Date:
April 23rd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 3718)
---------------------------------------
Vector Time (GMT): 2009/112/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4802014
49 A = 6736356
51 meter
Y = -4581101
10 meter E =
0008277
Z = -1121889
99 I = 51
39979
XDOT = 2642
670778 Wp = 338
05794
YDOT = -4211
160964 meter/sec RA = 231
40682 deg
ZDOT = 5877
977042 TA = 9
62769
MA = 9
61184
Ha = 189
990 n
mi
Hp = 189
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15754640
73 X = -4744980
94
Y = -15029859
24 feet Y = -4634481
18 meter
Z = -3680741
44 Z = -1145079
75
XDOT = 8670
179717 XDOT = 2661
009752
YDOT = -13816
144896 feet/sec YDOT = -4181
506290 meter/sec
ZDOT = 19284
701581 ZDOT = 5890
860027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21512172
28 X = -6556910
11
Y = -3264055
83 feet Y = -994884
22 meter
Z = -3771685
83 Z = -1149609
84
XDOT = -1169
651876 XDOT = -356
509892
YDOT = -14656
559692 feet/sec YDOT = -4467
319394 meter/sec
ZDOT = 19334
705745 ZDOT = 5893
218311
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 09112
51648172
00010596 00000-0 82463-4 0 9007
2 25544 51
6414 232
3299 0008882 271
4805 88
5339 15
72330485 37190
Satellite: ISS
Catalog Number: 25544
Epoch time: 09112
51648172 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 232
3299 deg
Eccentricity:
0008882
Arg of perigee: 271
4805 deg
Mean anomaly: 88
5339 deg
Mean motion: 15
72330485 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3719
Checksum: 317
Coasting Arc #2 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2009/113/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1450199
20 A = 6725950
31 meter
Y = 4263162
02 meter E =
0005571
Z = -5000519
86 I = 51
38475
XDOT = -6128
761067 Wp = 43
79021
YDOT = -4265
716635 meter/sec RA = 226
29307 deg
ZDOT = -1856
582371 TA = 208
20735
MA = 208
23753
Ha = 190
802 n
mi
Hp = 190
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4757871
38 X = -1473470
74
Y = 13986752
04 feet Y = 4246814
77 meter
Z = -16405905
06 Z = -5007621
72
XDOT = -20107
483814 XDOT = -6071
586493
YDOT = -13995
133317 feet/sec YDOT = -4333
932397 meter/sec
ZDOT = -6091
149511 ZDOT = -1886
217419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4460661
14 X = 1359609
52
Y = 14052356
80 feet Y = 4283158
35 meter
Z = -16433321
75 Z = -5008876
47
XDOT = -23439
554920 XDOT = -7144
376340
YDOT = 171
025001 feet/sec YDOT = 52
128420 meter/sec
ZDOT = -6207
253283 ZDOT = -1891
970801
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 09113
53337565
00010596 00000-0 82463-4 0 9012
2 25544 51
6417 227
1210 0008973 275
3382 84
6756 15
72364137 37351
Satellite: ISS
Catalog Number: 25544
Epoch time: 09113
53337565 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 227
1210 deg
Eccentricity:
0008973
Arg of perigee: 275
3382 deg
Mean anomaly: 84
6756 deg
Mean motion: 15
72364137 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3735
Checksum: 313
Coasting Arc #3 (Orbit 3750)
---------------------------------------
Vector Time (GMT): 2009/114/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5751184
16 A = 6734791
48 meter
Y = 2796574
12 meter E =
0005622
Z = 2101472
62 I = 51
43616
XDOT = -576
149533 Wp = 126
73630
YDOT = 5335
891297 meter/sec RA = 221
11971 deg
ZDOT = -5517
194896 TA = 29
73195
MA = 29
70001
Ha = 191
012 n
mi
Hp = 189
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18868714
42 X = 5709276
15
Y = 9175111
94 feet Y = 2860652
92 meter
Z = 6894595
20 Z = 2129310
67
XDOT = -1890
254373 XDOT = -608
