Date:
November 22nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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
326/18:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 187
1
000/00:00:00
000 0
0 0
0 179
1
328/09:45:33
979 -0
5 0
6 0
6
N/A 0
0 -0
0 187
4
000/00:00:07
958 -0
3 -0
0 179
2
328/10:20:30
409 0
8 1
9 1
9
N/A -1
1 0
2 188
5
000/00:27:00
819 1
3 -0
0 179
6
328/10:45:32
231 0
3 0
3 0
3
N/A 0
2 0
0 188
5
000/00:00:04
462 -0
1 -0
0 179
6
Coasting Arc #1 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2009/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4724883
78 A = 6724995
08 meter
Y = -4757783
05 meter E =
0017468
Z = 355127
31 I = 51
43765
XDOT = 3644
325720 Wp = 32
67631
YDOT = -3161
015287 meter/sec RA = 222
77891 deg
ZDOT = 6014
998762 TA = 331
20202
MA = 331
29833
Ha = 187
226 n
mi
Hp = 179
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15501587
19 X = -4673055
42
Y = -15609524
43 feet Y = -4810329
73 meter
Z = 1165115
86 Z = 332298
83
XDOT = 11956
449214 XDOT = 3650
181618
YDOT = -10370
785061 feet/sec YDOT = -3120
230177 meter/sec
ZDOT = 19734
247907 ZDOT = 6032
717091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21379471
16 X = 6516462
81
Y = -5203549
85 feet Y = -1586041
99 meter
Z = 1074818
69 Z = 327604
74
XDOT = 2374
900456 XDOT = 723
869659
YDOT = 13938
198198 feet/sec YDOT = 4248
362811 meter/sec
ZDOT = 19804
048166 ZDOT = 6036
273881
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 09324
56276393
00016717 00000-0 10270-3 0 9006
2 25544 51
6464 223
4136 0006217 357
5893 2
5240 15
76513791 30590
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324
56276393 = yrday
fracday
Element set: 900
Inclination: 51
6464 deg
RA of node: 223
4136 deg
Eccentricity:
0006217
Arg of perigee: 357
5893 deg
Mean anomaly: 2
5240 deg
Mean motion: 15
76513791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 310
Coasting Arc #2 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2009/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3714272
62 A = 6713381
04 meter
Y = 2288371
19 meter E =
0014425
Z = -5113929
81 I = 51
42226
XDOT = -5257
376426 Wp = 75
69642
YDOT = -5445
617016 meter/sec RA = 217
59428 deg
ZDOT = 1388
435655 TA = 207
60851
MA = 207
68519
Ha = 187
207 n
mi
Hp = 179
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12185933
78 X = -3714742
63
Y = 7507779
50 feet Y = 2246833
87 meter
Z = -16777984
94 Z = -5131974
92
XDOT = -17248
610322 XDOT = -5202
836707
YDOT = -17866
197558 feet/sec YDOT = -5504
103284 meter/sec
ZDOT = 4555
235090 ZDOT = 1363
026917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -420923
19 X = -128297
39
Y = -14223029
44 feet Y = -4335179
37 meter
Z = -16849117
81 Z = -5135611
11
XDOT = 23088
350088 XDOT = 7037
329107
YDOT = -5934
293710 feet/sec YDOT = -1808
772723 meter/sec
ZDOT = 4454
709574 ZDOT = 1357
795478
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 09325
51356871
00016717 00000-0 10270-3 0 9013
2 25544 51
6466 218
5131 0006184
6471 359
4701 15
76572533 30745
Satellite: ISS
Catalog Number: 25544
Epoch time: 09325
51356871 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 218
5131 deg
Eccentricity:
0006184
Arg of perigee:
6471 deg
Mean anomaly: 359
4701 deg
Mean motion: 15
76572533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 302
Coasting Arc #3 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4344756
01 A = 6723060
20 meter
Y = 4703038
31 meter E =
0004725
Z = -2056242
08 I = 51
47939
XDOT = -4904
788868 Wp = 78
