Date:
September 10th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8557 31 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 1914)
---------------------------------------
Vector Time (GMT): 2009/251/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3910126
75 A = 6720279
30 meter
Y = -1646203
92 meter E =
0012099
Z = 5202819
97 I = 51
33954
XDOT = 3791
949676 Wp = 66
10116
YDOT = 6672
411274 meter/sec RA = 236
01151 deg
ZDOT = -732
431139 TA = 30
92264
MA = 30
85145
Ha = 193
197 n
mi
Hp = 180
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12828499
84 X = 3902969
65
Y = -5400931
50 feet Y = -1602518
36 meter
Z = 17069619
32 Z = 5221798
26
XDOT = 12440
779777 XDOT = 3720
613851
YDOT = 21891
113103 feet/sec YDOT = 6714
416191 meter/sec
ZDOT = -2402
989302 ZDOT = -714
183249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13446763
72 X = 4098573
58
Y = 3220825
73 feet Y = 981707
68 meter
Z = 17144188
52 Z = 5225548
66
XDOT = -2757
662861 XDOT = -840
535640
YDOT = 24027
054105 feet/sec YDOT = 7323
446091 meter/sec
ZDOT = -2330
777382 ZDOT = -710
420946
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 09251
98034546
00020000 00000-0 20000-3 0 9005
2 25544 51
6371 236
6914 0009055 67
2252 292
9867 15
73993008 19153
Satellite: ISS
Catalog Number: 25544
Epoch time: 09251
98034546 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 236
6914 deg
Eccentricity:
0009055
Arg of perigee: 67
2252 deg
Mean anomaly: 292
9867 deg
Mean motion: 15
73993008 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1915
Checksum: 310
Coasting Arc #2 (Orbit 1930)
---------------------------------------
Vector Time (GMT): 2009/252/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3807373
35 A = 6731939
52 meter
Y = -5502554
91 meter E =
0022062
Z = 650482
63 I = 51
39625
XDOT = 4310
157338 Wp = 59
70160
YDOT = -2259
655261 meter/sec RA = 230
86811 deg
ZDOT = 5973
790396 TA = 307
41054
MA = 307
61115
Ha = 193
278 n
mi
Hp = 180
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12491382
38 X = -3748719
82
Y = -18053001
66 feet Y = -5544803
23 meter
Z = 2134129
37 Z = 632128
82
XDOT = 14140
936149 XDOT = 4306
084937
YDOT = -7413
567128 feet/sec YDOT = -2211
479168 meter/sec
ZDOT = 19599
049857 ZDOT = 5994
719533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 294539
89 X = 89775
76
Y = -21958214
73 feet Y = -6692863
85 meter
Z = 2061568
12 Z = 628365
96
XDOT = 14123
743842 XDOT = 4304
917123
YDOT = 2081
683885 feet/sec YDOT = 634
497248 meter/sec
ZDOT = 19681
262228 ZDOT = 5998
848727
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 09252
99616078
00020000 00000-0 20000-3 0 9014
2 25544 51
6365 231
4734 0009059 71
2183 288
9962 15
74027763 19317
Satellite: ISS
Catalog Number: 25544
Epoch time: 09252
99616078 = yrday
fracday
Element set: 901
Inclination: 51
6365 deg
RA of node: 231
4734 deg
Eccentricity:
0009059
Arg of perigee: 71
2183 deg
Mean anomaly: 288
9962 deg
Mean motion: 15
74027763 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1931
Checksum: 313
Coasting Arc #3 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2009/253/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3610745
30 A = 6720156
48 meter
Y = 2265938
37 meter E =
0023536
Z = -5215232
30 I = 51
37655
XDOT = -4858
014042 Wp = 88
53138
YDOT = -5898
466788 meter/sec RA = 225
70065 deg
ZDOT = 804
355177 TA = 189
14747
MA = 189
19042
Ha = 193
306 n
mi
Hp = 180
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11846277
24 X = -3610480
17
Y = 7434181
01 feet Y = 2225562
36 meter
Z = -17110342
18 Z = -5232772
82
XDOT = -15938
366280 XDOT = -4795
602757
YDOT = -19351
925158 feet/sec YDOT = -5952
442995 meter/sec
ZDOT = 2638
960556 ZDOT = 780
