Date:
February 7th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
040/21:39:00
446 0
4 1
9 1
9
N/A 1
7 0
1 191
5
000/00:05:00
892 -0
8 -0
0 188
5
Coasting Arc #1 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2011/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4244931
52 A = 6725832
25 meter
Y = -1174666
19 meter E =
0003518
Z = 5083898
13 I = 51
88628
XDOT = 3808
832265 Wp = 179
34884
YDOT = -6474
614280 meter/sec RA = 130
57687 deg
ZDOT = 1680
829730 TA = 254
51884
MA = 254
55769
Ha = 191
312 n
mi
Hp = 187
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13926940
69 X = -4256176
51
Y = -3853891
69 feet Y = -1222198
55 meter
Z = 16679455
81 Z = 5063249
62
XDOT = 12496
168850 XDOT = 3872
784656
YDOT = -21242
172835 feet/sec YDOT = -6431
664074 meter/sec
ZDOT = 5514
533234 ZDOT = 1699
487608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6419530
85 X = -1956673
00
Y = -13052731
85 feet Y = -3978472
67 meter
Z = 16596150
74 Z = 5058506
75
XDOT = 23211
582011 XDOT = 7074
890197
YDOT = -4293
926873 feet/sec YDOT = -1308
788911 meter/sec
ZDOT = 5589
912779 ZDOT = 1703
805415
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 11033
55057394
00016717 00000-0 10270-3 0 9003
2 25544 51
6453 131
2635 0004208 263
2373 96
8311 15
72326504 19718
Satellite: ISS
Catalog Number: 25544
Epoch time: 11033
55057394 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 131
2635 deg
Eccentricity:
0004208
Arg of perigee: 263
2373 deg
Mean anomaly: 96
8311 deg
Mean motion: 15
72326504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 285
Coasting Arc #2 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2011/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2349258
19 A = 6735295
00 meter
Y = 5986992
49 meter E =
0005208
Z = -1989415
96 I = 51
93687
XDOT = -5257
857493 Wp = 1
44480
YDOT = -198
405967 meter/sec RA = 125
44250 deg
ZDOT = 5617
206633 TA = 336
51021
MA = 336
53399
Ha = 191
191 n
mi
Hp = 187
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7707540
00 X = -2406367
37
Y = 19642363
80 feet Y = 5960402
34 meter
Z = -6526955
24 Z = -2000966
99
XDOT = -17250
188625 XDOT = -5282
534563
YDOT = -650
938211 feet/sec YDOT = -257
340479 meter/sec
ZDOT = 18429
155621 ZDOT = 5591
604883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19657693
16 X = -5991664
88
Y = 7628364
11 feet Y = 2325125
38 meter
Z = -6573654
51 Z = -2003649
89
XDOT = -10700
705261 XDOT = -3261
574963
YDOT = -11797
962363 feet/sec YDOT = -3596
018928 meter/sec
ZDOT = 18325
841121 ZDOT = 5585
716374
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 11034
50394218
00016717 00000-0 10270-3 0 9019
2 25544 51
6452 126
3811 0004214 270
4396 89
6283 15
72292259 19863
Satellite: ISS
Catalog Number: 25544
Epoch time: 11034
50394218 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 126
3811 deg
Eccentricity:
0004214
Arg of perigee: 270
4396 deg
Mean anomaly: 89
6283 deg
Mean motion: 15
72292259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 306
Coasting Arc #3 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2011/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4755850
46 A = 6727496
55 meter
Y = -850408
35 meter E =
0007161
Z = -4688557
39 I = 51
92696
XDOT = -1533
820468 Wp = 58
02483
YDOT = 6988
820728 meter/sec RA = 120
38016 deg
ZDOT = -2822
886262 TA = 184
18495
MA = 184
19094
Ha = 191
155 n
mi
Hp = 187
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15603183
94 X = 4787781
87
Y = -2790053
63 feet Y = -797047
11 meter
Z = -15382406
14 Z = -4665376
63
XDOT = -5032
219383 XDOT = -1598
144147
YDOT = 22929
201864 feet/sec YDOT = 6971
308912 meter/sec
ZDOT = -9261
437868 ZDOT = -2830
493700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12831293
19 X = 3910978
16
Y = 9458933
52 feet Y = 2883082
94 meter
Z = -15288840
98 Z = -4660038
73
XDOT = -19363
604895 XDOT = -5902
026772
YDOT = 11244
