Date:
June 25th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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 710)
---------------------------------------
Vector Time (GMT): 2009/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1498042
88 A = 6731140
10 meter
Y = 6331888
25 meter E =
0021821
Z = 1675120
37 I = 51
32539
XDOT = -4500
873492 Wp = 128
09474
YDOT = 2582
919116 meter/sec RA = 268
58121 deg
ZDOT = -5701
287484 TA = 33
28183
MA = 33
14480
Ha = 192
726 n
mi
Hp = 181
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4914838
85 X = 1418989
97
Y = 20773911
59 feet Y = 6348197
89 meter
Z = 5495801
75 Z = 1682207
06
XDOT = -14766
645314 XDOT = -4501
726156
YDOT = 8474
144082 feet/sec YDOT = 2532
584127 meter/sec
ZDOT = -18705
011431 ZDOT = -5723
153989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20590002
34 X = 6275832
71
Y = -5608336
88 feet Y = -1709421
08 meter
Z = 5523879
19 Z = 1683678
38
XDOT = 8573
645567 XDOT = 2613
247169
YDOT = 12850
143599 feet/sec YDOT = 3916
723769 meter/sec
ZDOT = -18790
607319 ZDOT = -5727
377111
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 09175
53508363
00010596 00000-0 82463-4 0 9005
2 25544 51
6420 269
1845 0008574 148
7064 211
4611 15
73933443 7116
Satellite: ISS
Catalog Number: 25544
Epoch time: 09175
53508363 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 269
1845 deg
Eccentricity:
0008574
Arg of perigee: 148
7064 deg
Mean anomaly: 211
4611 deg
Mean motion: 15
73933443 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 711
Checksum: 301
Coasting Arc #2 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2009/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3705769
15 A = 6721339
84 meter
Y = -2599191
78 meter E =
0013766
Z = 4964395
55 I = 51
29513
XDOT = 2364
930073 Wp = 141
25590
YDOT = 7075
252956 meter/sec RA = 263
45390 deg
ZDOT = 1925
537047 TA = 289
99144
MA = 290
13962
Ha = 192
441 n
mi
Hp = 181
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12158035
27 X = 3710442
56
Y = -8527532
09 feet Y = -2557726
45 meter
Z = 16287386
99 Z = 4982408
81
XDOT = 7758
956933 XDOT = 2276
283858
YDOT = 23212
772166 feet/sec YDOT = 7101
203001 meter/sec
ZDOT = 6317
378764 ZDOT = 1936
811635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9145938
37 X = -2787682
01
Y = -11601173
40 feet Y = -3536037
65 meter
Z = 16357878
45 Z = 4985881
35
XDOT = 21931
693403 XDOT = 6684
780149
YDOT = -8257
606797 feet/sec YDOT = -2516
918552 meter/sec
ZDOT = 6361
924829 ZDOT = 1939
114688
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 09176
55093721
00010596 00000-0 82463-4 0 9016
2 25544 51
6421 263
9678 0008399 152
8650 207
2953 15
74002171 7270
Satellite: ISS
Catalog Number: 25544
Epoch time: 09176
55093721 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 263
9678 deg
Eccentricity:
0008399
Arg of perigee: 152
8650 deg
Mean anomaly: 207
2953 deg
Mean motion: 15
74002171 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 727
Checksum: 316
Coasting Arc #3 (Orbit 741)
---------------------------------------
Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2605930
85 A = 6731033
63 meter
Y = -5980567
17 meter E =
0008184
Z = -1668230
21 I = 51
33148
XDOT = 3968
355254 Wp = 99
02992
YDOT = -3312
001704 meter/sec RA = 258
26408 deg
ZDOT = 5697
053322 TA = 242
46970
MA = 242
55289
Ha = 192
428 n
mi
Hp = 182
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8549641
90 X = -2530757
61
Y = -19621283
38 feet Y = -6009287
65 meter
Z = -5473196
23 Z = -1680707
94
XDOT = 13019
538236 XDOT = 3977
420812
YDOT = -10866
147322 feet/sec YDOT = -3267
575392 meter/sec