906353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13891166
86 X = -4234027
66
Y = -524206
86 feet Y = -159778
25 meter
Z = -17179226
75 Z = -5236228
31
XDOT = -2229
401044 XDOT = -679
521438
YDOT = -23971
188225 feet/sec YDOT = -7306
418171 meter/sec
ZDOT = 2546
317747 ZDOT = 776
117649
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 09253
94847576
00020000 00000-0 20000-3 0 9020
2 25544 51
6364 226
5818 0009154 75
7419 284
4761 15
74053921 19460
Satellite: ISS
Catalog Number: 25544
Epoch time: 09253
94847576 = yrday
fracday
Element set: 902
Inclination: 51
6364 deg
RA of node: 226
5818 deg
Eccentricity:
0009154
Arg of perigee: 75
7419 deg
Mean anomaly: 284
4761 deg
Mean motion: 15
74053921 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1946
Checksum: 322
Coasting Arc #4 (Orbit 1961)
---------------------------------------
Vector Time (GMT): 2009/254/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4657764
56 A = 6731593
55 meter
Y = 4794858
36 meter E =
0016877
Z = -770008
12 I = 51
43759
XDOT = -3933
999673 Wp = 111
93776
YDOT = 2882
765100 meter/sec RA = 220
56198 deg
ZDOT = -5955
988499 TA = 76
47750
MA = 76
28952
Ha = 193
236 n
mi
Hp = 180
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15281379
80 X = 4607542
03
Y = 15731162
61 feet Y = 4846663
43 meter
Z = -2526273
35 Z = -747502
52
XDOT = -12906
823075 XDOT = -3937
009602
YDOT = 9457
890747 feet/sec YDOT = 2838
756035 meter/sec
ZDOT = -19540
644683 ZDOT = -5975
107248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4070891
25 X = 1240807
65
Y = 21560589
72 feet Y = 6571667
75 meter
Z = -2437399
88 Z = -742919
48
XDOT = -14315
459645 XDOT = -4363
352100
YDOT = 527
810901 feet/sec YDOT = 160
876763 meter/sec
ZDOT = -19615
709032 ZDOT = -5978
868113
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 09254
96426411
00020000 00000-0 20000-3 0 9035
2 25544 51
6364 221
3641 0009169 78
0982 282
1209 15
74119778 19627
Satellite: ISS
Catalog Number: 25544
Epoch time: 09254
96426411 = yrday
fracday
Element set: 903
Inclination: 51
6364 deg
RA of node: 221
3641 deg
Eccentricity:
0009169
Arg of perigee: 78
0982 deg
Mean anomaly: 282
1209 deg
Mean motion: 15
74119778 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1962
Checksum: 304
Coasting Arc #5 (Orbit 1977)
---------------------------------------
Vector Time (GMT): 2009/255/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3235704
74 A = 6720194
02 meter
Y = -2774867
82 meter E =
0012399
Z = 5185272
95 I = 51
42146
XDOT = 5785
029039 Wp = 77
49880
YDOT = 5013
307515 meter/sec RA = 215
39527 deg
ZDOT = -922
625234 TA = 21
33159
MA = 21
27996
Ha = 193
276 n
mi
Hp = 180
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10615829
20 X = 3241304
19
Y = -9103897
06 feet Y = -2738653
03 meter
Z = 17012050
36 Z = 5201005
57
XDOT = 18979
754065 XDOT = 5733
021359
YDOT = 16447
859301 feet/sec YDOT = 5077
708332 meter/sec
ZDOT = -3026
985677 ZDOT = -894
647827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13761519
28 X = 4194511
08
Y = -2023001
99 feet Y = -616611
01 meter
Z = 17073800
95 Z = 5204094
53
XDOT = 7029
317688 XDOT = 2142
536031
YDOT = 23077
867513 feet/sec YDOT = 7034
134018 meter/sec
ZDOT = -2916
546954 ZDOT = -888
963511
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 09255
98004236
00020000 00000-0 20000-3 0 9046
2 25544 51
6357 216
1462 0009255 83
9063 276
3155 15
74055798 19786
Satellite: ISS
Catalog Number: 25544
Epoch time: 09255
98004236 = yrday
fracday
Element set: 904
Inclination: 51
6357 deg
RA of node: 216
1462 deg
Eccentricity:
0009255
Arg of perigee: 83
9063 deg
Mean anomaly: 276
3155 deg
Mean motion: 15
74055798 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1978
