 25544 51
6378 114
0972 0003917 234
3586 125
7212 15
72268947 7634
Satellite: ISS
Catalog Number: 25544
Epoch time: 08290
56154606 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 114
0972 deg
Eccentricity:
0003917
Arg of perigee: 234
3586 deg
Mean anomaly: 125
7212 deg
Mean motion: 15
72268947 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 763
Checksum: 298
Coasting Arc #3 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2008/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3708929
71 A = 6725092
00 meter
Y = 1937857
28 meter E =
0012089
Z = -5274756
11 I = 51
92941
XDOT = -2864
578494 Wp = 105
97472
YDOT = 7111
161076 meter/sec RA = 108
44891 deg
ZDOT = 596
175310 TA = 169
68946
MA = 169
66464
Ha = 191
865 n
mi
Hp = 187
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12168404
55 X = 3712609
23
Y = 6357799
48 feet Y = 1979353
33 meter
Z = -17305630
29 Z = -5256728
60
XDOT = -9398
223407 XDOT = -2946
779947
YDOT = 23330
580957 feet/sec YDOT = 7078
668083 meter/sec
ZDOT = 1955
955742 ZDOT = 582
059198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13810288
78 X = -4209376
02
Y = -431429
62 feet Y = -131499
75 meter
Z = -17235611
84 Z = -5253414
49
XDOT = -1629
563898 XDOT = -496
691076
YDOT = -24098
656463 feet/sec YDOT = -7345
270490 meter/sec
ZDOT = 1901
928314 ZDOT = 579
707750
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 08291
51493082
00020000 00000-0 20000-3 0 9023
2 25544 51
6378 109
2128 0003836 236
2283 123
8514 15
72290661 7786
Satellite: ISS
Catalog Number: 25544
Epoch time: 08291
51493082 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 109
2128 deg
Eccentricity:
0003836
Arg of perigee: 236
2283 deg
Mean anomaly: 123
8514 deg
Mean motion: 15
72290661 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 778
Checksum: 291
Coasting Arc #4 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2008/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1537257
61 A = 6736870
44 meter
Y = -6551996
73 meter E =
0011553
Z = 22389
89 I = 51
97843
XDOT = 4622
999465 Wp = 152
38021
YDOT = 1059
742138 meter/sec RA = 103
35319 deg
ZDOT = -6065
757465 TA = 27
37782
MA = 27
31699
Ha = 191
597 n
mi
Hp = 187
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5043496
08 X = 1610300
07
Y = -21496052
26 feet Y = -6534397
83 meter
Z = 73457
64 Z = 30035
27
XDOT = 15167
321078 XDOT = 4640
272787
YDOT = 3476
844285 feet/sec YDOT = 1111
535988 meter/sec
ZDOT = -19900
779084 ZDOT = -6043
256347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5112914
82 X = 1558416
44
Y = 21479527
71 feet Y = 6546960
05 meter
Z = 102484
09 Z = 31237
15
XDOT = -13654
669181 XDOT = -4161
943166
YDOT = 3358
628916 feet/sec YDOT = 1023
710094 meter/sec
ZDOT = -19813
504501 ZDOT = -6039
156172
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 08292
53186222
00020000 00000-0 20000-3 0 9032
2 25544 51
6385 104
0034 0003785 244
8411 115
2359 15
72353418 7944
Satellite: ISS
Catalog Number: 25544
Epoch time: 08292
53186222 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 104
0034 deg
Eccentricity:
0003785
Arg of perigee: 244
8411 deg
Mean anomaly: 115
2359 deg
Mean motion: 15
72353418 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 794
Checksum: 278
Coasting Arc #5 (Orbit 809)
---------------------------------------
Vector Time (GMT): 2008/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4183553
79 A = 6725148
28 meter
Y = 128996
22 meter E =
0002985
Z = 5264767
75 I = 51
94358
XDOT = 591
852484 Wp = 193
09412
YDOT = -7647
174907 meter/sec RA = 98
25839 deg
ZDOT = 654
904114 TA = 250
68711
MA = 250
71939
Ha = 191
833 n
mi
Hp = 187
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13725570
18 X = -4210261
12
Y = 423215
