Date:
March 15th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
077/02:55:34
987 -0
4 0
8 0
8
N/A -0
3 -0
0 186
1
000/00:05:09
975 0
7 -0
1 180
6
080/02:40:34
911 0
0 0
6 0
6
N/A -0
5 -0
0 186
5
000/00:05:09
822 0
3 -0
1 180
2
Coasting Arc #1 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2008/073/08:39:35
824
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4281614
74 A = 6715443
91 meter
Y = 1884460
51 meter E =
0010536
Z = -4827805
10 I = 51
78844
XDOT = -5072
524388 Wp = 74
95189
YDOT = 5241
991014 meter/sec RA = 149
41824 deg
ZDOT = -2454
262257 TA = 171
11296
MA = 171
09430
Ha = 186
120 n
mi
Hp = 180
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14047292
47 X = 4283676
72
Y = 6182613
22 feet Y = 1932351
46 meter
Z = -15839255
57 Z = -4807000
09
XDOT = -16642
140382 XDOT = -5118
841820
YDOT = 17198
133247 feet/sec YDOT = 5185
008160 meter/sec
ZDOT = -8052
041524 ZDOT = -2479
017040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1849274
87 X = 563658
98
Y = 15318551
54 feet Y = 4669094
51 meter
Z = -15759292
82 Z = -4803432
45
XDOT = -22125
092099 XDOT = -6743
728072
YDOT = -5703
779782 feet/sec YDOT = -1738
512078 meter/sec
ZDOT = -8146
289253 ZDOT = -2482
988964
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 08073
38098223
00020000 00000-0 20000-3 0 9002
2 25544 51
6369 150
2616 0001389 233
7168 126
3868 15
76352984 13417
Satellite: ISS
Catalog Number: 25544
Epoch time: 08073
38098223 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 150
2616 deg
Eccentricity:
0001389
Arg of perigee: 233
7168 deg
Mean anomaly: 126
3868 deg
Mean motion: 15
76352984 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1341
Checksum: 301
Coasting Arc #2 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2008/074/08:39:35
824
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4631741
99 A = 6724516
73 meter
Y = -4666919
54 meter E =
0013511
Z = 1375635
09 I = 51
84426
XDOT = 4319
664248 Wp = 124
87277
YDOT = 2553
161151 meter/sec RA = 144
24418 deg
ZDOT = -5849
825793 TA = 40
03187
MA = 39
93236
Ha = 186
043 n
mi
Hp = 180
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15196003
90 X = 4676901
44
Y = -15311415
81 feet Y = -4614872
26 meter
Z = 4513238
48 Z = 1398245
58
XDOT = 14172
126797 XDOT = 4319
210514
YDOT = 8376
512963 feet/sec YDOT = 2601
463585 meter/sec
ZDOT = -19192
341839 ZDOT = -5828
842135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20980728
30 X = 6394925
99
Y = 4937845
40 feet Y = 1505055
28 meter
Z = 4599351
39 Z = 1401882
30
XDOT = 676
927811 XDOT = 206
327597
YDOT = 15023
224793 feet/sec YDOT = 4579
078917 meter/sec
ZDOT = -19111
606651 ZDOT = -5825
217707
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 08074
39527898
00020000 00000-0 20000-3 0 9010
2 25544 51
6371 145
0337 0001334 235
2466 124
8573 15
76395808 13575
Satellite: ISS
Catalog Number: 25544
Epoch time: 08074
39527898 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 145
0337 deg
Eccentricity:
0001334
Arg of perigee: 235
2466 deg
Mean anomaly: 124
8573 deg
Mean motion: 15
76395808 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1357
Checksum: 307
Coasting Arc #3 (Orbit 1372)
---------------------------------------
Vector Time (GMT): 2008/075/08:39:35
824
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3251121
41 A = 6713177
83 meter
Y = -2639563
91 meter E =
0002415
Z = 5245784
74 I = 51
83075
XDOT = 5453
854372 Wp = 142
13957
YDOT = -5404
890055 meter/sec RA = 139
12328 deg
ZDOT = 658
424520 TA = 301
60986
MA = 301
63342
Ha = 185
969 n
mi
Hp = 180
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10666408
83 X = -3246846
49
Y = -8659986
57 feet Y = -2675895
89 meter
Z = 17210579
87 Z = 5230001
40
XDOT = 17893
223005 XDOT = 5510
688887
YDOT = -17732
578922 feet/sec YDOT = -5343
584165 meter/sec
ZDOT = 2160
185434 ZDOT = 685
057029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1526002
