Date:
October 16th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4036 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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
There are no maneuvers
Coasting Arc #1 (Orbit 1229)
---------------------------------------
Vector Time (GMT): 2006/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4337356
60 A = 6712713
23 meter
Y = 961070
70 meter E =
0025986
Z = -5054787
58 I = 51
30375
XDOT = 232
027837 Wp = 89
02728
YDOT = -7507
390280 meter/sec RA = 281
80175 deg
ZDOT = -1633
286329 TA = 165
21230
MA = 165
13615
Ha = 190
271 n
mi
Hp = 174
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14230172
57 X = -4323225
65
Y = 3153119
11 feet Y = 912646
82 meter
Z = -16583948
74 Z = -5075824
30
XDOT = 761
246184 XDOT = 323
893535
YDOT = -24630
545537 feet/sec YDOT = -7504
282022 meter/sec
ZDOT = -5358
550949 ZDOT = -1631
935744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11612635
21 X = 3539531
21
Y = -8659365
61 feet Y = -2639374
64 meter
Z = -16662215
28 Z = -5078643
22
XDOT = 8719
324055 XDOT = 2657
649972
YDOT = 21953
397536 feet/sec YDOT = 6691
395569 meter/sec
ZDOT = -5354
533629 ZDOT = -1632
061850
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 06289
51866449
00020000 00000-0 20000-3 0 9007
2 25544 51
6310 282
3685 0012875 101
3794 258
8818 15
76909084 12305
Satellite: ISS
Catalog Number: 25544
Epoch time: 06289
51866449 = yrday
fracday
Element set: 900
Inclination: 51
6310 deg
RA of node: 282
3685 deg
Eccentricity:
0012875
Arg of perigee: 101
3794 deg
Mean anomaly: 258
8818 deg
Mean motion: 15
76909084 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1230
Checksum: 314
Coasting Arc #2 (Orbit 1245)
---------------------------------------
Vector Time (GMT): 2006/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -423169
85 A = 6723711
00 meter
Y = 6687102
77 meter E =
0025238
Z = 435529
89 I = 51
33643
XDOT = -4842
945814 Wp = 117
51248
YDOT = 100
693600 meter/sec RA = 276
60205 deg
ZDOT = -5998
259999 TA = 57
72250
MA = 57
47823
Ha = 190
172 n
mi
Hp = 174
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1388352
53 X = -500030
26
Y = 21939313
53 feet Y = 6681940
92 meter
Z = 1428903
84 Z = 433287
10
XDOT = -15888
929835 XDOT = -4814
573108
YDOT = 330
359579 feet/sec YDOT = 46
695448 meter/sec
ZDOT = -19679
330705 ZDOT = -6021
718334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8050835
55 X = -2453894
67
Y = -20456448
17 feet Y = -6235125
40 meter
Z = 1421457
88 Z = 433260
36
XDOT = 12655
053265 XDOT = 3857
260235
YDOT = -6412
098820 feet/sec YDOT = -1954
407720 meter/sec
ZDOT = -19766
739424 ZDOT = -6024
902176
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 06290
53260399
00020000 00000-0 20000-3 0 9014
2 25544 51
6306 277
1372 0012853 104
5429 255
7162 15
76953820 12463
Satellite: ISS
Catalog Number: 25544
Epoch time: 06290
53260399 = yrday
fracday
Element set: 901
Inclination: 51
6306 deg
RA of node: 277
1372 deg
Eccentricity:
0012853
Arg of perigee: 104
5429 deg
Mean anomaly: 255
7162 deg
Mean motion: 15
76953820 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1246
Checksum: 289
Coasting Arc #3 (Orbit 1261)
---------------------------------------
Vector Time (GMT): 2006/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4150260
94 A = 6711779
75 meter
Y = 792053
30 meter E =
0014943
Z = 5202106
51 I = 51
29374
XDOT = -686
774963 Wp = 100
68347
YDOT = 7662
203386 meter/sec RA = 271
41930 deg
ZDOT = -619
943544 TA = 355
21756
MA = 355
23182
Ha = 189
983 n
mi
Hp = 174
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13616341