94 feet Y = 82063
76 meter
Z = 17272860
07 Z = 5244378
76
XDOT = 1941
773240 XDOT = 674
138973
YDOT = -25089
156518 feet/sec YDOT = -7640
096410 meter/sec
ZDOT = 2148
635543 ZDOT = 657
978950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12057733
55 X = 3675197
19
Y = -6775251
56 feet Y = -2065096
67 meter
Z = 17193868
43 Z = 5240691
10
XDOT = 9410
824868 XDOT = 2868
419420
YDOT = 22252
557180 feet/sec YDOT = 6782
579428 meter/sec
ZDOT = 2159
866425 ZDOT = 658
327286
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 08293
54878688
00020000 00000-0 20000-3 0 9049
2 25544 51
6383 98
7934 0003694 244
7284 115
3495 15
72281035 8102
Satellite: ISS
Catalog Number: 25544
Epoch time: 08293
54878688 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 98
7934 deg
Eccentricity:
0003694
Arg of perigee: 244
7284 deg
Mean anomaly: 115
3495 deg
Mean motion: 15
72281035 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 810
Checksum: 323
Coasting Arc #6 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2008/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 504711
33 A = 6736363
66 meter
Y = 6621542
77 meter E =
0006495
Z = -1109024
06 I = 51
98604
XDOT = -4716
581704 Wp = 21
53031
YDOT = 1349
929606 meter/sec RA = 93
14213 deg
ZDOT = 5930
186025 TA = 326
40157
MA = 326
44274
Ha = 191
547 n
mi
Hp = 187
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1655877
05 X = 436018
17
Y = 21724221
70 feet Y = 6626802
70 meter
Z = -3638530
38 Z = -1106738
78
XDOT = -15474
349424 XDOT = -4760
134491
YDOT = 4428
902906 feet/sec YDOT = 1296
942357 meter/sec
ZDOT = 19455
990896 ZDOT = 5907
166780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11859660
10 X = -3614824
40
Y = -18278424
87 feet Y = -5571263
90 meter
Z = -3629088
99 Z = -1106146
33
XDOT = 10238
183057 XDOT = 3120
598196
YDOT = -10477
119088 feet/sec YDOT = -3193
425898 meter/sec
ZDOT = 19366
906850 ZDOT = 5903
033208
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 08294
50213931
00020000 00000-0 20000-3 0 9051
2 25544 51
6394 93
9094 0003771 246
9246 113
1519 15
72342061 8252
Satellite: ISS
Catalog Number: 25544
Epoch time: 08294
50213931 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 93
9094 deg
Eccentricity:
0003771
Arg of perigee: 246
9246 deg
Mean anomaly: 113
1519 deg
Mean motion: 15
72342061 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 825
Checksum: 285
Coasting Arc #7 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2008/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3880200
21 A = 6725854
57 meter
Y = -2185119
93 meter E =
0009656
Z = -5049097
83 I = 51
95177
XDOT = 1692
007189 Wp = 77
95079
YDOT = 7271
432552 meter/sec RA = 88
06872 deg
ZDOT = -1847
577986 TA = 174
29323
MA = 174
28222
Ha = 191
463 n
mi
Hp = 187
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12730315
64 X = 3928874
07
Y = -7169028
66 feet Y = -2141457
08 meter
Z = -16565281
60 Z = -5030129
40
XDOT = 5551
204687 XDOT = 1619
546400
YDOT = 23856
406009 feet/sec YDOT = 7289
948427 meter/sec
ZDOT = -6061
607567 ZDOT = -1839
534038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7621419
35 X = -2323008
62
Y = 12561592
84 feet Y = 3828773
50 meter
Z = -16491962
14 Z = -5026750
06
XDOT = -15708
544934 XDOT = -4787
964496
YDOT = -17442
930455 feet/sec YDOT = -5316
605203 meter/sec
ZDOT = -6029
794813 ZDOT = -1837
881459
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 08295
51903886
00020000 00000-0 20000-3 0 9069
2 25544 51
6399 88
7008 0003633 251
6498 108
4269 15
72375310 8413
Satellite: ISS
Catalog Number: 25544
Epoch time: 08295
51903886 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 88
7008 deg
Eccentricity:
0003633
Arg of perigee: 251
6498 deg
Mean anomaly: 108