00 X = 465125
41
Y = -13730575
51 feet Y = -4185079
41 meter
Z = 17149761
47 Z = 5227247
30
XDOT = 23559
254981 XDOT = 7180
860918
YDOT = 5451
525944 feet/sec YDOT = 1661
625108 meter/sec
ZDOT = 2261
642286 ZDOT = 689
348569
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 08075
40954401
00020000 00000-0 20000-3 0 9028
2 25544 51
6381 139
8060 0001296 246
7346 113
3683 15
76486125 13737
Satellite: ISS
Catalog Number: 25544
Epoch time: 08075
40954401 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 139
8060 deg
Eccentricity:
0001296
Arg of perigee: 246
7346 deg
Mean anomaly: 113
3683 deg
Mean motion: 15
76486125 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1373
Checksum: 287
Coasting Arc #4 (Orbit 1388)
---------------------------------------
Vector Time (GMT): 2008/076/08:39:35
824
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4805954
48 A = 6725086
40 meter
Y = 4688826
27 meter E =
0011730
Z = 257717
65 I = 51
89260
XDOT = -3152
458610 Wp = 45
42848
YDOT = -3572
813702 meter/sec RA = 133
98166 deg
ZDOT = 6055
590172 TA = 317
36549
MA = 317
45647
Ha = 185
901 n
mi
Hp = 180
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15767567
19 X = -4859280
40
Y = 15383288
29 feet Y = 4634785
19 meter
Z = 845530
33 Z = 234241
14
XDOT = -10342
711976 XDOT = -3141
688983
YDOT = -11721
829730 feet/sec YDOT = -3608
005970 meter/sec
ZDOT = 19867
421824 ZDOT = 6040
302031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21530023
36 X = -6562351
12
Y = -4675799
08 feet Y = -1425183
56 meter
Z = 756076
80 Z = 230452
21
XDOT = 3673
142357 XDOT = 1119
573790
YDOT = -13615
599580 feet/sec YDOT = -4150
034752 meter/sec
ZDOT = 19808
385165 ZDOT = 6037
595798
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 08076
42378196
00020000 00000-0 20000-3 0 9033
2 25544 51
6386 134
5784 0001102 253
4245 106
6799 15
76490020 13895
Satellite: ISS
Catalog Number: 25544
Epoch time: 08076
42378196 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 134
5784 deg
Eccentricity:
0001102
Arg of perigee: 253
4245 deg
Mean anomaly: 106
6799 deg
Mean motion: 15
76490020 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1389
Checksum: 300
Coasting Arc #5 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2008/077/02:58:09
975
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5014214
52 A = 6724604
41 meter
Y = 4241978
73 meter E =
0013461
Z = 1410739
30 I = 51
90109
XDOT = -2177
939868 Wp = 55
39920
YDOT = -4528
355932 meter/sec RA = 130
07348 deg
ZDOT = 5843
640272 TA = 320
07831
MA = 320
17722
Ha = 186
092 n
mi
Hp = 180
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16450835
04 X = -5068129
30
Y = 13917253
04 feet Y = 4185605
52 meter
Z = 4628409
78 Z = 1386249
63
XDOT = -7145
472008 XDOT = -2155
527998
YDOT = -14856
810800 feet/sec YDOT = -4552
585376 meter/sec
ZDOT = 19172
048136 ZDOT = 5833
114655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4099637
11 X = 1249569
39
Y = -21174718
89 feet Y = -6454054
32 meter
Z = 4535012
51 Z = 1382271
81
XDOT = 13425
615064 XDOT = 4092
127472
YDOT = 6719
385269 feet/sec YDOT = 2048
068630 meter/sec
ZDOT = 19131
154617 ZDOT = 5831
175927
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 08077
18444470
00020000 00000-0 20000-3 0 9047
2 25544 51
6349 130
6579 0001372 303
5164 56
5870 15
76375007 14014
Satellite: ISS
Catalog Number: 25544
Epoch time: 08077
18444470 = yrday
fracday
Element set: 904
Inclination: 51
6349 deg
RA of node: 130
6579 deg
Eccentricity:
0001372
Arg of perigee: 303
5164 deg
Mean anomaly: 56
5870 deg
Mean motion: 15
76375007 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1401
Checksum: 283
Coasting Arc #6 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2008/078/02:58:09
975
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1512802
81 A = 6715221
68 meter
Y = 4437058
06 meter E =
0010762
Z = -4818103
00 I = 51
88751
XDOT = -5619
001141 Wp = 105
59023