69699
YDOT = 2111
243698 meter/sec RA = 212
45603 deg
ZDOT = -5544
611073 TA = 124
30826
MA = 124
26352
Ha = 187
276 n
mi
Hp = 179
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14254448
84 X = 4301831
87
Y = 15429915
72 feet Y = 4751384
10 meter
Z = -6746201
04 Z = -2035238
86
XDOT = -16091
826995 XDOT = -4901
097574
YDOT = 6926
652552 feet/sec YDOT = 2056
416552 meter/sec
ZDOT = -18190
981211 ZDOT = -5568
429696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20439068
92 X = -6229828
21
Y = 4962924
34 feet Y = 1512699
34 meter
Z = -6663083
58 Z = -2030907
88
XDOT = 2103
132951 XDOT = 641
034923
YDOT = -15843
544480 feet/sec YDOT = -4829
112357 meter/sec
ZDOT = -18284
919774 ZDOT = -5573
243547
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 09326
52773759
00016717 00000-0 10270-3 0 9024
2 25544 51
6465 213
2853 0006061 3
3113 356
8091 15
76573281 30906
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
52773759 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 213
2853 deg
Eccentricity:
0006061
Arg of perigee: 3
3113 deg
Mean anomaly: 356
8091 deg
Mean motion: 15
76573281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 304
Coasting Arc #4 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2009/326/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4821365
76 A = 6715830
17 meter
Y = 1286487
11 meter E =
0010375
Z = -4502309
82 I = 51
45938
XDOT = -4371
334401 Wp = 78
62917
YDOT = -5519
880291 meter/sec RA = 211
00977 deg
ZDOT = 3111
914860 TA = 222
45004
MA = 222
53033
Ha = 187
139 n
mi
Hp = 179
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15818129
12 X = -4813521
47
Y = 4220758
23 feet Y = 1232615
97 meter
Z = -14771357
67 Z = -4525713
15
XDOT = -14341
648298 XDOT = -4324
402551
YDOT = -18109
843476 feet/sec YDOT = -5568
500965 meter/sec
ZDOT = 10209
694421 ZDOT = 3090
792220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16186953
15 X = -4933783
32
Y = -1809459
88 feet Y = -551523
37 meter
Z = -14863694
66 Z = -4530454
13
XDOT = -6933
963158 XDOT = -2113
471971
YDOT = -20934
839105 feet/sec YDOT = -6380
938959 meter/sec
ZDOT = 10126
066642 ZDOT = 3086
425112
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 09326
78127601
00016717 00000-0 10270-3 0 9032
2 25544 51
6435 211
9733 0005666 6
8395 353
2846 15
76603458 30948
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
78127601 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 211
9733 deg
Eccentricity:
0005666
Arg of perigee: 6
8395 deg
Mean anomaly: 353
2846 deg
Mean motion: 15
76603458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 324
Coasting Arc #5 (Orbit 3109)
---------------------------------------
Vector Time (GMT): 2009/327/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 731798
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3373075
87 A = 6719519
77 meter
Y = 4686177
44 meter E =
0008350
Z = -3448064
64 I = 51
49851
XDOT = -6115
832176 Wp = 46
31009
YDOT = 1054
929038 meter/sec RA = 205
89167 deg
ZDOT = -4550
273089 TA = 174
62094
MA = 174
61197
Ha = 187
218 n
mi
Hp = 179
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11066521
87 X = 3337173
80
Y = 15374597
92 feet Y = 4723696
65 meter
Z = -11312548
04 Z = -3431764
94
XDOT = -20065
066194 XDOT = -6105
069350
YDOT = 3461
053273 feet/sec YDOT = 986
598661 meter/sec
ZDOT = -14928
717485 ZDOT = -4579
957967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5071909
68 X = 1545918
07
Y = 18291485
54 feet Y = 5575244
79 meter
Z = -11247986
47 Z = -3428386