ZDOT = 18691
119824 ZDOT = 5716
352859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18982709
24 X = -5785929
78
Y = 9859343
06 feet Y = 3005127
76 meter
Z = -5522419
72 Z = -1683233
53
XDOT = -11016
958328 XDOT = -3357
968898
YDOT = -10741
017510 feet/sec YDOT = -3273
862137 meter/sec
ZDOT = 18766
617864 ZDOT = 5720
065125
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 09177
50328800
00010596 00000-0 82463-4 0 9022
2 25544 51
6414 259
0779 0008142 155
7789 204
3759 15
73965589 7420
Satellite: ISS
Catalog Number: 25544
Epoch time: 09177
50328800 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 259
0779 deg
Eccentricity:
0008142
Arg of perigee: 155
7789 deg
Mean anomaly: 204
3759 deg
Mean motion: 15
73965589 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 742
Checksum: 342
Coasting Arc #4 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3226999
52 A = 6721261
19 meter
Y = 3149856
50 meter E =
0016288
Z = -4996200
63 I = 51
30505
XDOT = -3546
150818 Wp = 106
16551
YDOT = -6566
191120 meter/sec RA = 253
13639 deg
ZDOT = -1858
717443 TA = 145
84800
MA = 145
74311
Ha = 192
271 n
mi
Hp = 182
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10587268
76 X = -3237711
53
Y = 10334174
87 feet Y = 3113711
06 meter
Z = -16391734
34 Z = -5011902
84
XDOT = -11634
353077 XDOT = -3463
433777
YDOT = -21542
621784 feet/sec YDOT = -6605
383517 meter/sec
ZDOT = -6098
154340 ZDOT = -1875
744398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11203405
07 X = 3414797
86
Y = 9557847
34 feet Y = 2913231
87 meter
Z = -16453135
08 Z = -5014915
57
XDOT = -19760
738378 XDOT = -6023
073058
YDOT = 12603
244233 feet/sec YDOT = 3841
468842 meter/sec
ZDOT = -6165
256632 ZDOT = -1879
170222
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 09178
51911306
00010596 00000-0 82463-4 0 9034
2 25544 51
6404 253
8609 0008213 159
8925 200
2564 15
74000737 7581
Satellite: ISS
Catalog Number: 25544
Epoch time: 09178
51911306 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 253
8609 deg
Eccentricity:
0008213
Arg of perigee: 159
8925 deg
Mean anomaly: 200
2564 deg
Mean motion: 15
74000737 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 758
Checksum: 305
Coasting Arc #5 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3581637
74 A = 6730900
14 meter
Y = 5458123
11 meter E =
0020594
Z = 1588382
50 I = 51
34805
XDOT = -3373
128374 Wp = 133
16923
YDOT = 3892
306728 meter/sec RA = 247
94775 deg
ZDOT = -5736
276790 TA = 29
20985
MA = 29
09484
Ha = 192
075 n
mi
Hp = 182
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11750780
00 X = 3512621
86
Y = 17907228
05 feet Y = 5497789
00 meter
Z = 5211228
66 Z = 1605615
01
XDOT = -11066
694142 XDOT = -3388
536488
YDOT = 12770
035197 feet/sec YDOT = 3854
500979 meter/sec
ZDOT = -18819
805743 ZDOT = -5752
700304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16595417
70 X = 5058283
31
Y = -13514062
75 feet Y = -4119086
33 meter
Z = 5279088
07 Z = 1609066
04
XDOT = 12851
632630 XDOT = 3917
177626
YDOT = 8363
777280 feet/sec YDOT = 2549
279315 meter/sec
ZDOT = -18883
993985 ZDOT = -5755
841367
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 09179
53492256
00010596 00000-0 82463-4 0 9046
2 25544 51
6405 248
6439 0008085 162
3108 197
8339 15
74055148 7749
Satellite: ISS
Catalog Number: 25544
Epoch time: 09179
53492256 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 248
6439 deg
Eccentricity:
0008085
Arg of perigee: 162
3108 deg
Mean anomaly: 197
8339 deg
Mean motion: 15
74055148 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 774
Checksum: 335
Coasting Arc #6 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2647289