751538 feet/sec YDOT = 3427
400269 meter/sec
ZDOT = -9292
240379 ZDOT = -2832
274868
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 11035
52084918
00016717 00000-0 10270-3 0 9026
2 25544 51
6445 121
1726 0004177 272
7984 87
2700 15
72338043 20029
Satellite: ISS
Catalog Number: 25544
Epoch time: 11035
52084918 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 121
1726 deg
Eccentricity:
0004177
Arg of perigee: 272
7984 deg
Mean anomaly: 87
2700 deg
Mean motion: 15
72338043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 289
Coasting Arc #4 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2011/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 326934
22 A = 6733047
00 meter
Y = -6053364
87 meter E =
0009309
Z = 2920385
60 I = 51
96063
XDOT = 5389
911549 Wp = 97
34421
YDOT = -2154
859849 meter/sec RA = 115
23377 deg
ZDOT = -5057
485522 TA = 49
21644
MA = 49
13571
Ha = 191
166 n
mi
Hp = 187
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1072618
84 X = 380413
49
Y = -19860120
98 feet Y = -6049409
78 meter
Z = 9581317
59 Z = 2922103
90
XDOT = 17683
436842 XDOT = 5438
174658
YDOT = -7069
750161 feet/sec YDOT = -2094
316918 meter/sec
ZDOT = -16592
800268 ZDOT = -5031
184783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14875156
46 X = 4533947
69
Y = -13197346
98 feet Y = -4022551
36 meter
Z = 9588342
72 Z = 2922526
86
XDOT = 16545
201313 XDOT = 5042
977360
YDOT = 6640
752570 feet/sec YDOT = 2024
101383 meter/sec
ZDOT = -16486
618695 ZDOT = -5025
121378
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 11036
53773700
00016717 00000-0 10270-3 0 9033
2 25544 51
6444 115
9636 0004054 279
5674 80
5030 15
72393292 20180
Satellite: ISS
Catalog Number: 25544
Epoch time: 11036
53773700 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 115
9636 deg
Eccentricity:
0004054
Arg of perigee: 279
5674 deg
Mean anomaly: 80
5030 deg
Mean motion: 15
72393292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 297
Coasting Arc #5 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2011/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4482620
96 A = 6729415
67 meter
Y = 2874920
22 meter E =
0006473
Z = 4109860
26 I = 51
96032
XDOT = -746
836610 Wp = 104
20437
YDOT = -6640
563461 meter/sec RA = 110
18168 deg
ZDOT = 3824
077914 TA = 306
66854
MA = 306
72802
Ha = 191
257 n
mi
Hp = 187
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14706761
66 X = -4534400
16
Y = 9432152
94 feet Y = 2824503
50 meter
Z = 13483793
52 Z = 4087958
35
XDOT = -2450
251346 XDOT = -691
101286
YDOT = -21786
625527 feet/sec YDOT = -6648
603247 meter/sec
ZDOT = 12546
187383 ZDOT = 3820
585528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17157808
68 X = -5229700
08
Y = -3638852
62 feet Y = -1109122
28 meter
Z = 13395349
51 Z = 4082902
53
XDOT = 13206
073997 XDOT = 4025
211354
YDOT = -16055
837930 feet/sec YDOT = -4893
819401 meter/sec
ZDOT = 12532
195727 ZDOT = 3819
813258
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 11037
55460506
00016717 00000-0 10270-3 0 9044
2 25544 51
6441 110
7539 0004120 283
0688 77
0014 15
72427949 20349
Satellite: ISS
Catalog Number: 25544
Epoch time: 11037
55460506 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 110
7539 deg
Eccentricity:
0004120
Arg of perigee: 283
0688 deg
Mean anomaly: 77
0014 deg
Mean motion: 15
72427949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 287
Coasting Arc #6 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2011/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1570475
03 A = 6730561
98 meter
Y = 5382822
67 meter E =
0001972
Z = -3724482
37 I = 51
97309
XDOT = -4660
363801 Wp = 89
67666
YDOT = 4343
869808 meter/sec RA = 105
03064 deg
ZDOT = 4314
856600 TA = 225
70378
MA = 225
71996
Ha = 191
248 n
mi
Hp = 187
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5152477
15 X = 1528259
05
Y = 17660179
38 feet Y = 5400148
47 meter