Checksum: 314
Coasting Arc #6 (Orbit 1993)
---------------------------------------
Vector Time (GMT): 2009/256/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5394734
19 A = 6731525
76 meter
Y = -3923962
11 meter E =
0021737
Z = 842641
92 I = 51
48616
XDOT = 3463
501689 Wp = 67
86073
YDOT = -3459
859673 meter/sec RA = 210
26149 deg
ZDOT = 5948
281053 TA = 301
35562
MA = 301
56814
Ha = 193
232 n
mi
Hp = 180
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17699259
14 X = -5354548
20
Y = -12873891
43 feet Y = -3984064
51 meter
Z = 2764573
24 Z = 816532
04
XDOT = 11363
194517 XDOT = 3473
037482
YDOT = -11351
245646 feet/sec YDOT = -3421
075440 meter/sec
ZDOT = 19515
357784 ZDOT = 5965
129828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8366438
77 X = -2550090
54
Y = -20237654
02 feet Y = -6168436
95 meter
Z = 2661537
51 Z = 811236
63
XDOT = 14048
796732 XDOT = 4282
073244
YDOT = -3181
584863 feet/sec YDOT = -969
747066 meter/sec
ZDOT = 19581
463439 ZDOT = 5968
430056
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 09256
99580249
00020000 00000-0 20000-3 0 9052
2 25544 51
6365 210
9284 0009187 88
4338 271
7877 15
74132542 19949
Satellite: ISS
Catalog Number: 25544
Epoch time: 09256
99580249 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node: 210
9284 deg
Eccentricity:
0009187
Arg of perigee: 88
4338 deg
Mean anomaly: 271
7877 deg
Mean motion: 15
74132542 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1994
Checksum: 333
Coasting Arc #7 (Orbit 2008)
---------------------------------------
Vector Time (GMT): 2009/257/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2822513
02 A = 6720043
54 meter
Y = 3239055
56 meter E =
0023744
Z = -5187972
19 I = 51
47472
XDOT = -6493
222194 Wp = 95
92476
YDOT = -3969
624038 meter/sec RA = 205
09718 deg
ZDOT = 1055
972641 TA = 184
18314
MA = 184
20303
Ha = 193
242 n
mi
Hp = 180
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9260213
34 X = -2833320
90
Y = 10626822
72 feet Y = 3207432
00 meter
Z = -17020906
15 Z = -5201710
19
XDOT = -21303
222420 XDOT = -6453
480265
YDOT = -13023
700911 feet/sec YDOT = -4042
012832 meter/sec
ZDOT = 3464
477169 ZDOT = 1024
525453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13290307
32 X = -4050885
67
Y = 4495742
11 feet Y = 1370302
20 meter
Z = -17074782
35 Z = -5204393
66
XDOT = -11416
581230 XDOT = -3479
773959
YDOT = -21084
359493 feet/sec YDOT = -6426
512773 meter/sec
ZDOT = 3340
408457 ZDOT = 1018
156498
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 09257
94806675
00020000 00000-0 20000-3 0 9063
2 25544 51
6371 206
0374 0009267 91
9900 268
2324 15
74144298 20092
Satellite: ISS
Catalog Number: 25544
Epoch time: 09257
94806675 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 206
0374 deg
Eccentricity:
0009267
Arg of perigee: 91
9900 deg
Mean anomaly: 268
2324 deg
Mean motion: 15
74144298 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2009
Checksum: 307
Coasting Arc #8 (Orbit 2024)
---------------------------------------
Vector Time (GMT): 2009/258/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5928532
59 A = 6731222
00 meter
Y = 3013035
29 meter E =
0017518
Z = -1016391
59 I = 51
54019
XDOT = -2989
617892 Wp = 119
55201
YDOT = 3914
782293 meter/sec RA = 199
96822 deg
ZDOT = -5917
710304 TA = 71
57240
MA = 71
38203
Ha = 193
172 n
mi
Hp = 180
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19450566
24 X = 5899337
09
Y = 9885286
37 feet Y = 3079168
33 meter
Z = -3334618
07 Z = -987662
11
XDOT = -9808
457651 XDOT = -3004
424547
YDOT = 12843
773927 feet/sec YDOT = 3881
267512 meter/sec
ZDOT = -19415
060053 ZDOT = -5932
269922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12058270