28
XDOT = -18596
281662 XDOT = -5668
146651
YDOT = -4093
351471 feet/sec YDOT = -1247
653528 meter/sec
ZDOT = -15045
873601 ZDOT = -4585
982274
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 09327
79541388
00016717 00000-0 10270-3 0 9047
2 25544 51
6435 206
7450 0005717 10
3740 349
7541 15
76651705 31106
Satellite: ISS
Catalog Number: 25544
Epoch time: 09327
79541388 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 206
7450 deg
Eccentricity:
0005717
Arg of perigee: 10
3740 deg
Mean anomaly: 349
7541 deg
Mean motion: 15
76651705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3110
Checksum: 307
Coasting Arc #6 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2009/328/09:45:37
958
Vector Time (MET): N/A
Weight (LBS) : 731746
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2507445
42 A = 6717338
76 meter
Y = 4639319
97 meter E =
0011950
Z = -4173604
89 I = 51
51024
XDOT = -6753
840519 Wp = 44
68305
YDOT = 347
554696 meter/sec RA = 202
61189 deg
ZDOT = -3669
273869 TA = 187
77013
MA = 187
78866
Ha = 187
350 n
mi
Hp = 179
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8226526
96 X = 2475656
26
Y = 15220866
05 feet Y = 4667182
19 meter
Z = -13692929
42 Z = -4161500
51
XDOT = -22158
269420 XDOT = -6739
400064
YDOT = 1140
271313 feet/sec YDOT = 272
110208 meter/sec
ZDOT = -12038
300095 ZDOT = -3702
049374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14664213
36 X = -4469652
23
Y = -9253300
86 feet Y = -2820406
10 meter
Z = -13644929
26 Z = -4158974
44
XDOT = 18065
228256 XDOT = 5506
281572
YDOT = -10676
720243 feet/sec YDOT = -3254
264330 meter/sec
ZDOT = -12167
697134 ZDOT = -3708
714087
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 09328
42923894
00016717 00000-0 10270-3 0 9055
2 25544 51
6459 203
4825 0005895 8
4948 351
6316 15
76572109 31200
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
42923894 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 203
4825 deg
Eccentricity:
0005895
Arg of perigee: 8
4948 deg
Mean anomaly: 351
6316 deg
Mean motion: 15
76572109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 329
Coasting Arc #7 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2009/328/10:34:00
819
Vector Time (MET): N/A
Weight (LBS) : 731742
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1366322
84 A = 6716544
39 meter
Y = -4600206
27 meter E =
0008931
Z = 4690709
39 I = 51
50381
XDOT = 7189
211731 Wp = 65
51459
YDOT = 632
721729 meter/sec RA = 202
43394 deg
ZDOT = 2714
221772 TA = 357
75422
MA = 357
75823
Ha = 188
549 n
mi
Hp = 179
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4482686
49 X = -1337567
91
Y = -15092540
27 feet Y = -4615324
78 meter
Z = 15389466
50 Z = 4684141
30
XDOT = 23586
652660 XDOT = 7168
416827
YDOT = 2075
858692 feet/sec YDOT = 712
999319 meter/sec
ZDOT = 8904
927074 ZDOT = 2749
096959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13389263
50 X = 4081047
52
Y = 8331309
32 feet Y = 2539383
08 meter
Z = 15363327
67 Z = 4682742
27
XDOT = -18454
537916 XDOT = -5624
943157
YDOT = 12980
897115 feet/sec YDOT = 3956
577441 meter/sec
ZDOT = 9042
658694 ZDOT = 2756
202370
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 09328
49264297
00016717 00000-0 10270-3 0 9068
2 25544 51
6455 203
1555 0007492 9
0784 351
0515 15
76126549 31212
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
49264297 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 203
1555 deg
Eccentricity:
0007492
Arg of perigee: 9
0784 deg
Mean anomaly: 351
0515 deg
Mean motion: 15