08 A = 6720956
94 meter
Y = -3616190
25 meter E =
0012680
Z = 5006149
43 I = 51
32712
XDOT = 4633
661344 Wp = 150
20217
YDOT = 5887
714377 meter/sec RA = 242
82007 deg
ZDOT = 1789
873745 TA = 282
41263
MA = 282
55451
Ha = 191
919 n
mi
Hp = 182
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8685331
61 X = 2663210
26
Y = -11864141
24 feet Y = -3586498
32 meter
Z = 16424374
77 Z = 5019048
16
XDOT = 15202
300999 XDOT = 4558
784672
YDOT = 19316
648217 feet/sec YDOT = 5939
111808 meter/sec
ZDOT = 5872
289189 ZDOT = 1812
202887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12814549
81 X = -3905874
78
Y = -7093843
37 feet Y = -2162203
46 meter
Z = 16474757
01 Z = 5021505
94
XDOT = 16825
884356 XDOT = 5128
529552
YDOT = -16455
699183 feet/sec YDOT = -5015
697111 meter/sec
ZDOT = 5960
163281 ZDOT = 1816
657768
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 09180
55071603
00010596 00000-0 82463-4 0 9050
2 25544 51
6405 243
4267 0008055 166
9225 193
2149 15
74083439 7909
Satellite: ISS
Catalog Number: 25544
Epoch time: 09180
55071603 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 243
4267 deg
Eccentricity:
0008055
Arg of perigee: 166
9225 deg
Mean anomaly: 193
2149 deg
Mean motion: 15
74083439 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 790
Checksum: 309
Coasting Arc #7 (Orbit 804)
---------------------------------------
Vector Time (GMT): 2009/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4476171
68 A = 6730944
90 meter
Y = -4794562
20 meter E =
0006485
Z = -1519507
26 I = 51
37489
XDOT = 2696
475967 Wp = 100
83700
YDOT = -4335
084178 meter/sec RA = 237
63374 deg
ZDOT = 5754
964526 TA = 242
37246
MA = 242
43832
Ha = 191
857 n
mi
Hp = 182
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14685602
62 X = -4414843
89
Y = -15730190
95 feet Y = -4844274
26 meter
Z = -4985260
03 Z = -1541104
22
XDOT = 8846
705927 XDOT = 2716
794594
YDOT = -14222
717118 feet/sec YDOT = -4304
817778 meter/sec
ZDOT = 18881
117212 ZDOT = 5768
112793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13559756
83 X = -4133013
88
Y = 16684861
68 feet Y = 5085545
84 meter
Z = -5070210
49 Z = -1545400
16
XDOT = -14074
289336 XDOT = -4289
843389
YDOT = -5704
147617 feet/sec YDOT = -1738
624194 meter/sec
ZDOT = 18932
440343 ZDOT = 5770
607817
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 09181
50301045
00010596 00000-0 82463-4 0 9063
2 25544 51
6399 238
5356 0007848 169
7043 190
4282 15
74064770 8054
Satellite: ISS
Catalog Number: 25544
Epoch time: 09181
50301045 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 238
5356 deg
Eccentricity:
0007848
Arg of perigee: 169
7043 deg
Mean anomaly: 190
4282 deg
Mean motion: 15
74064770 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 805
Checksum: 317
Coasting Arc #8 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2077699
58 A = 6720770
60 meter
Y = 3928413
01 meter E =
0015001
Z = -5052750
80 I = 51
35800
XDOT = -5552
006757 Wp = 109
17498
YDOT = -5058
414500 meter/sec RA = 232
50591 deg
ZDOT = -1658
679763 TA = 144
84763
MA = 144
74857
Ha = 191
710 n
mi
Hp = 182
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6816599
69 X = -2096927
93
Y = 12888494
14 feet Y = 3905072
22 meter
Z = -16577266
42 Z = -5062890
41
XDOT = -18215
245265 XDOT = -5486
972478
YDOT = -16595
848097 feet/sec YDOT = -5120
136408 meter/sec
ZDOT = -5441
862740 ZDOT = -1685
494298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13773429
85 X = 4198141
42
Y = 4643180
72 feet Y = 1415241
48 meter
Z = -16616816
10 Z = -5064805
55
XDOT = -13241
189249 XDOT = -4035
914483