971408
YDOT = 17506
205043 feet/sec YDOT = 5329
264885 meter/sec
ZDOT = -18101
033122 ZDOT = -5520
073672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20556491
38 X = 6265618
57
Y = -4015864
98 feet Y = -1224035
65 meter
Z = 7003570
28 Z = 2134688
22
XDOT = 8825
543512 XDOT = 2690
025663
YDOT = 13551
008596 feet/sec YDOT = 4130
347420 meter/sec
ZDOT = -18111
871295 ZDOT = -5520
498371
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 09114
55025100
00010596 00000-0 82463-4 0 9025
2 25544 51
6416 221
9120 0008816 279
3183 80
6983 15
72387471 37513
Satellite: ISS
Catalog Number: 25544
Epoch time: 09114
55025100 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 221
9120 deg
Eccentricity:
0008816
Arg of perigee: 279
3183 deg
Mean anomaly: 80
6983 deg
Mean motion: 15
72387471 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3751
Checksum: 298
Coasting Arc #4 (Orbit 3766)
---------------------------------------
Vector Time (GMT): 2009/115/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -480075
46 A = 6727388
36 meter
Y = -4885329
47 meter E =
0001810
Z = 4601716
35 I = 51
43536
XDOT = 6812
145392 Wp = 216
89684
YDOT = 2078
470107 meter/sec RA = 216
02246 deg
ZDOT = 2916
417391 TA = 204
10986
MA = 204
11834
Ha = 191
144 n
mi
Hp = 189
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1575050
73 X = -447766
06
Y = -16027983
84 feet Y = -4890517
40 meter
Z = 15097494
58 Z = 4599462
47
XDOT = 22349
558374 XDOT = 6774
229520
YDOT = 6819
127646 feet/sec YDOT = 2154
435436 meter/sec
ZDOT = 9568
298528 ZDOT = 2949
419536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11181677
81 X = -3408175
40
Y = -11602765
25 feet Y = -3536522
85 meter
Z = 15088317
12 Z = 4598919
06
XDOT = 20917
148050 XDOT = 6375
546726
YDOT = -7543
900597 feet/sec YDOT = -2299
380902 meter/sec
ZDOT = 9697
402349 ZDOT = 2955
768236
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 09115
56710499
00010596 00000-0 82463-4 0 9030
2 25544 51
6421 216
7017 0008898 283
9822 76
0351 15
72457977 37671
Satellite: ISS
Catalog Number: 25544
Epoch time: 09115
56710499 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 216
7017 deg
Eccentricity:
0008898
Arg of perigee: 283
9822 deg
Mean anomaly: 76
0351 deg
Mean motion: 15
72457977 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3767
Checksum: 341
Coasting Arc #5 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2009/116/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5981350
86 A = 6732678
84 meter
Y = -815864
91 meter E =
0006113
Z = -2971891
65 I = 51
47757
XDOT = -1703
513394 Wp = 316
06316
YDOT = -5626
559316 meter/sec RA = 210
84061 deg
ZDOT = 4971
434337 TA = 9
56620
MA = 9
55456
Ha = 191
351 n
mi
Hp = 189
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19623854
51 X = -5957345
92
Y = -2676722
13 feet Y = -882617
49 meter
Z = -9750300
70 Z = -3000891
46
XDOT = -5588
954706 XDOT = -1664
620540
YDOT = -18459
840274 feet/sec YDOT = -5645
391784 meter/sec
ZDOT = 16310
480107 ZDOT = 4963
252667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16890133
24 X = -5148112
61
Y = 10235236
17 feet Y = 3119699
98 meter
Z = -9863681
41 Z = -3006450
09
XDOT = -15288
382747 XDOT = -4659
899061
YDOT = -9536
111449 feet/sec YDOT = -2906
606770 meter/sec
ZDOT = 16278
086320 ZDOT = 4961
560710
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 09116
52039075
00010596 00000-0 82463-4 0 9042
2 25544 51
6416 211
8187 0009016 288
6747 71
3436 15
72444799 37827
Satellite: ISS
Catalog Number: 25544
Epoch time: 09116