76126549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 314
Coasting Arc #8 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2009/328/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3520996
94 A = 6715328
07 meter
Y = -2825807
58 meter E =
0012209
Z = 4969145
86 I = 51
49989
XDOT = 6152
133256 Wp = 29
68336
YDOT = 4209
731938 meter/sec RA = 202
35575 deg
ZDOT = -1952
790783 TA = 79
27827
MA = 79
14084
Ha = 188
511 n
mi
Hp = 179
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11551827
24 X = 3528194
39
Y = -9271022
24 feet Y = -2786393
74 meter
Z = 16302971
98 Z = 4986268
42
XDOT = 20184
164227 XDOT = 6114
088487
YDOT = 13811
456488 feet/sec YDOT = 4278
316108 meter/sec
ZDOT = -6406
793906 ZDOT = -1922
995498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1762477
48 X = -537203
14
Y = 14631656
49 feet Y = 4459728
90 meter
Z = 16370453
96 Z = 4989714
37
XDOT = -23062
244242 XDOT = -7029
372045
YDOT = 4303
978140 feet/sec YDOT = 1311
852537 meter/sec
ZDOT = -6288
960565 ZDOT = -1916
875180
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 09328
49264394
00016717 00000-0 10270-3 0 9077
2 25544 51
6455 203
1557 0007504 9
8343 350
2966 15
76103453 31217
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
49264394 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 203
1557 deg
Eccentricity:
0007504
Arg of perigee: 9
8343 deg
Mean anomaly: 350
2966 deg
Mean motion: 15
76103453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 308
Coasting Arc #9 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2009/329/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5186232
41 A = 6723923
76 meter
Y = -3558027
67 meter E =
0019052
Z = 2345434
95 I = 51
55711
XDOT = 4562
769195 Wp = 53
43160
YDOT = -3075
995233 meter/sec RA = 197
23307 deg
ZDOT = 5403
901894 TA = 333
06336
MA = 333
16213
Ha = 188
798 n
mi
Hp = 179
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17015198
20 X = -5157454
35
Y = -11673319
12 feet Y = -3615862
37 meter
Z = 7694996
55 Z = 2320309
58
XDOT = 14969
715206 XDOT = 4570
574795
YDOT = -10091
847877 feet/sec YDOT = -3024
928244 meter/sec
ZDOT = 17729
336922 ZDOT = 5426
087010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20308200
33 X = 6189939
46
Y = -3857441
59 feet Y = -1175748
20 meter
Z = 7595621
42 Z = 2315145
41
XDOT = -3615
166477 XDOT = -1101
902742
YDOT = 16174
525515 feet/sec YDOT = 4929
995377 meter/sec
ZDOT = 17816
802730 ZDOT = 5430
561472
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 09329
50713650
00016717 00000-0 10270-3 0 9085
2 25544 51
6458 197
9299 0007577 14
2980 345
8397 15
76082797 31372
Satellite: ISS
Catalog Number: 25544
Epoch time: 09329
50713650 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 197
9299 deg
Eccentricity:
0007577
Arg of perigee: 14
2980 deg
Mean anomaly: 345
8397 deg
Mean motion: 15
76082797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 361
Coasting Arc #10 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2009/330/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4425327
77 A = 6717759
23 meter
Y = 2585901
86 meter E =
0011432
Z = -4349514
94 I = 51
56642
XDOT = -5651
827762 Wp = 70
18295
YDOT = -3966
013172 meter/sec RA = 192
03120 deg
ZDOT = 3403
468349 TA = 234
12675
MA = 234
23295
Ha = 188
661 n
mi
Hp = 179
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14518791
90 X = -4432785
31
Y = 8483929
99 feet Y = 2536373
70 meter
Z = -14270062
13 Z = -4371031
62
XDOT = -18542
742000 XDOT = -5623
592803
YDOT = -13011