90 X = 3675360
97
Y = 18203967
76 feet Y = 5548569
37 meter
Z = -3221296
61 Z = -981851
21
XDOT = -13442
010552 XDOT = -4097
124816
YDOT = 5509
131097 feet/sec YDOT = 1679
183158 meter/sec
ZDOT = -19472
127390 ZDOT = -5935
104429
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 09258
96379983
00020000 00000-0 20000-3 0 9074
2 25544 51
6369 200
8181 0009195 94
9427 265
2786 15
74187583 20255
Satellite: ISS
Catalog Number: 25544
Epoch time: 09258
96379983 = yrday
fracday
Element set: 907
Inclination: 51
6369 deg
RA of node: 200
8181 deg
Eccentricity:
0009195
Arg of perigee: 94
9427 deg
Mean anomaly: 265
2786 deg
Mean motion: 15
74187583 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2025
Checksum: 341
Coasting Arc #9 (Orbit 2040)
---------------------------------------
Vector Time (GMT): 2009/259/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2373282
33 A = 6720126
35 meter
Y = -3599959
28 meter E =
0012507
Z = 5143816
79 I = 51
53209
XDOT = 7046
766878 Wp = 86
83723
YDOT = 2876
967267 meter/sec RA = 194
80438 deg
ZDOT = -1234
548134 TA = 14
98073
MA = 14
94372
Ha = 193
174 n
mi
Hp = 180
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7786359
34 X = 2388373
73
Y = -11810890
03 feet Y = -3573335
04 meter
Z = 16876039
33 Z = 5155383
07
XDOT = 23119
313905 XDOT = 7020
069576
YDOT = 9438
868985 feet/sec YDOT = 2955
618988 meter/sec
ZDOT = -4050
354771 ZDOT = -1200
380244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12400614
50 X = 3779707
30
Y = -6694639
61 feet Y = -2040526
15 meter
Z = 16921340
94 Z = 5157624
72
XDOT = 15320
420900 XDOT = 4669
664290
YDOT = 18454
357994 feet/sec YDOT = 5624
888316 meter/sec
ZDOT = -3915
615307 ZDOT = -1193
479545
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 09259
97952116
00020000 00000-0 20000-3 0 9082
2 25544 51
6378 195
6005 0009308 99
3984 260
8231 15
74152675 20412
Satellite: ISS
Catalog Number: 25544
Epoch time: 09259
97952116 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 195
6005 deg
Eccentricity:
0009308
Arg of perigee: 99
3984 deg
Mean anomaly: 260
8231 deg
Mean motion: 15
74152675 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2041
Checksum: 316
Coasting Arc #10 (Orbit 2056)
---------------------------------------
Vector Time (GMT): 2009/260/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6318628
65 A = 6731011
57 meter
Y = -1997126
12 meter E =
0021254
Z = 1142858
99 I = 51
60007
XDOT = 2446
000937 Wp = 75
82754
YDOT = -4318
790768 meter/sec RA = 189
68373 deg
ZDOT = 5890
440452 TA = 296
69721
MA = 296
91464
Ha = 193
086 n
mi
Hp = 180
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20730408
96 X = -6301378
62
Y = -6552251
05 feet Y = -2067688
18 meter
Z = 3749537
38 Z = 1112205
24
XDOT = 8024
937456 XDOT = 2465
497949
YDOT = -14169
261050 feet/sec YDOT = -4291
328548 meter/sec
ZDOT = 19325
592033 ZDOT = 5902
370892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15357420
77 X = -4680941
85
Y = -15418272
92 feet Y = -4699489
58 meter
Z = 3628686
76 Z = 1106023
72
XDOT = 12450
342997 XDOT = 3794
864546
YDOT = -7773
346382 feet/sec YDOT = -2369
315977 meter/sec
ZDOT = 19372
278401 ZDOT = 5904
670457
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 09260
99522376
00020000 00000-0 20000-3 0 9098
2 25544 51
6393 190
3831 0009229 103
8716 256
3475 15
74226643 20578
Satellite: ISS
Catalog Number: 25544
Epoch time: 09260
99522376 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 190
3831 deg
Eccentricity:
0009229
Arg of perigee: 103
8716 deg
Mean anomaly: 256
3475 deg
Mean motion: 15
74226643 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2057
Checksum: 308
Coasting Arc #11 (Orbit 2071)
---------------------------------------