Z = -12219430
33 Z = -3716955
93
XDOT = -15289
907482 XDOT = -4729
551754
YDOT = 14251
541366 feet/sec YDOT = 4291
368136 meter/sec
ZDOT = 14156
353674 ZDOT = 4292
048797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8372162
18 X = -2551835
03
Y = 16403540
73 feet Y = 4999799
22 meter
Z = -12189142
13 Z = -3715250
52
XDOT = -19766
270797 XDOT = -6024
759339
YDOT = 357
586641 feet/sec YDOT = 108
992408 meter/sec
ZDOT = 14064
222856 ZDOT = 4286
775127
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 11038
50790335
00016717 00000-0 10270-3 0 9057
2 25544 51
6431 105
8705 0003978 288
5706 71
5024 15
72463257 20497
Satellite: ISS
Catalog Number: 25544
Epoch time: 11038
50790335 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 105
8705 deg
Eccentricity:
0003978
Arg of perigee: 288
5706 deg
Mean anomaly: 71
5024 deg
Mean motion: 15
72463257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 308
Coasting Arc #7 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2011/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3521289
37 A = 6731564
92 meter
Y = -4613339
97 meter E =
0002079
Z = -3413270
04 I = 51
98309
XDOT = 2714
033872 Wp = 37
78939
YDOT = 5504
332381 meter/sec RA = 99
98147 deg
ZDOT = -4639
548743 TA = 182
26212
MA = 182
26306
Ha = 191
343 n
mi
Hp = 187
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11552786
66 X = 3589195
65
Y = -15135629
81 feet Y = -4573583
22 meter
Z = -11198392
52 Z = -3395998
81
XDOT = 8904
310604 XDOT = 2674
819360
YDOT = 18058
833271 feet/sec YDOT = 5534
462915 meter/sec
ZDOT = -15221
616610 ZDOT = -4626
459661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18794659
04 X = 5728612
08
Y = -3297469
82 feet Y = -1005068
80 meter
Z = -11128595
99 Z = -3391996
06
XDOT = -5820
967188 XDOT = -1774
230799
YDOT = 18016
804169 feet/sec YDOT = 5491
521911 meter/sec
ZDOT = -15168
884275 ZDOT = -4623
475927
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 11039
52473628
00016717 00000-0 10270-3 0 9064
2 25544 51
6430 100
6604 0003963 294
2305 65
8443 15
72462126 20653
Satellite: ISS
Catalog Number: 25544
Epoch time: 11039
52473628 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 100
6604 deg
Eccentricity:
0003963
Arg of perigee: 294
2305 deg
Mean anomaly: 65
8443 deg
Mean motion: 15
72462126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 291
Coasting Arc #8 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2011/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3066621
84 A = 6728214
17 meter
Y = -4113301
16 meter E =
0007534
Z = 4351018
13 I = 51
97696
XDOT = 3227
221478 Wp = 46
69249
YDOT = -6073
453723 meter/sec RA = 94
83202 deg
ZDOT = -3458
294757 TA = 78
11872
MA = 78
03425
Ha = 191
394 n
mi
Hp = 187
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10061095
28 X = -3041534
35
Y = -13495082
53 feet Y = -4147453
58 meter
Z = 14274993
86 Z = 4336181
76
XDOT = 10587
996974 XDOT = 3311
695640
YDOT = -19926
029274 feet/sec YDOT = -6036
892756 meter/sec
ZDOT = -11346
111406 ZDOT = -3442
411808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1357693
89 X = 413825
10
Y = -16828649
00 feet Y = -5129372
22 meter
Z = 14215188
39 Z = 4332789
42
XDOT = 19964
066018 XDOT = 6085
047322
YDOT = -7943
588189 feet/sec YDOT = -2421
205680 meter/sec
ZDOT = -11281
880412 ZDOT = -3438
717150
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 11040
54154815
00016717 00000-0 10270-3 0 9073
2 25544 51
6433 95
4506 0004146 299
4777 60
5972 15
72529332 20812
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
54154815 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 95
4506 deg
Eccentricity:
0004146
Arg of perigee: 299
4777 deg
Mean anomaly: 60
5972 deg
Mean motion: 15
72529332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 309
Coasting Arc #9 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2011/040/21:41:30
892