66 X = 4115824
40
Y = 2598600
05 feet Y = 838271
57 meter
Z = 17067278
58 Z = 5222185
05
XDOT = -2253
198697 XDOT = -769
392128
YDOT = 25138
462554 feet/sec YDOT = 7654
061517 meter/sec
ZDOT = -2033
935511 ZDOT = -623
481061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13285589
29 X = -4049447
62
Y = 3617604
98 feet Y = 1102646
00 meter
Z = 17142214
91 Z = 5224947
10
XDOT = -8786
237901 XDOT = -2678
045312
YDOT = -22591
049375 feet/sec YDOT = -6885
751850 meter/sec
ZDOT = -2046
066554 ZDOT = -623
641086
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 06291
54652873
00020000 00000-0 20000-3 0 9029
2 25544 51
6300 271
9063 0012715 108
6048 251
6499 15
76964434 12624
Satellite: ISS
Catalog Number: 25544
Epoch time: 06291
54652873 = yrday
fracday
Element set: 902
Inclination: 51
6300 deg
RA of node: 271
9063 deg
Eccentricity:
0012715
Arg of perigee: 108
6048 deg
Mean anomaly: 251
6499 deg
Mean motion: 15
76964434 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1262
Checksum: 295
Coasting Arc #4 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2006/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 782013
96 A = 6722559
37 meter
Y = -6499105
21 meter E =
0024262
Z = 1505235
64 I = 51
33156
XDOT = 4745
178533 Wp = 86
20107
YDOT = 1923
143371 meter/sec RA = 266
25749 deg
ZDOT = 5760
134350 TA = 290
47868
MA = 290
73897
Ha = 189
979 n
mi
Hp = 174
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2565662
61 X = 847317
44
Y = -21322523
66 feet Y = -6489995
08 meter
Z = 4938437
13 Z = 1509193
75
XDOT = 15568
171040 XDOT = 4695
338807
YDOT = 6309
525495 feet/sec YDOT = 1975
928270 meter/sec
ZDOT = 18898
078576 ZDOT = 5783
065660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7452033
06 X = 2271379
68
Y = 20138590
22 feet Y = 6138242
30 meter
Z = 4952291
19 Z = 1509458
35
XDOT = -15171
668558 XDOT = -4624
324576
YDOT = 882
936404 feet/sec YDOT = 269
119016 meter/sec
ZDOT = 18983
803305 ZDOT = 5786
263247
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 06292
56043649
00020000 00000-0 20000-3 0 9038
2 25544 51
6301 266
6757 0012789 113
2976 246
9536 15
77039743 12782
Satellite: ISS
Catalog Number: 25544
Epoch time: 06292
56043649 = yrday
fracday
Element set: 903
Inclination: 51
6301 deg
RA of node: 266
6757 deg
Eccentricity:
0012789
Arg of perigee: 113
2976 deg
Mean anomaly: 246
9536 deg
Mean motion: 15
77039743 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1278
Checksum: 322
Coasting Arc #5 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2006/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4162033
20 A = 6714249
35 meter
Y = -2539783
95 meter E =
0023524
Z = -4638923
31 I = 51
30653
XDOT = 1170
340576 Wp = 112
82967
YDOT = -7056
305196 meter/sec RA = 261
03860 deg
ZDOT = 2815
618286 TA = 185
14684
MA = 185
17106
Ha = 189
993 n
mi
Hp = 174
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13654964
56 X = -4110788
08
Y = -8332624
51 feet Y = -2586039
85 meter
Z = -15219564
68 Z = -4659018
31
XDOT = 3839
700053 XDOT = 1235
480100
YDOT = -23150
607597 feet/sec YDOT = -7042
853426 meter/sec
ZDOT = 9237
592803 ZDOT = 2821
462556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15895477
09 X = 4844941
42
Y = 963622
10 feet Y = 293712
01 meter
Z = -15294805
59 Z = -4661856
74
XDOT = 7625
034957 XDOT = 2324
110655
YDOT = 21049
769989 feet/sec YDOT = 6415
969893 meter/sec
ZDOT = 9258
396913 ZDOT = 2821
959379
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 06293
51096491
00020000 00000-0 20000-3 0 9048
2 25544 51
6304 261
7707 0012665 115