854238 feet/sec YDOT = -4029
057501 meter/sec
ZDOT = 11166
234742 ZDOT = 3376
079674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3890131
71 X = 1185712
15
Y = -16285278
70 feet Y = -4963752
95 meter
Z = -14354916
67 Z = -4375378
60
XDOT = 21088
915862 XDOT = 6427
901555
YDOT = -4677
856036 feet/sec YDOT = -1425
810520 meter/sec
ZDOT = 11057
894997 ZDOT = 3370
446395
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 09330
45819974
00016717 00000-0 10270-3 0 9098
2 25544 51
6460 193
0310 0007517 16
5633 343
5776 15
76136865 31529
Satellite: ISS
Catalog Number: 25544
Epoch time: 09330
45819974 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 193
0310 deg
Eccentricity:
0007517
Arg of perigee: 16
5633 deg
Mean anomaly: 343
5776 deg
Mean motion: 15
76136865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 321
Coasting Arc #11 (Orbit 3167)
---------------------------------------
Vector Time (GMT): 2009/331/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4588024
97 A = 6720629
56 meter
Y = 3398283
41 meter E =
0010810
Z = -3558945
10 I = 51
60544
XDOT = -5579
198921 Wp = 45
81448
YDOT = 2873
903093 meter/sec RA = 186
92591 deg
ZDOT = -4449
198845 TA = 176
63487
MA = 176
62760
Ha = 188
728 n
mi
Hp = 179
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15052575
37 X = 4566972
89
Y = 11149223
79 feet Y = 3449471
85 meter
Z = -11676329
06 Z = -3536706
96
XDOT = -18304
458401 XDOT = -5589
306839
YDOT = 9428
815923 feet/sec YDOT = 2811
456856 meter/sec
ZDOT = -14597
109070 ZDOT = -4476
327664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18459527
77 X = -5626464
07
Y = 3489681
18 feet Y = 1063654
83 meter
Z = -11588349
17 Z = -3532128
83
XDOT = 5746
905315 XDOT = 1751
656740
YDOT = -18418
861866 feet/sec YDOT = -5614
069097 meter/sec
ZDOT = -14704
122168 ZDOT = -4481
816437
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 09331
47264622
00016717 00000-0 10270-3 0 9107
2 25544 51
6458 187
8052 0007435 19
4872 340
6575 15
76152102 31680
Satellite: ISS
Catalog Number: 25544
Epoch time: 09331
47264622 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 187
8052 deg
Eccentricity:
0007435
Arg of perigee: 19
4872 deg
Mean anomaly: 340
6575 deg
Mean motion: 15
76152102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3168
Checksum: 311
Coasting Arc #12 (Orbit 3183)
---------------------------------------
Vector Time (GMT): 2009/332/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5274583
91 A = 6720888
27 meter
Y = -2484123
72 meter E =
0017118
Z = 3337090
00 I = 51
63730
XDOT = 4777
898227 Wp = 66
38082
YDOT = 3839
994957 meter/sec RA = 181
72097 deg
ZDOT = -4667
882408 TA = 74
30746
MA = 74
11868
Ha = 188
711 n
mi
Hp = 178
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17305065
32 X = 5285758
38
Y = -8150012
22 feet Y = -2425077
91 meter
Z = 10948457
99 Z = 3362741
63
XDOT = 15675
519119 XDOT = 4757
279961
YDOT = 12598
408652 feet/sec YDOT = 3893
309193 meter/sec
ZDOT = -15314
574831 ZDOT = -4644
720640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5450058
60 X = -1661177
86
Y = 18274531
28 feet Y = 5570077
14 meter
Z = 11049664
47 Z = 3367937
73
XDOT = -18572
921649 XDOT = -5661
026519
YDOT = 3715
684475 feet/sec YDOT = 1132
540628 meter/sec
ZDOT = -15222
922415 ZDOT = -4639
946752
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 09332
48706974
00016717 00000-0 10270-3 0 9111
2 25544 51
6457 182
5791 0007647 23
5390 336
6123 15
76232530 31843
Satellite: ISS
Catalog Number: 25544
Epoch time: 09332