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4047863
55 A = 6726453
99 meter
Y = -1846080
35 meter E =
0009508
Z = -5053311
42 I = 51
96952
XDOT = 1075
133601 Wp = 59
69609
YDOT = 7390
529983 meter/sec RA = 92
81235 deg
ZDOT = -1836
564347 TA = 192
64407
MA = 192
66794
Ha = 191
498 n
mi
Hp = 188
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13280392
23 X = 4092753
63
Y = -6056694
06 feet Y = -1800563
81 meter
Z = -16579105
71 Z = -5033538
12
XDOT = 3527
341209 XDOT = 1001
332957
YDOT = 24247
145613 feet/sec YDOT = 7402
140093 meter/sec
ZDOT = -6025
473580 ZDOT = -1831
520853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9159432
69 X = -2791795
08
Y = -11480355
68 feet Y = -3499212
41 meter
Z = -16499252
50 Z = -5028972
16
XDOT = 21790
574195 XDOT = 6641
767015
YDOT = -8744
571505 feet/sec YDOT = -2665
345395 meter/sec
ZDOT = -6005
266113 ZDOT = -1830
405111
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 11040
92285226
00016717 00000-0 10270-3 0 9087
2 25544 51
6444 93
4976 0004980 289
3866 70
6757 15
72162121 20874
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
92285226 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 93
4976 deg
Eccentricity:
0004980
Arg of perigee: 289
3866 deg
Mean anomaly: 70
6757 deg
Mean motion: 15
72162121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 325
Coasting Arc #10 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2011/041/21:41:30
892
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1936424
87 A = 6735442
92 meter
Y = -6073484
33 meter E =
0009113
Z = 2161935
38 I = 51
99982
XDOT = 4195
606565 Wp = 107
87716
YDOT = -3314
568422 meter/sec RA = 87
68112 deg
ZDOT = -5537
351788 TA = 48
07009
MA = 47
99244
Ha = 191
629 n
mi
Hp = 188
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6353099
97 X = -1878868
24
Y = -19926129
71 feet Y = -6094816
77 meter
Z = 7092963
83 Z = 2152668
22
XDOT = 13765
113403 XDOT = 4259
257933
YDOT = -10874
568314 feet/sec YDOT = -3267
294771 meter/sec
ZDOT = -18167
164658 ZDOT = -5516
815190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17549728
76 X = -5349157
33
Y = 11399426
59 feet Y = 3474545
23 meter
Z = 7055689
47 Z = 2150574
15
XDOT = -13303
105779 XDOT = -4054
786641
YDOT = -9254
113171 feet/sec YDOT = -2820
653695 meter/sec
ZDOT = -18084
191441 ZDOT = -5512
061551
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 11041
93987835
00016717 00000-0 10270-3 0 9095
2 25544 51
6442 88
2893 0004942 292
6172 67
4467 15
72149500 21034
Satellite: ISS
Catalog Number: 25544
Epoch time: 11041
93987835 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 88
2893 deg
Eccentricity:
0004942
Arg of perigee: 292
6172 deg
Mean anomaly: 67
4467 deg
Mean motion: 15
72149500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 323
Coasting Arc #11 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2011/042/21:41:30
892
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3103304
77 A = 6728341
75 meter
Y = 3842778
11 meter E =
0003640
Z = 4566368
75 I = 51
97467
XDOT = -3236
682045 Wp = 108
99937
YDOT = -6271
899335 meter/sec RA = 82
62519 deg
ZDOT = 3075
261704 TA = 310
51480
MA = 310
54650
Ha = 191
850 n
mi
Hp = 188
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10181446
09 X = -3168227
04
Y = 12607539
74 feet Y = 3807712
06 meter
Z = 14981524
77 Z = 4551135
46
XDOT = -10619
035582 XDOT = -3181
246755
YDOT = -20577
097555 feet/sec YDOT = -6307
783928 meter/sec
ZDOT = 10089
441287 ZDOT = 3059
672774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14972622
79 X = 4563655
43
Y = 6346179
21 feet Y = 1934315
42 meter
Z = 14919938
46 Z = 4547597
24
XDOT = -16318
380780 XDOT = -4973
842462
YDOT = 14903
076356 feet/sec YDOT = 4542
457673 meter/sec
ZDOT = 10026
659618 ZDOT = 3056
125852
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 11042
95688445
00016717 00000-0 10270-3 0 9105
2 25544 51
6449 83
0806 0005007 297