52039075 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 211
8187 deg
Eccentricity:
0009016
Arg of perigee: 288
6747 deg
Mean anomaly: 71
3436 deg
Mean motion: 15
72444799 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3782
Checksum: 329
Coasting Arc #6 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2009/117/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2466847
04 A = 6729429
74 meter
Y = 4772762
73 meter E =
0005919
Z = -4055251
93 I = 51
49170
XDOT = -6665
156231 Wp = 347
49478
YDOT = 176
581270 meter/sec RA = 205
75609 deg
ZDOT = -3839
923056 TA = 242
84914
MA = 242
90951
Ha = 191
613 n
mi
Hp = 189
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8093330
17 X = 2432993
92
Y = 15658670
38 feet Y = 4800159
48 meter
Z = -13304632
31 Z = -4043349
62
XDOT = -21867
310468 XDOT = -6647
981410
YDOT = 579
334876 feet/sec YDOT = 102
143929 meter/sec
ZDOT = -12598
172755 ZDOT = -3872
261276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16322761
33 X = 4975177
65
Y = 6745992
75 feet Y = 2056178
59 meter
Z = -13257761
36 Z = -4040965
66
XDOT = -15833
271244 XDOT = -4825
981075
YDOT = 13259
738966 feet/sec YDOT = 4041
568437 meter/sec
ZDOT = -12724
539734 ZDOT = -3878
439711
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 09117
53721010
00010596 00000-0 82463-4 0 9052
2 25544 51
6406 206
6093 0008934 292
5723 67
4493 15
72477463 37980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09117
53721010 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 206
6093 deg
Eccentricity:
0008934
Arg of perigee: 292
5723 deg
Mean anomaly: 67
4493 deg
Mean motion: 15
72477463 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3798
Checksum: 322
Coasting Arc #7 (Orbit 3813)
---------------------------------------
Vector Time (GMT): 2009/118/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5513146
45 A = 6730273
86 meter
Y = -1078774
44 meter E =
0006615
Z = 3708078
02 I = 51
52263
XDOT = 3878
259063 Wp = 33
88934
YDOT = 5086
600758 meter/sec RA = 200
57120 deg
ZDOT = -4277
289627 TA = 101
38718
MA = 101
31287
Ha = 191
759 n
mi
Hp = 188
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18087750
82 X = 5506786
32
Y = -3539286
21 feet Y = -1017159
12 meter
Z = 12165610
31 Z = 3734845
70
XDOT = 12723
947056 XDOT = 3841
870174
YDOT = 16688
322696 feet/sec YDOT = 5129
766641 meter/sec
ZDOT = -14033
102452 ZDOT = -4258
536716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11281680
37 X = 3438656
18
Y = -14486626
03 feet Y = -4415523
61 meter
Z = 12270155
07 Z = 3739943
26
XDOT = 19554
336853 XDOT = 5960
161873
YDOT = 3379
659931 feet/sec YDOT = 1030
120347 meter/sec
ZDOT = -13959
426759 ZDOT = -4254
833276
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 09118
55401010
00010596 00000-0 82463-4 0 9061
2 25544 51
6406 201
3990 0008983 297
8648 62
1603 15
72537869 38147
Satellite: ISS
Catalog Number: 25544
Epoch time: 09118
55401010 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 201
3990 deg
Eccentricity:
0008983
Arg of perigee: 297
8648 deg
Mean anomaly: 62
1603 deg
Mean motion: 15
72537869 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3814
Checksum: 318
Coasting Arc #8 (Orbit 3829)
---------------------------------------
Vector Time (GMT): 2009/119/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4231953
59 A = 6731338
79 meter
Y = -3973209
15 meter E =
0006795
Z = 3399108
73 I = 51
55370
XDOT = 5765
131203 Wp = 46
67931
YDOT = -2197
902736 meter/sec RA = 195
49097 deg
ZDOT = 4607
401681 TA = 353
50077
MA = 353