YDOT = 19529
705001 feet/sec YDOT = 5952
654084 meter/sec
ZDOT = -5547
295801 ZDOT = -1690
815760
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 09182
51877647
00010596 00000-0 82463-4 0 9072
2 25544 51
6402 233
3178 0007914 173
1298 186
9975 15
74094733 8218
Satellite: ISS
Catalog Number: 25544
Epoch time: 09182
51877647 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 233
3178 deg
Eccentricity:
0007914
Arg of perigee: 173
1298 deg
Mean anomaly: 186
9975 deg
Mean motion: 15
74094733 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 821
Checksum: 340
Coasting Arc #9 (Orbit 836)
---------------------------------------
Vector Time (GMT): 2009/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5206130
86 A = 6730862
00 meter
Y = 4015232
68 meter E =
0019356
Z = 1385846
88 I = 51
41195
XDOT = -2025
842272 Wp = 139
06339
YDOT = 4643
051998 meter/sec RA = 227
32423 deg
ZDOT = -5810
766333 TA = 25
63676
MA = 25
54092
Ha = 191
448 n
mi
Hp = 182
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17080481
84 X = 5154112
71
Y = 13173335
55 feet Y = 4073159
59 meter
Z = 4546741
75 Z = 1411012
68
XDOT = -6646
464148 XDOT = -2049
383378
YDOT = 15233
110231 feet/sec YDOT = 4620
267213 meter/sec
ZDOT = -19064
194007 ZDOT = -5820
664292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10047028
94 X = 3062334
42
Y = -19063775
36 feet Y = -5810638
73 meter
Z = 4645661
23 Z = 1415997
54
XDOT = 14739
083935 XDOT = 4492
472783
YDOT = 3088
210641 feet/sec YDOT = 941
286603 meter/sec
ZDOT = -19102
760353 ZDOT = -5822
521355
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 09183
53452656
00010596 00000-0 82463-4 0 9085
2 25544 51
6403 228
1007 0007725 176
3034 183
8187 15
74157788 8373
Satellite: ISS
Catalog Number: 25544
Epoch time: 09183
53452656 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 228
1007 deg
Eccentricity:
0007725
Arg of perigee: 176
3034 deg
Mean anomaly: 183
8187 deg
Mean motion: 15
74157788 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 837
Checksum: 328
Coasting Arc #10 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2009/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1458806
86 A = 6720432
02 meter
Y = -4150824
01 meter E =
0011329
Z = 5078994
97 I = 51
39707
XDOT = 6337
128490 Wp = 159
42259
YDOT = 4104
566725 meter/sec RA = 222
19751 deg
ZDOT = 1522
813932 TA = 275
85834
MA = 275
98747
Ha = 191
395 n
mi
Hp = 182
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4786111
73 X = 1480440
80
Y = -13618189
00 feet Y = -4134390
77 meter
Z = 16663369
31 Z = 5086133
63
XDOT = 20791
103969 XDOT = 6283
361977
YDOT = 13466
426263 feet/sec YDOT = 4175
131291 meter/sec
ZDOT = 4996
108701 ZDOT = 1553
469901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14258207
37 X = -4345901
61
Y = -2034470
45 feet Y = -620106
59 meter
Z = 16691143
36 Z = 5087460
50
XDOT = 9157
200114 XDOT = 2791
114595
YDOT = -21890
669569 feet/sec YDOT = -6672
276085 meter/sec
ZDOT = 5116
578837 ZDOT = 1559
533229
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 09184
55026291
00010596 00000-0 82463-4 0 9091
2 25544 51
6394 222
8835 0007756 179
5330 180
5842 15
74166515 8538
Satellite: ISS
Catalog Number: 25544
Epoch time: 09184
55026291 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 222
8835 deg
Eccentricity:
0007756
Arg of perigee: 179
5330 deg
Mean anomaly: 180
5842 deg
Mean motion: 15
74166515 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 853
Checksum: 329
Coasting Arc #11 (Orbit 867)
---------------------------------------
Vector Time (GMT): 2009/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5822500