6565 244
5909 15
76987207 12930
Satellite: ISS
Catalog Number: 25544
Epoch time: 06293
51096491 = yrday
fracday
Element set: 904
Inclination: 51
6304 deg
RA of node: 261
7707 deg
Eccentricity:
0012665
Arg of perigee: 115
6565 deg
Mean anomaly: 244
5909 deg
Mean motion: 15
76987207 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1293
Checksum: 310
Coasting Arc #6 (Orbit 1308)
---------------------------------------
Vector Time (GMT): 2006/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1320794
10 A = 6718664
19 meter
Y = 5687191
59 meter E =
0017047
Z = -3331336
07 I = 51
32853
XDOT = -4797
795434 Wp = 111
92392
YDOT = -3823
590306 meter/sec RA = 255
90336 deg
ZDOT = -4650
620840 TA = 107
47800
MA = 107
29159
Ha = 189
845 n
mi
Hp = 174
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4333313
97 X = -1368107
43
Y = 18658765
06 feet Y = 5672157
04 meter
Z = -10929580
27 Z = -3337867
84
XDOT = -15740
798668 XDOT = -4732
090442
YDOT = -12544
587617 feet/sec YDOT = -3876
874754 meter/sec
ZDOT = -15257
942388 ZDOT = -4673
769382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5330160
38 X = -1624632
89
Y = -18384804
80 feet Y = -5603688
50 meter
Z = -10953136
12 Z = -3338515
89
XDOT = 18438
256098 XDOT = 5619
980459
YDOT = 3747
005814 feet/sec YDOT = 1142
087372 meter/sec
ZDOT = -15344
742053 ZDOT = -4677
077378
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 06294
52484486
00020000 00000-0 20000-3 0 9056
2 25544 51
6312 256
5388 0012647 119
3213 240
9217 15
77043421 13099
Satellite: ISS
Catalog Number: 25544
Epoch time: 06294
52484486 = yrday
fracday
Element set: 905
Inclination: 51
6312 deg
RA of node: 256
5388 deg
Eccentricity:
0012647
Arg of perigee: 119
3213 deg
Mean anomaly: 240
9217 deg
Mean motion: 15
77043421 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1309
Checksum: 287
Coasting Arc #7 (Orbit 1324)
---------------------------------------
Vector Time (GMT): 2006/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4224382
18 A = 6718563
93 meter
Y = 4007657
71 meter E =
0024163
Z = 3324311
47 I = 51
33687
XDOT = -1886
506031 Wp = 106
82146
YDOT = 5863
463729 meter/sec RA = 250
67099 deg
ZDOT = -4650
611520 TA = 33
76207
MA = 33
60842
Ha = 189
670 n
mi
Hp = 174
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13859521
59 X = 4163104
63
Y = 13148483
29 feet Y = 4054554
57 meter
Z = 10906533
70 Z = 3344685
18
XDOT = -6189
324249 XDOT = -1929
339371
YDOT = 19237
085725 feet/sec YDOT = 5842
128142 meter/sec
ZDOT = -15257
911811 ZDOT = -4659
880662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18528624
58 X = -5647524
77
Y = -4470436
24 feet Y = -1362588
97 meter
Z = 10983018
71 Z = 3347624
10
XDOT = -4675
441354 XDOT = -1425
074525
YDOT = -18357
368767 feet/sec YDOT = -5595
326000 meter/sec
ZDOT = -15291
647132 ZDOT = -4660
894046
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 06295
53870945
00020000 00000-0 20000-3 0 9068
2 25544 51
6314 251
3079 0012546 123
1643 237
0727 15
77067091 13259
Satellite: ISS
Catalog Number: 25544
Epoch time: 06295
53870945 = yrday
fracday
Element set: 906
Inclination: 51
6314 deg
RA of node: 251
3079 deg
Eccentricity:
0012546
Arg of perigee: 123
1643 deg
Mean anomaly: 237
0727 deg
Mean motion: 15
77067091 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1325
Checksum: 289
Coasting Arc #8 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2006/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2034994
10 A = 6713967
91 meter
Y = -4429727
94 meter E =
0020580
Z = 4607125
82 I = 51
33339
XDOT = 4890
959554 Wp = 123
35917
