Date:
October 25th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2616)
---------------------------------------
Vector Time (GMT): 2009/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6494121
43 A = 6727405
95 meter
Y = 478184
49 meter E =
0012032
Z = 1658584
54 I = 51
70396
XDOT = -1822
703235 Wp = 146
00803
YDOT = -4807
426525 meter/sec RA = 7
39164 deg
ZDOT = -5740
569213 TA = 15
66120
MA = 15
62401
Ha = 187
403 n
mi
Hp = 184
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21306172
67 X = -6507043
17
Y = 1568846
76 feet Y = 405491
11 meter
Z = 5441550
31 Z = 1627004
09
XDOT = -5979
997491 XDOT = -1740
923086
YDOT = -15772
396737 feet/sec YDOT = -4827
351682 meter/sec
ZDOT = -18833
888493 ZDOT = -5749
225540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17423762
13 X = 5310762
70
Y = -12416378
95 feet Y = -3784512
30 meter
Z = 5317028
41 Z = 1620630
26
XDOT = 12298
754789 XDOT = 3748
660460
YDOT = 9164
272310 feet/sec YDOT = 2793
270200 meter/sec
ZDOT = -18868
183252 ZDOT = -5751
022255
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 09296
53488743
00016717 00000-0 10270-3 0 9005
2 25544 51
6441 7
7314 0007011 238
2855 121
7626 15
75276209 26172
Satellite: ISS
Catalog Number: 25544
Epoch time: 09296
53488743 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 7
7314 deg
Eccentricity:
0007011
Arg of perigee: 238
2855 deg
Mean anomaly: 121
7626 deg
Mean motion: 15
75276209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2617
Checksum: 311
Coasting Arc #2 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2009/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1405477
06 A = 6716877
26 meter
Y = 4114142
97 meter E =
0006393
Z = 5123514
18 I = 51
63951
XDOT = -7527
087250 Wp = 204
50718
YDOT = 814
416004 meter/sec RA = 2
27538 deg
ZDOT = 1405
763470 TA = 232
00098
MA = 232
05872
Ha = 186
995 n
mi
Hp = 184
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4611145
22 X = 1334478
02
Y = 13497844
38 feet Y = 4129462
78 meter
Z = 16809429
73 Z = 5130169
71
XDOT = -24695
168143 XDOT = -7542
463817
YDOT = 2671
968516 feet/sec YDOT = 730
157681 meter/sec
ZDOT = 4612
084876 ZDOT = 1369
158925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11020199
83 X = -3358956
91
Y = -9006778
00 feet Y = -2745265
93 meter
Z = 16835811
14 Z = 5131555
24
XDOT = 18824
004348 XDOT = 5737
556525
YDOT = -14649
551173 feet/sec YDOT = -4465
183197 meter/sec
ZDOT = 4467
759757 ZDOT = 1361
773174
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 09297
54987811
00016717 00000-0 10270-3 0 9018
2 25544 51
6442 2
5088 0007065 242
8083 117
2361 15
75346599 26331
Satellite: ISS
Catalog Number: 25544
Epoch time: 09297
54987811 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 2
5088 deg
Eccentricity:
0007065
Arg of perigee: 242
8083 deg
Mean anomaly: 117
2361 deg
Mean motion: 15
75346599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 323
Coasting Arc #3 (Orbit 2647)
---------------------------------------
Vector Time (GMT): 2009/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6614429
45 A = 6728113
83 meter
Y = -939376
63 meter E =
0005674
Z = -764351
99 I = 51
64662
XDOT = 1352
268971 Wp = 3
96944
YDOT = 4666
112984 meter/sec RA = 357
11099 deg
ZDOT = 5975
660679 TA = 347
69624
MA = 347
71009
Ha = 186
676 n
mi
Hp = 184
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21700884
04 X = 6628155
26
Y = -3081944
33 feet Y = -865333
43 meter
Z = -2507716
50 Z = -732185
27
XDOT = 4436
577988 XDOT = 1270
962061
YDOT = 15308
769633 feet/sec YDOT = 4680
780210 meter/sec
ZDOT = 19605
185955 ZDOT = 5982
032628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16472787
28 X = -5020905
56
Y = 14480815
03 feet Y = 4413752
42 meter
Z = -2380896
11 Z = -725697
14
XDOT = -10950
560593 XDOT = -3337
730869
YDOT = -9233
976813 feet/sec YDOT = -2814
516133 meter/sec
ZDOT = 19630
467810 ZDOT = 5983
366588
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 09298
50139769
00016717 00000-0 10270-3 0 9027
2 25544 51
6435 357
6128 0006807 248
4690 111
5748 15
75346437 26484
Satellite: ISS
Catalog Number: 25544
Epoch time: 09298
50139769 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 357
6128 deg
Eccentricity:
0006807
Arg of perigee: 248
4690 deg
Mean anomaly: 111
5748 deg
Mean motion: 15
75346437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2648
Checksum: 345
Coasting Arc #4 (Orbit 2663)
---------------------------------------
Vector Time (GMT): 2009/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -924055