53 A = 6730894
78 meter
Y = -3136896
47 meter E =
0005064
Z = -1256645
85 I = 51
45603
XDOT = 1340
251991 Wp = 96
41974
YDOT = -4821
177890 meter/sec RA = 217
02038 deg
ZDOT = 5844
554962 TA = 249
77262
MA = 249
82708
Ha = 191
247 n
mi
Hp = 183
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19102692
02 X = -5780885
93
Y = -10291655
08 feet Y = -3201774
14 meter
Z = -4122853
82 Z = -1284831
03
XDOT = 4397
152202 XDOT = 1365
671897
YDOT = -15817
512764 feet/sec YDOT = -4806
049436 meter/sec
ZDOT = 19175
049088 ZDOT = 5851
126682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6148920
29 X = -1874190
90
Y = 20786928
42 feet Y = 6335855
78 meter
Z = -4233593
79 Z = -1290399
39
XDOT = -14844
589329 XDOT = -4524
630827
YDOT = -493
376789 feet/sec YDOT = -150
381245 meter/sec
ZDOT = 19200
564762 ZDOT = 5852
332139
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 09185
50250261
00010596 00000-0 82463-4 0 9105
2 25544 51
6398 217
9921 0007695 183
1365 176
9751 15
74192870 8681
Satellite: ISS
Catalog Number: 25544
Epoch time: 09185
50250261 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 217
9921 deg
Eccentricity:
0007695
Arg of perigee: 183
1365 deg
Mean anomaly: 176
9751 deg
Mean motion: 15
74192870 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 868
Checksum: 336
Coasting Arc #12 (Orbit 883)
---------------------------------------
Vector Time (GMT): 2009/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -905082
97 A = 6720171
07 meter
Y = 4254778
70 meter E =
0013853
Z = -5132395
56 I = 51
44432
XDOT = -6929
438234 Wp = 111
80954
YDOT = -3065
845548 meter/sec RA = 211
89324 deg
ZDOT = -1327
537421 TA = 145
48674
MA = 145
39672
Ha = 191
096 n
mi
Hp = 183
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2969432
33 X = -927661
28
Y = 13959247
71 feet Y = 4244532
33 meter
Z = -16838568
12 Z = -5136846
42
XDOT = -22734
377407 XDOT = -6888
191522
YDOT = -10058
548385 feet/sec YDOT = -3143
103688 meter/sec
ZDOT = -4355
437732 ZDOT = -1361
100852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14247965
43 X = 4342779
86
Y = -305189
17 feet Y = -93021
66 meter
Z = -16855795
50 Z = -5137646
47
XDOT = -4777
983841 XDOT = -1456
329475
YDOT = 23338
130320 feet/sec YDOT = 7113
462122 meter/sec
ZDOT = -4487
290723 ZDOT = -1367
726212
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 09186
51821026
00010596 00000-0 82463-4 0 9111
2 25544 51
6399 212
7741 0007675 187
2493 172
8560 15
74190610 8841
Satellite: ISS
Catalog Number: 25544
Epoch time: 09186
51821026 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 212
7741 deg
Eccentricity:
0007675
Arg of perigee: 187
2493 deg
Mean anomaly: 172
8560 deg
Mean motion: 15
74190610 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 884
Checksum: 322
Coasting Arc #13 (Orbit 899)
---------------------------------------
Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6258877
95 A = 6731012
89 meter
Y = 2199969
80 meter E =
0018178
Z = 1068090
41 I = 51
50582
XDOT = -709
319278 Wp = 145
96505
YDOT = 4901
850022 meter/sec RA = 206
72245 deg
ZDOT = -5906
506633 TA = 22
31749
MA = 22
23849
Ha = 190
907 n
mi
Hp = 183
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20534376
47 X = 6228623
80
Y = 7217748
69 feet Y = 2269790
86 meter
Z = 3504233
63 Z = 1098422
68
XDOT = -2327
162987 XDOT = -735
387442
YDOT = 16082
185110 feet/sec YDOT = 4893
773410 meter/sec
ZDOT = -19378
302603 ZDOT = -5910
014823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2102293
65 X = 640779
10
Y = -21644575
59 feet Y = -6597266
64 meter
Z = 3623378
99 Z = 1104405
92
XDOT = 14566
410630 XDOT = 4439