YDOT = 4627
471793 meter/sec RA = 124
90411 deg
ZDOT = 2498
996509 TA = 188
77429
MA = 188
79312
Ha = 186
067 n
mi
Hp = 180
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4963263
80 X = 1486479
50
Y = 14557277
10 feet Y = 4453827
61 meter
Z = -15807424
53 Z = -4810818
17
XDOT = -18435
043112 XDOT = -5682
468061
YDOT = 15181
994072 feet/sec YDOT = 4564
282208 meter/sec
ZDOT = 8198
807443 ZDOT = 2471
545513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13206140
64 X = -4025231
67
Y = -7940093
43 feet Y = -2420140
48 meter
Z = -15778965
12 Z = -4809428
57
XDOT = 3884
560024 XDOT = 1184
013895
YDOT = -22534
364479 feet/sec YDOT = -6868
474293 meter/sec
ZDOT = 8094
094242 ZDOT = 2467
079925
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 08078
13533832
00020000 00000-0 20000-3 0 9055
2 25544 51
6346 125
7560 0001214 309
0067 51
0989 15
76421742 14169
Satellite: ISS
Catalog Number: 25544
Epoch time: 08078
13533832 = yrday
fracday
Element set: 905
Inclination: 51
6346 deg
RA of node: 125
7560 deg
Eccentricity:
0001214
Arg of perigee: 309
0067 deg
Mean anomaly: 51
0989 deg
Mean motion: 15
76421742 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1416
Checksum: 276
Coasting Arc #7 (Orbit 1431)
---------------------------------------
Vector Time (GMT): 2008/079/02:58:09
975
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4771276
89 A = 6721477
88 meter
Y = -3729728
55 meter E =
0003482
Z = -2917456
34 I = 51
92480
XDOT = 1328
619111 Wp = 106
35267
YDOT = 5651
584759 meter/sec RA = 119
81259 deg
ZDOT = -5058
137710 TA = 107
10540
MA = 107
06726
Ha = 186
048 n
mi
Hp = 180
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15653795
59 X = 4826800
91
Y = -12236642
24 feet Y = -3676063
21 meter
Z = -9571707
17 Z = -2894142
72
XDOT = 4358
986585 XDOT = 1289
894546
YDOT = 18541
944746 feet/sec YDOT = 5666
225185 meter/sec
ZDOT = -16594
939992 ZDOT = -5051
777938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3885752
66 X = -1184377
41
Y = 19528766
51 feet Y = 5952368
03 meter
Z = -9482748
14 Z = -2890341
63
XDOT = -14067
966499 XDOT = -4287
916189
YDOT = -10835
667106 feet/sec YDOT = -3302
711334 meter/sec
ZDOT = -16569
882389 ZDOT = -5050
500152
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 08079
14959544
00020000 00000-0 20000-3 0 9060
2 25544 51
6347 120
5283 0001269 320
2448 39
8623 15
76482643 14327
Satellite: ISS
Catalog Number: 25544
Epoch time: 08079
14959544 = yrday
fracday
Element set: 906
Inclination: 51
6347 deg
RA of node: 120
5283 deg
Eccentricity:
0001269
Arg of perigee: 320
2448 deg
Mean anomaly: 39
8623 deg
Mean motion: 15
76482643 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1432
Checksum: 299
Coasting Arc #8 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2008/080/02:43:09
822
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4407045
98 A = 6714345
53 meter
Y = 85597
04 meter E =
0004352
Z = 5061980
96 I = 51
91226
XDOT = 1854
067624 Wp = 114
84152
YDOT = -7277
287543 meter/sec RA = 114
72140 deg
ZDOT = 1734
295629 TA = 318
52977
MA = 318
56279
Ha = 186
516 n
mi
Hp = 180
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14458812
27 X = -4432265
45
Y = 280830
18 feet Y = 36174
43 meter
Z = 16607549
07 Z = 5040510
56
XDOT = 6082
899029 XDOT = 1926
880807
YDOT = -23875
615299 feet/sec YDOT = -7256
147005 meter/sec
ZDOT = 5689
946288 ZDOT = 1743
480160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11286554
89 X = 3440141
93
Y = -9191161
63 feet Y = -2801466
06 meter
Z = 16525224
07 Z = 5036888
30
XDOT = 9281
737266 XDOT = 2829
073519
YDOT = 21707
235836 feet/sec YDOT = 6616
365483 meter/sec
ZDOT = 5724
306632 ZDOT = 1744
768661
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 08080
16382840
00020000 00000-0 20000-3 0 9074
2 25544 51
6340 115
2994 0001299 343
8925 16
2197 15
76375205 14481
Satellite: ISS
Catalog Number: 25544
Epoch time: 08080
16382840 = yrday
fracday