48706974 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 182
5791 deg
Eccentricity:
0007647
Arg of perigee: 23
5390 deg
Mean anomaly: 336
6123 deg
Mean motion: 15
76232530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3184
Checksum: 318
Coasting Arc #13 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2009/333/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3686352
20 A = 6717123
50 meter
Y = -3346188
67 meter E =
0012215
Z = 4497504
40 I = 51
65342
XDOT = 6435
430577 Wp = 74
49719
YDOT = -2866
983636 meter/sec RA = 176
61756 deg
ZDOT = 3137
882670 TA = 344
23346
MA = 344
27146
Ha = 188
952 n
mi
Hp = 178
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12094331
36 X = -3670509
25
Y = -10978309
30 feet Y = -3387323
39 meter
Z = 14755591
85 Z = 4479633
81
XDOT = 21113
617380 XDOT = 6451
767676
YDOT = -9406
114291 feet/sec YDOT = -2794
927741 meter/sec
ZDOT = 10294
890650 ZDOT = 3169
186381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16273495
69 X = 4960161
49
Y = -2012941
00 feet Y = -613544
42 meter
Z = 14684856
95 Z = 4475944
40
XDOT = -6829
681513 XDOT = -2081
686925
YDOT = 20882
302077 feet/sec YDOT = 6364
925673 meter/sec
ZDOT = 10418
418572 ZDOT = 3175
533981
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 09333
50147236
00016717 00000-0 10270-3 0 9126
2 25544 51
6449 177
3525 0007650 27
4713 332
6854 15
76213100 32005
Satellite: ISS
Catalog Number: 25544
Epoch time: 09333
50147236 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 177
3525 deg
Eccentricity:
0007650
Arg of perigee: 27
4713 deg
Mean anomaly: 332
6854 deg
Mean motion: 15
76213100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 285
Coasting Arc #14 (Orbit 3214)
---------------------------------------
Vector Time (GMT): 2009/334/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5869829
04 A = 6723824
75 meter
Y = 2534286
01 meter E =
0013944
Z = -2065342
85 I = 51
70565
XDOT = -3631
200141 Wp = 35
06809
YDOT = -3897
788549 meter/sec RA = 171
42534 deg
ZDOT = 5566
955335 TA = 301
87367
MA = 302
00929
Ha = 188
750 n
mi
Hp = 178
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19257969
29 X = -5887698
25
Y = 8314586
66 feet Y = 2468546
43 meter
Z = -6776059
23 Z = -2093902
47
XDOT = -11913
386290 XDOT = -3614
388569
YDOT = -12788
020173 feet/sec YDOT = -3938
301349 meter/sec
ZDOT = 18264
289157 ZDOT = 5549
354872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5961227
61 X = 1816982
18
Y = -20072997
16 feet Y = -6118249
53 meter
Z = -6888777
96 Z = -2099699
52
XDOT = 16057
306743 XDOT = 4894
267095
YDOT = -1442
628775 feet/sec YDOT = -439
713251 meter/sec
ZDOT = 18194
594759 ZDOT = 5545
712483
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 09334
45245187
00016717 00000-0 10270-3 0 9136
2 25544 51
6438 172
4524 0007572 29
2579 330
9008 15
76259615 32150
Satellite: ISS
Catalog Number: 25544
Epoch time: 09334
45245187 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 172
4524 deg
Eccentricity:
0007572
Arg of perigee: 29
2579 deg
Mean anomaly: 330
9008 deg
Mean motion: 15
76259615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3215
Checksum: 320
Coasting Arc #15 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2009/335/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2589555
54 A = 6714327
01 meter
Y = 3524094
47 meter E =
0019874
Z = -5111971
39 I = 51
70203
XDOT = -6953
465677 Wp = 63
03528
YDOT = 2918
278722 meter/sec RA = 166
30815 deg
ZDOT = -1506
233322 TA = 192
48742
MA = 192
53674
Ha = 188