50958
Ha = 191
978 n
mi
Hp = 188
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13884362
18 X = -4203722
35
Y = -13035463
10 feet Y = -4020375
79 meter
Z = 11151931
55 Z = 3378617
96
XDOT = 18914
472450 XDOT = 5766
897949
YDOT = -7210
966981 feet/sec YDOT = -2133
424219 meter/sec
ZDOT = 15116
147246 ZDOT = 4635
412992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19087990
58 X = -5818019
53
Y = -366249
48 feet Y = -111632
84 meter
Z = 11071534
01 Z = 3374603
57
XDOT = 9151
133425 XDOT = 2789
265468
YDOT = -16558
152752 feet/sec YDOT = -5046
924959 meter/sec
ZDOT = 15225
485554 ZDOT = 4640
727997
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 09119
57079208
00010596 00000-0 82463-4 0 9075
2 25544 51
6400 196
1885 0008963 301
5683 58
4604 15
72557237 38303
Satellite: ISS
Catalog Number: 25544
Epoch time: 09119
57079208 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 196
1885 deg
Eccentricity:
0008963
Arg of perigee: 301
5683 deg
Mean anomaly: 58
4604 deg
Mean motion: 15
72557237 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3830
Checksum: 328
Coasting Arc #9 (Orbit 3844)
---------------------------------------
Vector Time (GMT): 2009/120/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4423107
97 A = 6728017
64 meter
Y = 2670351
43 meter E =
0002453
Z = -4309205
01 I = 51
57117
XDOT = -5697
437985 Wp = 29
18900
YDOT = -3837
353390 meter/sec RA = 190
31162 deg
ZDOT = 3473
014903 TA = 275
96437
MA = 275
99232
Ha = 192
018 n
mi
Hp = 188
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14511509
10 X = -4431706
16
Y = 8760995
49 feet Y = 2620841
91 meter
Z = -14137811
73 Z = -4330713
21
XDOT = -18692
381842 XDOT = -5670
975932
YDOT = -12589
742094 feet/sec YDOT = -3900
917777 meter/sec
ZDOT = 11394
405849 ZDOT = 3445
400648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4592960
18 X = -1399934
26
Y = 16243907
23 feet Y = 4951142
92 meter
Z = -14221703
61 Z = -4334775
26
XDOT = -21123
580966 XDOT = -6438
467478
YDOT = 3900
084716 feet/sec YDOT = 1188
745821 meter/sec
ZDOT = 11286
154897 ZDOT = 3440
020013
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 09120
52400978
00010596 00000-0 82463-4 0 9085
2 25544 51
6391 191
3041 0008905 306
5312 53
5030 15
72594064 38457
Satellite: ISS
Catalog Number: 25544
Epoch time: 09120
52400978 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 191
3041 deg
Eccentricity:
0008905
Arg of perigee: 306
5312 deg
Mean anomaly: 53
5030 deg
Mean motion: 15
72594064 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3845
Checksum: 292
Coasting Arc #10 (Orbit 3860)
---------------------------------------
Vector Time (GMT): 2009/121/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5597124
13 A = 6733156
08 meter
Y = 2631089
66 meter E =
0003973
Z = -2663737
29 I = 51
61786
XDOT = -4244
405210 Wp = 317
33574
YDOT = 3751
745773 meter/sec RA = 185
23034 deg
ZDOT = -5205
318868 TA = 252
97072
MA = 253
01425
Ha = 192
313 n
mi
Hp = 187
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18363268
15 X = 5580226
81
Y = 8632183
91 feet Y = 2693585
63 meter
Z = -8739295
58 Z = -2636587
35
XDOT = -13925
213944 XDOT = -4260
755902
YDOT = 12308
877208 feet/sec YDOT = 3704
191220 meter/sec
ZDOT = -17077
817807 ZDOT = -5225
977708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19249591
38 X = 5867275
45
Y = -6559356
36 feet Y = -1999291
82 meter
Z = -8632935
72 Z = -2631318
81
XDOT = -1895
134296 XDOT = -577
636933
YDOT = 17053
186034 feet/sec YDOT = 5197
811103 meter/sec
ZDOT = -17158
315723 ZDOT = -5229