4269 deg
Mean motion: 15
72375310 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 841
Checksum: 314
Coasting Arc #8 (Orbit 856)
---------------------------------------
Vector Time (GMT): 2008/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2394326
73 A = 6734922
71 meter
Y = -5924961
05 meter E =
0011145
Z = 2106816
57 I = 51
97920
XDOT = 3940
871219 Wp = 121
30537
YDOT = -3576
918177 meter/sec RA = 82
93363 deg
ZDOT = -5564
816673 TA = 35
27587
MA = 35
20216
Ha = 191
382 n
mi
Hp = 187
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7855402
66 X = -2338129
54
Y = -19438848
59 feet Y = -5951421
56 meter
Z = 6912127
87 Z = 2095321
39
XDOT = 12929
367518 XDOT = 4007
609157
YDOT = -11735
295855 feet/sec YDOT = -3532
475992 meter/sec
ZDOT = -18257
272549 ZDOT = -5545
509573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16676136
91 X = 5082886
53
Y = 12731993
68 feet Y = 3880711
67 meter
Z = 6867058
43 Z = 2093079
41
XDOT = -4335
654123 XDOT = -1321
507377
YDOT = 15513
883622 feet/sec YDOT = 4728
631728 meter/sec
ZDOT = -18182
757407 ZDOT = -5542
104458
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 08296
53592635
00020000 00000-0 20000-3 0 9079
2 25544 51
6391 83
4899 0003785 256
1110 103
9632 15
72369990 8572
Satellite: ISS
Catalog Number: 25544
Epoch time: 08296
53592635 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 83
4899 deg
Eccentricity:
0003785
Arg of perigee: 256
1110 deg
Mean anomaly: 103
9632 deg
Mean motion: 15
72369990 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 857
Checksum: 323
Coasting Arc #9 (Orbit 872)
---------------------------------------
Vector Time (GMT): 2008/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2851531
12 A = 6727446
74 meter
Y = 3964357
07 meter E =
0005640
Z = 4626059
64 I = 51
95070
XDOT = -3670
340991 Wp = 138
71558
YDOT = -6090
010784 meter/sec RA = 77
87368 deg
ZDOT = 2950
315571 TA = 282
13100
MA = 282
19418
Ha = 191
270 n
mi
Hp = 187
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9355417
07 X = -2918122
10
Y = 13006420
83 feet Y = 3932097
43 meter
Z = 15177361
04 Z = 4612044
86
XDOT = -12041
801151 XDOT = -3616
300984
YDOT = -19980
350342 feet/sec YDOT = -6130
752404 meter/sec
ZDOT = 9679
513027 ZDOT = 2932
616316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1249356
04 X = 380803
72
Y = -16023899
31 feet Y = -4884084
51 meter
Z = 15123387
84 Z = 4609608
61
XDOT = 19589
477269 XDOT = 5970
872672
YDOT = 10616
836731 feet/sec YDOT = 3236
011836 meter/sec
ZDOT = 9610
385157 ZDOT = 2929
245396
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 08297
55280131
00020000 00000-0 20000-3 0 9088
2 25544 51
6401 78
2800 0003829 260
2749 99
7981 15
72422614 8731
Satellite: ISS
Catalog Number: 25544
Epoch time: 08297
55280131 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 78
2800 deg
Eccentricity:
0003829
Arg of perigee: 260
2749 deg
Mean anomaly: 99
7981 deg
Mean motion: 15
72422614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 873
Checksum: 301
Coasting Arc #10 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2008/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3898841
08 A = 6732807
45 meter
Y = 4583490
81 meter E =
0001347
Z = -3019157
76 I = 51
96211
XDOT = -2421
552672 Wp = 25
68246
YDOT = 5340
518335 meter/sec RA = 72
72687 deg
ZDOT = 4982
525959 TA = 299
60974
MA = 299
62315
Ha = 191
242 n
mi
Hp = 187
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12791473
38 X = 3861964
73
Y = 15037699
51 feet Y = 4626883
57 meter
Z = -9905373
24 Z = -3000306
70
XDOT = -7944
726614 XDOT = -2505
295827
YDOT = 17521
385614 feet/sec YDOT = 5312
971148 meter/sec
ZDOT = 16346
869943 ZDOT = 4970
558194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18916275