Vector Time (GMT): 2009/261/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1915525
19 A = 6720042
89 meter
Y = 3925862
45 meter E =
0023208
Z = -5127103
93 I = 51
59334
XDOT = -7351
186368 Wp = 103
52692
YDOT = -1718
893174 meter/sec RA = 184
52190 deg
ZDOT = 1430
377935 TA = 180
21503
MA = 180
21603
Ha = 193
013 n
mi
Hp = 180
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6284531
46 X = -1934375
83
Y = 12880126
15 feet Y = 3904335
99 meter
Z = -16821207
10 Z = -5136455
78
XDOT = -24118
065512 XDOT = -7338
367600
YDOT = -5639
413301 feet/sec YDOT = -1801
026647 meter/sec
ZDOT = 4692
840994 ZDOT = 1394
697023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11299335
02 X = -3444037
31
Y = 8745668
24 feet Y = 2665679
68 meter
Z = -16857767
02 Z = -5138247
39
XDOT = -18425
253447 XDOT = -5616
017250
YDOT = -15031
208067 feet/sec YDOT = -4581
512219 meter/sec
ZDOT = 4552
205277 ZDOT = 1387
512169
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 09261
94743389
00020000 00000-0 20000-3 0 9105
2 25544 51
6395 185
4924 0009200 106
9838 253
2334 15
74247746 20720
Satellite: ISS
Catalog Number: 25544
Epoch time: 09261
94743389 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 185
4924 deg
Eccentricity:
0009200
Arg of perigee: 106
9838 deg
Mean anomaly: 253
2334 deg
Mean motion: 15
74247746 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2072
Checksum: 307
Coasting Arc #12 (Orbit 2087)
---------------------------------------
Vector Time (GMT): 2009/262/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6506528
53 A = 6730655
03 meter
Y = 1016044
54 meter E =
0017304
Z = -1369668
78 I = 51
65921
XDOT = -1939
427477 Wp = 126
85820
YDOT = 4635
423676 meter/sec RA = 179
40741 deg
ZDOT = -5835
207188 TA = 68
18928
MA = 68
00528
Ha = 192
986 n
mi
Hp = 180
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21346878
37 X = 6501337
03
Y = 3333479
47 feet Y = 1088775
22 meter
Z = -4493663
97 Z = -1338072
45
XDOT = -6362
951041 XDOT = -1962
770764
YDOT = 15208
082927 feet/sec YDOT = 4613
604780 meter/sec
ZDOT = -19144
380539 ZDOT = -5844
686167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17830209
25 X = 5434647
78
Y = 12246976
29 feet Y = 3732878
37 meter
Z = -4369156
34 Z = -1331718
85
XDOT = -11319
216576 XDOT = -3450
097212
YDOT = 9709
546539 feet/sec YDOT = 2959
469785 meter/sec
ZDOT = -19181
395821 ZDOT = -5846
489446
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 09262
96310935
00020000 00000-0 20000-3 0 9116
2 25544 51
6397 180
2735 0009140 110
7724 249
4419 15
74263060 20880
Satellite: ISS
Catalog Number: 25544
Epoch time: 09262
96310935 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 180
2735 deg
Eccentricity:
0009140
Arg of perigee: 110
7724 deg
Mean anomaly: 249
4419 deg
Mean motion: 15
74263060 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2088
Checksum: 288
Coasting Arc #13 (Orbit 2103)
---------------------------------------
Vector Time (GMT): 2009/263/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1445015
69 A = 6720174
20 meter
Y = -4167721
14 meter E =
0012430
Z = 5058956
07 I = 51
65463
XDOT = 7506
087358 Wp = 94
00601
YDOT = 571
636019 meter/sec RA = 174
24545 deg
ZDOT = -1670
421352 TA = 12
04319
MA = 12
01350
Ha = 192
874 n
mi
Hp = 180
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4740865
12 X = 1466936
62
Y = -13673625
79 feet Y = -4151439
16 meter
Z = 16597624
89 Z = 5066029
63
XDOT = 24626
270861 XDOT = 7507
252073
YDOT = 1875
446258 feet/sec YDOT = 655
579887 meter/sec
ZDOT = -5480
385012 ZDOT = -1633
953482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9920585
19 X = 3023794
37
Y = -10493311
52 feet Y = -3198361
35 meter
Z = 16625203
74 Z = 5067362