9424 62
1231 15
72193680 21195
Satellite: ISS
Catalog Number: 25544
Epoch time: 11042
95688445 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 83
0806 deg
Eccentricity:
0005007
Arg of perigee: 297
9424 deg
Mean anomaly: 62
1231 deg
Mean motion: 15
72193680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 304
Coasting Arc #12 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2011/043/21:41:30
892
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3591602
96 A = 6732896
02 meter
Y = 4724971
93 meter E =
0003620
Z = -3175065
54 I = 51
98563
XDOT = -2708
175689 Wp = 1
17620
YDOT = 5320
298645 meter/sec RA = 77
48001 deg
ZDOT = 4857
568774 TA = 322
04513
MA = 322
07063
Ha = 191
898 n
mi
Hp = 188
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11783474
28 X = 3553924
10
Y = 15501876
42 feet Y = 4764924
78 meter
Z = -10416881
68 Z = -3157709
30
XDOT = -8885
090842 XDOT = -2791
063748
YDOT = 17455
048049 feet/sec YDOT = 5289
550660 meter/sec
ZDOT = 15936
905428 ZDOT = 4844
211454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11310248
42 X = 3447363
72
Y = -15896198
92 feet Y = -4845161
43 meter
Z = -10346932
05 Z = -3153744
89
XDOT = 18170
324542 XDOT = 5538
314920
YDOT = 2597
869772 feet/sec YDOT = 791
830707 meter/sec
ZDOT = 15882
846130 ZDOT = 4841
091501
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 11043
91031051
00016717 00000-0 10270-3 0 9118
2 25544 51
6453 78
1976 0005151 301
7297 58
3362 15
72230975 21343
Satellite: ISS
Catalog Number: 25544
Epoch time: 11043
91031051 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 78
1976 deg
Eccentricity:
0005151
Arg of perigee: 301
7297 deg
Mean anomaly: 58
3362 deg
Mean motion: 15
72230975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 285
Coasting Arc #13 (Orbit 2149)
---------------------------------------
Vector Time (GMT): 2011/044/21:41:30
892
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1514577
73 A = 6730649
32 meter
Y = -5286450
55 meter E =
0005189
Z = -3886353
34 I = 51
97053
XDOT = 4775
293394 Wp = 22
08677
YDOT = 4400
915063 meter/sec RA = 72
43217 deg
ZDOT = -4122
448443 TA = 205
02610
MA = 205
05126
Ha = 191
897 n
mi
Hp = 188
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4969087
05 X = 1592458
03
Y = -17343997
86 feet Y = -5269078
09 meter
Z = -12750503
09 Z = -3878806
63
XDOT = 15666
973076 XDOT = 4745
752274
YDOT = 14438
697712 feet/sec YDOT = 4454
150192 meter/sec
ZDOT = -13525
093318 ZDOT = -4099
322257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18052924
80 X = -5502531
48
Y = 614493
89 feet Y = 187297
74 meter
Z = -12719894
67 Z = -3877023
90
XDOT = 8852
985885 XDOT = 2698
390098
YDOT = -18147
882600 feet/sec YDOT = -5531
474616 meter/sec
ZDOT = -13431
841276 ZDOT = -4094
025221
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 11044
92728039
00016717 00000-0 10270-3 0 9120
2 25544 51
6453 72
9891 0005254 304
7362 55
3305 15
72248691 21507
Satellite: ISS
Catalog Number: 25544
Epoch time: 11044
92728039 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 72
9891 deg
Eccentricity:
0005254
Arg of perigee: 304
7362 deg
Mean anomaly: 55
3305 deg
Mean motion: 15
72248691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2150
Checksum: 301
Coasting Arc #14 (Orbit 2165)
---------------------------------------
Vector Time (GMT): 2011/045/21:41:30
892
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4590332
79 A = 6730135
42 meter
Y = -2877792
55 meter E =
0008740
Z = 3991083
14 I = 51
95910
XDOT = 635
354037 Wp = 50
64113
YDOT = -6554
725306 meter/sec RA = 67
28145 deg
ZDOT = -3984
384666 TA = 80
50113
MA = 80
40235
Ha = 192
043 n
mi
Hp = 187
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15060146
96 X = -4577199
04
Y = -9441576
60 feet Y = -2929051
05 meter
Z = 13094104
79 Z = 3968815
77
XDOT = 2084
494872 XDOT = 727
957884
YDOT = -21505
004284 feet/sec YDOT = -6547