798 n
mi
Hp = 178
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8495917
13 X = 2574789
75
Y = 11561989
74 feet Y = 3552970
53 meter
Z = -16771559
68 Z = -5099426
38
XDOT = -22813
207603 XDOT = -6978
264368
YDOT = 9574
405257 feet/sec YDOT = 2840
382512 meter/sec
ZDOT = -4941
710374 ZDOT = -1540
074037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14393864
87 X = -4387250
01
Y = -584620
52 feet Y = -178192
33 meter
Z = -16721851
02 Z = -5096820
19
XDOT = 6834
306133 XDOT = 2083
096509
YDOT = -22688
143146 feet/sec YDOT = -6915
346031 meter/sec
ZDOT = -5075
297550 ZDOT = -1546
950693
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 09335
46680945
00016717 00000-0 10270-3 0 9144
2 25544 51
6424 167
2250 0007548 33
1868 326
9769 15
76309410 32317
Satellite: ISS
Catalog Number: 25544
Epoch time: 09335
46680945 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 167
2250 deg
Eccentricity:
0007548
Arg of perigee: 33
1868 deg
Mean anomaly: 326
9769 deg
Mean motion: 15
76309410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 325
Coasting Arc #16 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2009/336/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6197229
77 A = 6725375
45 meter
Y = -2552562
31 meter E =
0014992
Z = 523856
58 I = 51
76901
XDOT = 2265
985594 Wp = 99
19107
YDOT = 4236
815415 meter/sec RA = 161
14404 deg
ZDOT = -6019
034709 TA = 75
11591
MA = 74
94993
Ha = 188
822 n
mi
Hp = 178
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20332118
68 X = 6222767
52
Y = -8374548
26 feet Y = -2483118
53 meter
Z = 1718689
56 Z = 554025
03
XDOT = 7434
335938 XDOT = 2247
680401
YDOT = 13900
313042 feet/sec YDOT = 4262
053586 meter/sec
ZDOT = -19747
489203 ZDOT = -6008
070110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5898838
42 X = -1797965
95
Y = 21173289
45 feet Y = 6453618
62 meter
Z = 1837803
50 Z = 560162
51
XDOT = -14058
951641 XDOT = -4285
168460
YDOT = -2168
404641 feet/sec YDOT = -660
929735 meter/sec
ZDOT = -19703
994535 ZDOT = -6005
777534
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 09336
48114501
00016717 00000-0 10270-3 0 9158
2 25544 51
6427 161
9984 0007584 37
0324 323
1362 15
76344207 32473
Satellite: ISS
Catalog Number: 25544
Epoch time: 09336
48114501 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 161
9984 deg
Eccentricity:
0007584
Arg of perigee: 37
0324 deg
Mean anomaly: 323
1362 deg
Mean motion: 15
76344207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 305
Coasting Arc #17 (Orbit 3262)
---------------------------------------
Vector Time (GMT): 2009/337/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1373795
82 A = 6713408
64 meter
Y = -3928150
36 meter E =
0009620
Z = 5262007
58 I = 51
75609
XDOT = 7133
213395 Wp = 49
94380
YDOT = -2912
308951 meter/sec RA = 156
00137 deg
ZDOT = -305
302582 TA = 42
98346
MA = 42
90834
Ha = 188
879 n
mi
Hp = 178
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4507204
14 X = -1355330
73
Y = -12887632
43 feet Y = -3943410
58 meter
Z = 17263804
39 Z = 5255377
78
XDOT = 23402
931086 XDOT = 7166
732310
YDOT = -9554
819392 feet/sec YDOT = -2832
353688 meter/sec
ZDOT = -1001
648892 ZDOT = -270
567940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13066958
19 X = 3982808
86
Y = 4070601
09 feet Y = 1240719
21 meter
Z = 17237450
83 Z = 5253975
01
XDOT = -6150
680997 XDOT = -1874
727568
YDOT = 23494
581811 feet/sec YDOT = 7161
148536 meter/sec
ZDOT = -864
480332 ZDOT = -263
493605
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 09337