YDOT = 5236
270553 meter/sec RA = 245
53858 deg
ZDOT = 2853
945597 TA = 298
24800
MA = 298
45560
Ha = 189
551 n
mi
Hp = 174
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6676489
83 X = 2061995
39
Y = -14533228
13 feet Y = -4406820
49 meter
Z = 15115242
19 Z = 4617077
76
XDOT = 16046
455229 XDOT = 4818
178945
YDOT = 17179
365330 feet/sec YDOT = 5290
557062 meter/sec
ZDOT = 9363
338573 ZDOT = 2877
529801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1844417
75 X = 562178
53
Y = 15851945
39 feet Y = 4831672
95 meter
Z = 15151723
78 Z = 4618245
41
XDOT = -21406
274158 XDOT = -6524
632364
YDOT = -6607
384167 feet/sec YDOT = -2013
930694 meter/sec
ZDOT = 9451
960506 ZDOT = 2880
957562
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 06296
55255684
00020000 00000-0 20000-3 0 9079
2 25544 51
6323 246
0775 0012488 128
0163 232
2131 15
77126183 13411
Satellite: ISS
Catalog Number: 25544
Epoch time: 06296
55255684 = yrday
fracday
Element set: 907
Inclination: 51
6323 deg
RA of node: 246
0775 deg
Eccentricity:
0012488
Arg of perigee: 128
0163 deg
Mean anomaly: 232
2131 deg
Mean motion: 15
77126183 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1341
Checksum: 282
Coasting Arc #9 (Orbit 1355)
---------------------------------------
Vector Time (GMT): 2006/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4248714
26 A = 6722288
91 meter
Y = -4984574
83 meter E =
0014499
Z = -1531025
69 I = 51
37412
XDOT = 2888
967356 Wp = 96
71541
YDOT = -4215
969177 meter/sec RA = 240
32153 deg
ZDOT = 5753
790825 TA = 246
34520
MA = 246
49745
Ha = 189
568 n
mi
Hp = 175
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13939351
23 X = -4185222
59
Y = -16353591
95 feet Y = -5031731
28 meter
Z = -5023050
17 Z = -1551512
45
XDOT = 9478
239358 XDOT = 2907
944432
YDOT = -13831
919872 feet/sec YDOT = -4183
557122 meter/sec
ZDOT = 18877
266487 ZDOT = 5767
871907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20466237
16 X = 6238109
09
Y = 6488349
22 feet Y = 1977648
84 meter
Z = -5100095
72 Z = -1554509
18
XDOT = -139
668878 XDOT = -42
571074
YDOT = 15205
515905 feet/sec YDOT = 4634
641248 meter/sec
ZDOT = 18929
172467 ZDOT = 5769
611768
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 06297
50302735
00020000 00000-0 20000-3 0 9086
2 25544 51
6320 241
1728 0012487 130
8258 229
3991 15
77104824 13562
Satellite: ISS
Catalog Number: 25544
Epoch time: 06297
50302735 = yrday
fracday
Element set: 908
Inclination: 51
6320 deg
RA of node: 241
1728 deg
Eccentricity:
0012487
Arg of perigee: 130
8258 deg
Mean anomaly: 229
3991 deg
Mean motion: 15
77104824 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1356
Checksum: 290
Coasting Arc #10 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2006/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3089541
20 A = 6711316
23 meter
Y = 2885191
12 meter E =
0024864
Z = -5232421
38 I = 51
35312
XDOT = -4731
652183 Wp = 108
03216
YDOT = -6036
286614 meter/sec RA = 235
16128 deg
ZDOT = -544
286234 TA = 156
82387
MA = 156
71154
Ha = 189
439 n
mi
Hp = 175
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10136290
03 X = -3096155
28
Y = 9465850
13 feet Y = 2850605
37 meter
Z = -17166736
80 Z = -5247446
77
XDOT = -15523
793251 XDOT = -4661
157795
YDOT = -19804
089942 feet/sec YDOT = -6088
804398 meter/sec
ZDOT = -1785
715990 ZDOT = -567
102269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3263740
13 X = 994787
99
Y = -13408287
28 feet Y = -4086845
96 meter
Z = -17222351
15 Z = -5249372
63
XDOT = 22820
471312 XDOT = 6955
679656
YDOT = 7918
034367 feet/sec YDOT = 2413