854632
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 09121
54075795
00010596 00000-0 82463-4 0 9094
2 25544 51
6393 186
0932 0008933 311
0920 48
9470 15
72600859 38610
Satellite: ISS
Catalog Number: 25544
Epoch time: 09121
54075795 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 186
0932 deg
Eccentricity:
0008933
Arg of perigee: 311
0920 deg
Mean anomaly: 48
9470 deg
Mean motion: 15
72600859 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3861
Checksum: 324
Coasting Arc #11 (Orbit 3876)
---------------------------------------
Vector Time (GMT): 2009/122/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2916165
96 A = 6726122
49 meter
Y = -3762846
74 meter E =
0010031
Z = 4755724
27 I = 51
62484
XDOT = 6937
703000 Wp = 359
98818
YDOT = 2070
909889 meter/sec RA = 180
06170 deg
ZDOT = -2605
731186 TA = 115
65517
MA = 115
55153
Ha = 192
396 n
mi
Hp = 187
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9567473
62 X = 2934923
54
Y = -12345297
71 feet Y = -3730131
73 meter
Z = 15602769
90 Z = 4769936
46
XDOT = 22761
492783 XDOT = 6926
688290
YDOT = 6794
323782 feet/sec YDOT = 2148
429823 meter/sec
ZDOT = -8548
986832 ZDOT = -2572
054496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2006251
65 X = -611505
50
Y = -15433385
13 feet Y = -4704095
79 meter
Z = 15658062
89 Z = 4772577
57
XDOT = 19824
350384 XDOT = 6042
461997
YDOT = -11149
388365 feet/sec YDOT = -3398
333574 meter/sec
ZDOT = -8417
133867 ZDOT = -2565
542403
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 09122
55748647
00010596 00000-0 82463-4 0 9101
2 25544 51
6396 180
8825 0009120 314
7795 45
2625 15
72655857 38772
Satellite: ISS
Catalog Number: 25544
Epoch time: 09122
55748647 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 180
8825 deg
Eccentricity:
0009120
Arg of perigee: 314
7795 deg
Mean anomaly: 45
2625 deg
Mean motion: 15
72655857 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3877
Checksum: 343
Coasting Arc #12 (Orbit 3892)
---------------------------------------
Vector Time (GMT): 2009/123/12:20:31
852
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6389999
78 A = 6734645
07 meter
Y = -928652
26 meter E =
0014583
Z = 1878952
29 I = 51
68228
XDOT = 2343
751964 Wp = 30
06949
YDOT = -4686
651617 meter/sec RA = 174
97441 deg
ZDOT = 5647
951799 TA = 350
79213
MA = 350
81884
Ha = 192
802 n
mi
Hp = 187
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20964566
21 X = -6388268
16
Y = -3046759
38 feet Y = -1000099
30 meter
Z = 6164541
63 Z = 1847913
76
XDOT = 7689
474948 XDOT = 2368
547871
YDOT = -15376
153599 feet/sec YDOT = -4660
303832 meter/sec
ZDOT = 18530
025588 ZDOT = 5659
397968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16800972
10 X = -5120936
30
Y = 12961707
01 feet Y = 3950728
30 meter
Z = 6043082
03 Z = 1841931
40
XDOT = -4821
517837 XDOT = -1469
598637
YDOT = -14919
560117 feet/sec YDOT = -4547
481924 meter/sec
ZDOT = 18574
433929 ZDOT = 5661
487462
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 09123
57420189
00010596 00000-0 82463-4 0 9113
2 25544 51
6393 175
6712 0009026 321
0375 39
0136 15
72617419 38934
Satellite: ISS
Catalog Number: 25544
Epoch time: 09123
57420189 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 175
6712 deg
Eccentricity:
0009026
Arg of perigee: 321
0375 deg
Mean anomaly: 39
0136 deg
Mean motion: 15
72617419 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3893
Checksum: 307
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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