Element set: 907
Inclination: 51
6340 deg
RA of node: 115
2994 deg
Eccentricity:
0001299
Arg of perigee: 343
8925 deg
Mean anomaly: 16
2197 deg
Mean motion: 15
76375205 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1448
Checksum: 297
Coasting Arc #9 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2008/081/02:43:09
822
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1702879
17 A = 6724977
06 meter
Y = 6460662
33 meter E =
0011327
Z = -714603
02 I = 51
96023
XDOT = -4779
770779 Wp = 35
44416
YDOT = -600
899536 meter/sec RA = 109
56626 deg
ZDOT = 6013
519018 TA = 316
79538
MA = 316
88418
Ha = 186
296 n
mi
Hp = 180
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5586873
93 X = -1771525
36
Y = 21196398
73 feet Y = 6441235
87 meter
Z = -2344498
09 Z = -723042
97
XDOT = -15681
662661 XDOT = -4801
908520
YDOT = -1971
455171 feet/sec YDOT = -654
472791 meter/sec
ZDOT = 19729
393103 ZDOT = 5990
245392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9021104
66 X = -2749632
70
Y = -19974257
21 feet Y = -6088153
60 meter
Z = -2376103
99 Z = -724236
50
XDOT = 12052
380988 XDOT = 3673
565725
YDOT = -7758
027604 feet/sec YDOT = -2364
646814 meter/sec
ZDOT = 19640
070762 ZDOT = 5986
293568
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 08081
11470237
00020000 00000-0 20000-3 0 9089
2 25544 51
6343 110
3975 0001100 348
1355 11
9783 15
76451590 14637
Satellite: ISS
Catalog Number: 25544
Epoch time: 08081
11470237 = yrday
fracday
Element set: 908
Inclination: 51
6343 deg
RA of node: 110
3975 deg
Eccentricity:
0001100
Arg of perigee: 348
1355 deg
Mean anomaly: 11
9783 deg
Mean motion: 15
76451590 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1463
Checksum: 268
Coasting Arc #10 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2008/082/02:43:09
822
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3971695
30 A = 6712984
36 meter
Y = 1195818
80 meter E =
0015079
Z = -5291071
58 I = 51
92890
XDOT = -2033
076130 Wp = 87
14960
YDOT = 7419
085647 meter/sec RA = 104
43936 deg
ZDOT = 151
756138 TA = 184
27959
MA = 184
29250
Ha = 186
294 n
mi
Hp = 180
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13030496
39 X = 3983731
26
Y = 3923290
02 feet Y = 1240299
30 meter
Z = -17359158
71 Z = -5271748
04
XDOT = -6670
197278 XDOT = -2116
623597
YDOT = 24340
832176 feet/sec YDOT = 7395
883507 meter/sec
ZDOT = 497
887593 ZDOT = 141
675768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12576902
20 X = -3833439
79
Y = 5438719
79 feet Y = 1657721
79 meter
Z = -17284915
10 Z = -5268442
12
XDOT = -10147
008591 XDOT = -3092
808218
YDOT = -22013
996677 feet/sec YDOT = -6709
866187 meter/sec
ZDOT = 460
096137 ZDOT = 140
237302
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 08082
12893986
00020000 00000-0 20000-3 0 9092
2 25544 51
6344 105
1694 0001060 359
9962
1202 15
76503729 14792
Satellite: ISS
Catalog Number: 25544
Epoch time: 08082
12893986 = yrday
fracday
Element set: 909
Inclination: 51
6344 deg
RA of node: 105
1694 deg
Eccentricity:
0001060
Arg of perigee: 359
9962 deg
Mean anomaly:
1202 deg
Mean motion: 15
76503729 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1479
Checksum: 296
Coasting Arc #11 (Orbit 1494)
---------------------------------------
Vector Time (GMT): 2008/083/02:43:09
822
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1835209
02 A = 6724430
30 meter
Y = -6388718
78 meter E =
0008959
Z = -993316
59 I = 51
97391
XDOT = 4367
124138 Wp = 136
73378
YDOT = 2175
442675 meter/sec RA = 99
31608 deg
ZDOT = -5961
088057 TA = 54
08025
MA = 53
99714
Ha = 186
212 n
mi
Hp = 179
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6021026
97 X = 1911337
63
Y = -20960363
46 feet Y = -6367770
86 meter
Z = -3258912
70 Z = -984215
61
XDOT = 14327
835098 XDOT = 4371
431346
YDOT = 7137
279116 feet/sec YDOT = 2224
301866 meter/sec
ZDOT = -19557
375515 ZDOT = -5939
862295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9196333