27 X = -5765680
70
Y = -5777421
17 feet Y = -1760957
97 meter
Z = -9831914
94 Z = -2996767
67
XDOT = -3058
047384 XDOT = -932
092843
YDOT = -17716
793562 feet/sec YDOT = -5400
078678 meter/sec
ZDOT = 16300
946514 ZDOT = 4968
528497
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 08298
50611238
00020000 00000-0 20000-3 0 9091
2 25544 51
6411 73
3962 0003688 264
9804 95
0938 15
72409421 8881
Satellite: ISS
Catalog Number: 25544
Epoch time: 08298
50611238 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 73
3962 deg
Eccentricity:
0003688
Arg of perigee: 264
9804 deg
Mean anomaly: 95
0938 deg
Mean motion: 15
72409421 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 888
Checksum: 314
Coasting Arc #11 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2008/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1285860
70 A = 6729565
96 meter
Y = -5220192
09 meter E =
0003960
Z = -4052038
34 I = 51
94173
XDOT = 5062
367736 Wp = 53
64253
YDOT = 4278
288625 meter/sec RA = 67
67471 deg
ZDOT = -3905
526786 TA = 176
21229
MA = 176
20929
Ha = 191
169 n
mi
Hp = 187
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4218703
07 X = 1363822
64
Y = -17126614
47 feet Y = -5205377
17 meter
Z = -13294089
05 Z = -4045601
84
XDOT = 16608
818030 XDOT = 5033
123702
YDOT = 14036
380002 feet/sec YDOT = 4334
735220 meter/sec
ZDOT = -12813
408090 ZDOT = -3881
004572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5868927
95 X = 1788849
24
Y = 16653074
39 feet Y = 5075857
07 meter
Z = -13269588
56 Z = -4044570
59
XDOT = -20443
346821 XDOT = -6231
132111
YDOT = -2928
439487 feet/sec YDOT = -892
588356 meter/sec
ZDOT = -12718
001038 ZDOT = -3876
446717
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 08299
52296473
00020000 00000-0 20000-3 0 9106
2 25544 51
6413 68
1864 0003749 269
6948 90
3785 15
72426036 9043
Satellite: ISS
Catalog Number: 25544
Epoch time: 08299
52296473 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 68
1864 deg
Eccentricity:
0003749
Arg of perigee: 269
6948 deg
Mean anomaly: 90
3785 deg
Mean motion: 15
72426036 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 904
Checksum: 321
Coasting Arc #12 (Orbit 919)
---------------------------------------
Vector Time (GMT): 2008/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4800893
18 A = 6730539
29 meter
Y = -2813701
87 meter E =
0008065
Z = 3780720
78 I = 51
93310
XDOT = 409
953312 Wp = 78
38485
YDOT = -6411
884982 meter/sec RA = 62
52088 deg
ZDOT = -4242
140415 TA = 56
06907
MA = 55
99242
Ha = 191
291 n
mi
Hp = 187
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15750961
89 X = -4787439
62
Y = -9231305
36 feet Y = -2867312
82 meter
Z = 12403939
58 Z = 3757430
27
XDOT = 1344
991181 XDOT = 502
229660
YDOT = -21036
368051 feet/sec YDOT = -6406
784917 meter/sec
ZDOT = -13917
783515 ZDOT = -4239
924344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18268374
61 X = 5568200
58
Y = -1346582
46 feet Y = -410438
33 meter
Z = 12313436
59 Z = 3753135
47
XDOT = 10635
506835 XDOT = 3241
702483
YDOT = 16815
836366 feet/sec YDOT = 5125
466924 meter/sec
ZDOT = -13909
733886 ZDOT = -4239
686888
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 08300
53980575
00020000 00000-0 20000-3 0 9114
2 25544 51
6418 62
9766 0003650 273
3693 86
7051 15
72428752 9201
Satellite: ISS
Catalog Number: 25544
Epoch time: 08300
53980575 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 62
9766 deg
Eccentricity:
0003650
Arg of perigee: 273
3693 deg
Mean anomaly: 86
7051 deg
Mean motion: 15
72428752 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 920
Checksum: 297
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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