49545828
00016717 00000-0 10270-3 0 9161
2 25544 51
6420 156
7704 0007522 40
9097 319
2631 15
76354098 32632
Satellite: ISS
Catalog Number: 25544
Epoch time: 09337
49545828 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 156
7704 deg
Eccentricity:
0007522
Arg of perigee: 40
9097 deg
Mean anomaly: 319
2631 deg
Mean motion: 15
76354098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3263
Checksum: 327
Coasting Arc #18 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2009/338/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6150331
02 A = 6724896
67 meter
Y = 2477758
19 meter E =
0021179
Z = 1055005
64 I = 51
82151
XDOT = -917
235981 Wp = 52
20546
YDOT = -4833
796236 meter/sec RA = 150
87005 deg
ZDOT = 5937
711909 TA = 319
32521
MA = 319
48320
Ha = 188
828 n
mi
Hp = 177
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20178251
37 X = -6182705
71
Y = 8129127
90 feet Y = 2408800
38 meter
Z = 3461304
58 Z = 1025048
80
XDOT = -3009
304401 XDOT = -891
960042
YDOT = -15858
911537 feet/sec YDOT = -4843
912916 meter/sec
ZDOT = 19480
682116 ZDOT = 5933
316573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5292890
76 X = 1613273
10
Y = -21119539
68 feet Y = -6437235
70 meter
Z = 3342982
07 Z = 1018940
94
XDOT = 13126
322766 XDOT = 4000
903179
YDOT = 6406
821203 feet/sec YDOT = 1952
799103 meter/sec
ZDOT = 19463
124621 ZDOT = 5932
360384
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 09338
50974837
00016717 00000-0 10270-3 0 9171
2 25544 51
6412 151
5423 0007510 44
4532 315
7234 15
76405795 32792
Satellite: ISS
Catalog Number: 25544
Epoch time: 09338
50974837 = yrday
fracday
Element set: 917
Inclination: 51
6412 deg
RA of node: 151
5423 deg
Eccentricity:
0007510
Arg of perigee: 44
4532 deg
Mean anomaly: 315
7234 deg
Mean motion: 15
76405795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 317
Coasting Arc #19 (Orbit 3293)
---------------------------------------
Vector Time (GMT): 2009/339/10:45:34
462
Vector Time (MET): N/A
Weight (LBS) : 731713
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 246422
62 A = 6714575
43 meter
Y = 4545646
96 meter E =
0018085
Z = -4950711
44 I = 51
81268
XDOT = -6890
966080 Wp = 85
35105
YDOT = 2678
144737 meter/sec RA = 145
70086 deg
ZDOT = 2124
072713 TA = 205
17279
MA = 205
26104
Ha = 188
824 n
mi
Hp = 177
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 808473
18 X = 219623
85
Y = 14913539
88 feet Y = 4548253
44 meter
Z = -16242491
59 Z = -4949578
78
XDOT = -22608
156429 XDOT = -6930
719810
YDOT = 8786
564099 feet/sec YDOT = 2600
863324 meter/sec
ZDOT = 6968
742497 ZDOT = 2090
500064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12733372
91 X = -3881132
06
Y = -7815338
94 feet Y = -2382115
31 meter
Z = -16237842
38 Z = -4949294
36
XDOT = 5226
099649 XDOT = 1592
915173
YDOT = -22663
197365 feet/sec YDOT = -6907
742557 meter/sec
ZDOT = 6836
114431 ZDOT = 2083
647679
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 09339
46062550
00016717 00000-0 10270-3 0 9188
2 25544 51
6410 146
6409 0007544 48
7561 311
4252 15
76444230 32942
Satellite: ISS
Catalog Number: 25544
Epoch time: 09339
46062550 = yrday
fracday
Element set: 918
Inclination: 51
6410 deg
RA of node: 146
6409 deg
Eccentricity:
0007544
Arg of perigee: 48
7561 deg
Mean anomaly: 311
4252 deg
Mean motion: 15
76444230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3294
Checksum: 304
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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