61 X = 2803042
49
Y = 19779751
30 feet Y = 6028868
20 meter
Z = -3224748
14 Z = -982903
23
XDOT = -14136
455761 XDOT = -4308
791716
YDOT = 3417
805989 feet/sec YDOT = 1041
747265 meter/sec
ZDOT = -19475
724782 ZDOT = -5936
200914
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 08083
14314534
00020000 00000-0 20000-3 0 9104
2 25544 51
6341 99
9396 0001256
8757 359
2409 15
76577409 14950
Satellite: ISS
Catalog Number: 25544
Epoch time: 08083
14314534 = yrday
fracday
Element set: 910
Inclination: 51
6341 deg
RA of node: 99
9396 deg
Eccentricity:
0001256
Arg of perigee:
8757 deg
Mean anomaly: 359
2409 deg
Mean motion: 15
76577409 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1495
Checksum: 306
Coasting Arc #12 (Orbit 1510)
---------------------------------------
Vector Time (GMT): 2008/084/02:43:09
822
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3704085
46 A = 6714271
85 meter
Y = -2595444
71 meter E =
0006910
Z = 4959161
66 I = 51
94303
XDOT = 2159
793667 Wp = 50
64939
YDOT = -7096
207800 meter/sec RA = 94
15664 deg
ZDOT = -2094
495100 TA = 59
57352
MA = 59
50526
Ha = 186
409 n
mi
Hp = 179
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12152511
34 X = -3698878
31
Y = -8515238
54 feet Y = -2636836
40 meter
Z = 16270215
41 Z = 4941179
99
XDOT = 7085
937228 XDOT = 2249
158768
YDOT = -23281
521653 feet/sec YDOT = -7071
556251 meter/sec
ZDOT = -6871
703085 ZDOT = -2083
785154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14797562
52 X = 4510297
06
Y = -1863802
22 feet Y = -568086
92 meter
Z = 16200960
27 Z = 4938052
69
XDOT = 10145
615607 XDOT = 3092
383637
YDOT = 20990
872943 feet/sec YDOT = 6398
018073 meter/sec
ZDOT = -6831
438092 ZDOT = -2082
222331
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 08084
15732313
00020000 00000-0 20000-3 0 9116
2 25544 51
6343 94
7105 0001017 13
6170 346
5022 15
76552248 15112
Satellite: ISS
Catalog Number: 25544
Epoch time: 08084
15732313 = yrday
fracday
Element set: 911
Inclination: 51
6343 deg
RA of node: 94
7105 deg
Eccentricity:
0001017
Arg of perigee: 13
6170 deg
Mean anomaly: 346
5022 deg
Mean motion: 15
76552248 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1511
Checksum: 250
Coasting Arc #13 (Orbit 1526)
---------------------------------------
Vector Time (GMT): 2008/085/02:43:09
822
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1953631
37 A = 6721633
49 meter
Y = 5865667
32 meter E =
0014156
Z = 2620282
56 I = 51
97113
XDOT = -4184
926806 Wp = 73
89363
YDOT = -3757
443766 meter/sec RA = 89
06275 deg
ZDOT = 5271
600012 TA = 315
80232
MA = 315
91532
Ha = 186
134 n
mi
Hp = 179
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6409551
73 X = -2031805
91
Y = 19244315
36 feet Y = 5843383
76 meter
Z = 8596727
54 Z = 2610601
53
XDOT = -13730
074824 XDOT = -4168
208088
YDOT = -12327
571410 feet/sec YDOT = -3804
148223 meter/sec
ZDOT = 17295
275631 ZDOT = 5251
310346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8394949
99 X = -2558780
76
Y = -18481789
87 feet Y = -5633249
55 meter
Z = 8560257
54 Z = 2609166
50
XDOT = 17173
009479 XDOT = 5234
333289
YDOT = 203
715590 feet/sec YDOT = 62
092512 meter/sec
ZDOT = 17217
041565 ZDOT = 5247
754269
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 08085
17146504
00020000 00000-0 20000-3 0 9121
2 25544 51
6356 89
4816 0000916 11
0417 349
0768 15
76668001 15276
Satellite: ISS
Catalog Number: 25544
Epoch time: 08085
17146504 = yrday
fracday
Element set: 912
Inclination: 51
6356 deg
RA of node: 89
4816 deg
Eccentricity:
0000916
Arg of perigee: 11
0417 deg
Mean anomaly: 349
0768 deg
Mean motion: 15
76668001 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1527
Checksum: 289
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 may contain past, current and future orbital data 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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