416875 meter/sec
ZDOT = -1871
592969 ZDOT = -570
461537
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 06298
51684575
00020000 00000-0 20000-3 0 9094
2 25544 51
6327 235
9410 0012417 134
8587 225
3589 15
77127758 13728
Satellite: ISS
Catalog Number: 25544
Epoch time: 06298
51684575 = yrday
fracday
Element set: 909
Inclination: 51
6327 deg
RA of node: 235
9410 deg
Eccentricity:
0012417
Arg of perigee: 134
8587 deg
Mean anomaly: 225
3589 deg
Mean motion: 15
77127758 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1372
Checksum: 324
Coasting Arc #11 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2006/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3922698
52 A = 6723099
61 meter
Y = 5414002
40 meter E =
0023439
Z = -597641
49 I = 51
41088
XDOT = -4217
202856 Wp = 139
26341
YDOT = 2410
767844 meter/sec RA = 229
98442 deg
ZDOT = -5990
061446 TA = 47
27729
MA = 47
08021
Ha = 189
370 n
mi
Hp = 175
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12869745
78 X = 3864770
15
Y = 17762475
06 feet Y = 5457544
32 meter
Z = -1960766
06 Z = -578724
95
XDOT = -13835
967376 XDOT = -4214
747569
YDOT = 7909
343320 feet/sec YDOT = 2363
622789 meter/sec
ZDOT = -19652
432564 ZDOT = -6010
543061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20610255
73 X = -6282005
95
Y = -7525132
14 feet Y = -2293660
28 meter
Z = -1889503
98 Z = -575920
81
XDOT = 6410
065356 XDOT = 1953
787921
YDOT = -12729
881200 feet/sec YDOT = -3880
067790 meter/sec
ZDOT = -19728
458852 ZDOT = -6013
234258
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 06299
53064855
00020000 00000-0 20000-3 0 9102
2 25544 51
6331 230
7098 0012444 138
7830 221
4277 15
77146659 13881
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
53064855 = yrday
fracday
Element set: 910
Inclination: 51
6331 deg
RA of node: 230
7098 deg
Eccentricity:
0012444
Arg of perigee: 138
7830 deg
Mean anomaly: 221
4277 deg
Mean motion: 15
77146659 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1388
Checksum: 305
Coasting Arc #12 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2006/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4271114
51 A = 6712120
62 meter
Y = -1365829
90 meter E =
0013745
Z = 4982286
15 I = 51
39326
XDOT = 4160
860871 Wp = 119
03951
YDOT = 6225
950368 meter/sec RA = 224
78726 deg
ZDOT = -1862
908721 TA = 348
94046
MA = 348
97064
Ha = 189
099 n
mi
Hp = 175
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14012842
87 X = 4261866
40
Y = -4481069
24 feet Y = -1318119
94 meter
Z = 16346083
16 Z = 5003013
12
XDOT = 13651
118343 XDOT = 4099
982051
YDOT = 20426
346353 feet/sec YDOT = 6272
139141 meter/sec
ZDOT = -6111
905253 ZDOT = -1842
842329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8838249
61 X = -2693898
48
Y = 11653275
42 feet Y = 3551918
35 meter
Z = 16423175
61 Z = 5005783
93
XDOT = -22073
069240 XDOT = -6727
871504
YDOT = -8246
585896 feet/sec YDOT = -2513
559381 meter/sec
ZDOT = -6036
236147 ZDOT = -1839
844778
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 06300
54443477
00020000 00000-0 20000-3 0 9118
2 25544 51
6327 225
4791 0012344 142
5309 217
6718 15
77192526 14040
Satellite: ISS
Catalog Number: 25544
Epoch time: 06300
54443477 = yrday
fracday
Element set: 911
Inclination: 51
6327 deg
RA of node: 225
4791 deg
Eccentricity:
0012344
Arg of perigee: 142
5309 deg
Mean anomaly: 217
6718 deg
Mean motion: 15
77192526 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1404
Checksum: 280
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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