841960
YDOT = -1849
201337 feet/sec YDOT = -563
636568 meter/sec
ZDOT = -19391
794412 ZDOT = -5910
618937
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 09187
53390333
00010596 00000-0 82463-4 0 9127
2 25544 51
6384 207
5561 0007577 190
1254 169
9757 15
74224828 9009
Satellite: ISS
Catalog Number: 25544
Epoch time: 09187
53390333 = yrday
fracday
Element set: 912
Inclination: 51
6384 deg
RA of node: 207
5561 deg
Eccentricity:
0007577
Arg of perigee: 190
1254 deg
Mean anomaly: 169
9757 deg
Mean motion: 15
74224828 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 900
Checksum: 326
Coasting Arc #14 (Orbit 915)
---------------------------------------
Vector Time (GMT): 2009/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 342418
00 A = 6719846
89 meter
Y = -4284546
28 meter E =
0009626
Z = 5165802
62 I = 51
49481
XDOT = 7364
256839 Wp = 171
74075
YDOT = 1954
126283 meter/sec RA = 201
59519 deg
ZDOT = 1122
984392 TA = 267
46529
MA = 267
57550
Ha = 190
780 n
mi
Hp = 183
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1123418
63 X = 365208
89
Y = -14056910
37 feet Y = -4280590
70 meter
Z = 16948171
33 Z = 5167520
62
XDOT = 24160
947636 XDOT = 7336
402961
YDOT = 6411
175470 feet/sec YDOT = 2036
321760 meter/sec
ZDOT = 3684
331996 ZDOT = 1158
692177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13851029
28 X = -4221793
72
Y = 2605273
08 feet Y = 794087
24 meter
Z = 16954670
46 Z = 5167783
56
XDOT = 212
425012 XDOT = 64
747144
YDOT = -23965
974889 feet/sec YDOT = -7304
829146 meter/sec
ZDOT = 3824
577069 ZDOT = 1165
731091
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 09188
54958145
00010596 00000-0 82463-4 0 9131
2 25544 51
6378 202
3377 0007505 194
2224 165
8729 15
74246668 9160
Satellite: ISS
Catalog Number: 25544
Epoch time: 09188
54958145 = yrday
fracday
Element set: 913
Inclination: 51
6378 deg
RA of node: 202
3377 deg
Eccentricity:
0007505
Arg of perigee: 194
2224 deg
Mean anomaly: 165
8729 deg
Mean motion: 15
74246668 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 916
Checksum: 341
Coasting Arc #15 (Orbit 930)
---------------------------------------
Vector Time (GMT): 2009/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6562982
18 A = 6730898
66 meter
Y = -1209985
33 meter E =
0004028
Z = -876865
31 I = 51
56167
XDOT = 109
846977 Wp = 81
54130
YDOT = -4886
176536 meter/sec RA = 196
43198 deg
ZDOT = 5944
058460 TA = 268
88486
MA = 268
93101
Ha = 190
570 n
mi
Hp = 183
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21532093
78 X = -6544704
56
Y = -3969768
14 feet Y = -1283274
09 meter
Z = -2876854
69 Z = -908703
58
XDOT = 360
390346 XDOT = 135
602180
YDOT = -16030
762914 feet/sec YDOT = -4884
805188 meter/sec
ZDOT = 19501
504134 ZDOT = 5944
653800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2041405
83 X = 622220
50
Y = 21782739
53 feet Y = 6639379
01 meter
Z = -3001888
60 Z = -914975
65
XDOT = -13902
996586 XDOT = -4237
633360
YDOT = 3980
428106 feet/sec YDOT = 1213
234487 meter/sec
ZDOT = 19503
558818 ZDOT = 5944
684728
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 09189
50176615
00010596 00000-0 82463-4 0 9143
2 25544 51
6384 197
4464 0007614 197
7258 162
3641 15
74318175 9319
Satellite: ISS
Catalog Number: 25544
Epoch time: 09189
50176615 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 197
4464 deg
Eccentricity:
0007614
Arg of perigee: 197
7258 deg
Mean anomaly: 162
3641 deg
Mean motion: 15
74318175 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 931
Checksum: 332
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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