10
XDOT = 20866
907408 XDOT = 6360
233378
YDOT = 11258
951199 feet/sec YDOT = 3431
728325 meter/sec
ZDOT = -5336
713357 ZDOT = -1626
630231
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 09263
97877011
00020000 00000-0 20000-3 0 9122
2 25544 51
6402 175
0562 0009119 114
0033 246
2085 15
74277399 21046
Satellite: ISS
Catalog Number: 25544
Epoch time: 09263
97877011 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 175
0562 deg
Eccentricity:
0009119
Arg of perigee: 114
0033 deg
Mean anomaly: 246
2085 deg
Mean motion: 15
74277399 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2104
Checksum: 280
Coasting Arc #14 (Orbit 2119)
---------------------------------------
Vector Time (GMT): 2009/264/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6543461
26 A = 6730320
11 meter
Y = 8841
92 meter E =
0020633
Z = 1551175
34 I = 51
71861
XDOT = 1377
523986 Wp = 83
83285
YDOT = -4905
704475 meter/sec RA = 169
13949 deg
ZDOT = 5775
648234 TA = 293
25565
MA = 293
47275
Ha = 192
842 n
mi
Hp = 180
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21468048
75 X = -6550609
25
Y = 29008
91 feet Y = -64370
79 meter
Z = 5089157
95 Z = 1519369
35
XDOT = 4519
435649 XDOT = 1404
220540
YDOT = -16094
830955 feet/sec YDOT = -4890
150580 meter/sec
ZDOT = 18948
977145 ZDOT = 5782
405488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19703848
15 X = -6005732
92
Y = -8596265
39 feet Y = -2620141
69 meter
Z = 4963877
17 Z = 1512989
76
XDOT = 9867
538497 XDOT = 3007
625734
YDOT = -11537
750171 feet/sec YDOT = -3516
706252 meter/sec
ZDOT = 18975
267470 ZDOT = 5783
661525
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 09264
99441452
00020000 00000-0 20000-3 0 9132
2 25544 51
6403 169
8383 0009119 117
9523 242
2564 15
74306674 21200
Satellite: ISS
Catalog Number: 25544
Epoch time: 09264
99441452 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 169
8383 deg
Eccentricity:
0009119
Arg of perigee: 117
9523 deg
Mean anomaly: 242
2564 deg
Mean motion: 15
74306674 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2120
Checksum: 294
Coasting Arc #15 (Orbit 2134)
---------------------------------------
Vector Time (GMT): 2009/265/22:24:46
878
Vector Time (MET): N/A
Weight (LBS) : 710966
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -976965
52 A = 6720290
27 meter
Y = 4394549
96 meter E =
0022016
Z = -5009450
21 I = 51
71431
XDOT = -7418
918393 Wp = 111
55361
YDOT = 548
203683 meter/sec RA = 163
97789 deg
ZDOT = 1926
622267 TA = 177
07992
MA = 177
06705
Ha = 192
697 n
mi
Hp = 180
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3205267
46 X = -1001698
15
Y = 14417814
82 feet Y = 4383486
47 meter
Z = -16435204
09 Z = -5014256
63
XDOT = -24340
283440 XDOT = -7433
856431
YDOT = 1798
568515 feet/sec YDOT = 465
157525 meter/sec
ZDOT = 6320
939197 ZDOT = 1890
544310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8424358
32 X = -2567744
42
Y = 12106363
35 feet Y = 3690019
55 meter
Z = -16453850
93 Z = -5015133
76
XDOT = -22304
866997 XDOT = -6798
523461
YDOT = -7118
209975 feet/sec YDOT = -2169
630400 meter/sec
ZDOT = 6178
853526 ZDOT = 1883
314555
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 09265
94656764
00020000 00000-0 20000-3 0 9143
2 25544 51
6401 164
9471 0009072 121
4659 238
7392 15
74349573 21350
Satellite: ISS
Catalog Number: 25544
Epoch time: 09265
94656764 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 164
9471 deg
Eccentricity:
0009072
Arg of perigee: 121
4659 deg
Mean anomaly: 238
7392 deg
Mean motion: 15
74349573 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2135
Checksum: 315
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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