102553 meter/sec
ZDOT = -13072
128168 ZDOT = -3981
073376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3951532
26 X = -1204427
03
Y = 17397733
92 feet Y = 5302829
30 meter
Z = 13004277
10 Z = 3963703
66
XDOT = -19755
893183 XDOT = -6021
596242
YDOT = 5301
372753 feet/sec YDOT = 1615
858415 meter/sec
ZDOT = -13058
579921 ZDOT = -3980
255160
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 11045
94423082
00016717 00000-0 10270-3 0 9134
2 25544 51
6453 67
7803 0005275 310
4572 49
6130 15
72323521 21667
Satellite: ISS
Catalog Number: 25544
Epoch time: 11045
94423082 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 67
7803 deg
Eccentricity:
0005275
Arg of perigee: 310
4572 deg
Mean anomaly: 49
6130 deg
Mean motion: 15
72323521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2166
Checksum: 285
Coasting Arc #15 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2011/046/21:41:30
892
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 455431
93 A = 6732983
84 meter
Y = 5980285
40 meter E =
0010586
Z = 3045641
77 I = 51
95506
XDOT = -5499
432038 Wp = 61
55791
YDOT = -2111
747675 meter/sec RA = 62
23012 deg
ZDOT = 4960
877163 TA = 333
53704
MA = 333
59106
Ha = 192
210 n
mi
Hp = 187
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1494199
24 X = 373730
69
Y = 19620358
94 feet Y = 5984921
51 meter
Z = 9992263
01 Z = 3047655
73
XDOT = -18042
756029 XDOT = -5499
507631
YDOT = -6928
306019 feet/sec YDOT = -2173
246065 meter/sec
ZDOT = 16275
843710 ZDOT = 4934
161586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17927206
19 X = 5464212
45
Y = -8102291
33 feet Y = -2469578
40 meter
Z = 10000229
48 Z = 3048069
95
XDOT = -849
336033 XDOT = -258
877623
YDOT = 18108
533041 feet/sec YDOT = 5519
480871 meter/sec
ZDOT = 16168
030993 ZDOT = 4928
015847
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 11046
96116367
00016717 00000-0 10270-3 0 9143
2 25544 51
6446 62
5705 0005278 314
5303 45
5427 15
72300943 21828
Satellite: ISS
Catalog Number: 25544
Epoch time: 11046
96116367 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 62
5705 deg
Eccentricity:
0005278
Arg of perigee: 314
5303 deg
Mean anomaly: 45
5427 deg
Mean motion: 15
72300943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 295
Coasting Arc #16 (Orbit 2196)
---------------------------------------
Vector Time (GMT): 2011/047/21:41:30
892
Vector Time (MET): N/A
Weight (LBS) : 863286
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4827700
41 A = 6727698
15 meter
Y = 791551
75 meter E =
0006201
Z = -4623446
16 I = 51
92174
XDOT = 1700
736108 Wp = 87
18846
YDOT = 6894
343848 meter/sec RA = 57
08136 deg
ZDOT = 2959
896901 TA = 212
05219
MA = 212
08991
Ha = 192
258 n
mi
Hp = 187
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15838912
12 X = 4840949
43
Y = 2596954
57 feet Y = 845611
97 meter
Z = -15168786
61 Z = -4599961
83
XDOT = 5579
842874 XDOT = 1609
137693
YDOT = 22619
238346 feet/sec YDOT = 6912
850438 meter/sec
ZDOT = 9710
947838 ZDOT = 2967
936114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3319091
93 X = -1011659
22
Y = -15794495
65 feet Y = -4814162
27 meter
Z = -15073982
00 Z = -4594549
71
XDOT = 17957
703597 XDOT = 5473
508056
YDOT = -13060
805474 feet/sec YDOT = -3980
933508 meter/sec
ZDOT = 9743
217569 ZDOT = 2969
732715
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 11047
91451818
00016717 00000-0 10270-3 0 9153
2 25544 51
6440 57
6862 0005286 316
7289 43
3458 15
72357280 21979
Satellite: ISS
Catalog Number: 25544
Epoch time: 11047
91451818 = yrday
fracday
Element set: 915
Inclination: 51
6440 deg
RA of node: 57
6862 deg
Eccentricity:
0005286
Arg of perigee: 316
7289 deg
Mean anomaly: 43
3458 deg
Mean motion: 15
72357280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2197
Checksum: 326
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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