82 A = 6716046
61 meter
Y = -4082805
50 meter E =
0008744
Z = -5259177
92 I = 51
57680
XDOT = 7577
424527 Wp = 100
18887
YDOT = -1317
451365 meter/sec RA = 351
97246 deg
ZDOT = -310
571637 TA = 166
87045
MA = 166
84767
Ha = 186
382 n
mi
Hp = 184
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3031679
22 X = -852783
99
Y = -13395031
17 feet Y = -4092740
38 meter
Z = -17254520
73 Z = -5263493
89
XDOT = 24860
316689 XDOT = 7593
102044
YDOT = -4322
346999 feet/sec YDOT = -1232
628483 meter/sec
ZDOT = -1018
935818 ZDOT = -273
721878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9957581
65 X = 3035070
89
Y = 9427203
66 feet Y = 2873411
68 meter
Z = -17271676
91 Z = -5264407
12
XDOT = -17441
246518 XDOT = -5316
091939
YDOT = 16833
597155 feet/sec YDOT = 5130
880413 meter/sec
ZDOT = -873
661781 ZDOT = -266
292111
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 09299
51631350
00016717 00000-0 10270-3 0 9033
2 25544 51
6435 352
3898 0006783 251
5565 108
4862 15
75429871 26643
Satellite: ISS
Catalog Number: 25544
Epoch time: 09299
51631350 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 352
3898 deg
Eccentricity:
0006783
Arg of perigee: 251
5565 deg
Mean anomaly: 108
4862 deg
Mean motion: 15
75429871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2664
Checksum: 340
Coasting Arc #5 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2009/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6580883
50 A = 6727806
70 meter
Y = 1343891
42 meter E =
0010257
Z = -241873
27 I = 51
58844
XDOT = -747
246250 Wp = 170
70469
YDOT = -4736
480263 meter/sec RA = 346
82202 deg
ZDOT = -6031
016749 TA = 11
92769
MA = 11
90342
Ha = 185
919 n
mi
Hp = 183
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21590825
13 X = -6594247
02
Y = 4409092
60 feet Y = 1270225
38 meter
Z = -793547
48 Z = -273876
19
XDOT = -2451
595310 XDOT = -664
928519
YDOT = -15539
633409 feet/sec YDOT = -4744
376295 meter/sec
ZDOT = -19786
800359 ZDOT = -6034
446861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15094076
71 X = 4600674
58
Y = -16048568
11 feet Y = -4891603
56 meter
Z = -919703
77 Z = -280325
71
XDOT = 9698
551547 XDOT = 2956
118512
YDOT = 10249
089753 feet/sec YDOT = 3123
922557 meter/sec
ZDOT = -19800
486818 ZDOT = -6035
188382
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 09300
53118935
00016717 00000-0 10270-3 0 9048
2 25544 51
6441 347
1669 0006556 256
2447 103
7988 15
75525361 26803
Satellite: ISS
Catalog Number: 25544
Epoch time: 09300
53118935 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 347
1669 deg
Eccentricity:
0006556
Arg of perigee: 256
2447 deg
Mean anomaly: 103
7988 deg
Mean motion: 15
75525361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 325
Coasting Arc #6 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2009/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 370541
82 A = 6715855
66 meter
Y = 4234181
33 meter E =
0003574
Z = 5202821
30 I = 51
51907
XDOT = -7451
873693 Wp = 280
45219
YDOT = 1733
518714 meter/sec RA = 341
65888 deg
ZDOT = -879
933580 TA = 177
94129
MA = 177
93982
Ha = 185
595 n
mi
Hp = 183
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1215688
40 X = 297892
11
Y = 13891671
03 feet Y = 4237918
94 meter
Z = 17069623
68 Z = 5204444
79
XDOT = -24448
404506 XDOT = -7466
429721
YDOT = 5687
397355 feet/sec YDOT = 1650
106047 meter/sec
ZDOT = -2886
921194 ZDOT = -916
170854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9104653
90 X = -2775098
51
Y = -10551689
14 feet Y = -3216154
85 meter
Z = 17076170
77 Z = 5204816
85
XDOT = 15587
594480 XDOT = 4751
098797
YDOT = -18353
786705 feet/sec YDOT = -5594
234188 meter/sec
ZDOT = -3029
756884 ZDOT = -923
469898
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 09301
54602550
00016717 00000-0 10270-3 0 9052
2 25544 51
6435 341
9439 0006539 260
1489 99
8937 15
75587601 26965
Satellite: ISS
Catalog Number: 25544
Epoch time: 09301
54602550 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 341
9439 deg
Eccentricity:
0006539
Arg of perigee: 260
1489 deg
Mean anomaly: 99
8937 deg
Mean motion: 15
75587601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 341
Coasting Arc #7 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2009/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6385743
13 A = 6726853
84 meter
Y = -1641524
90 meter E =
0008795
Z = 1306633
54 I = 51
52812
XDOT = 92
149644 Wp = 41
30391
YDOT = 5021
122000 meter/sec RA = 336
52319 deg
ZDOT = 5841
917383 TA = 333
07276
MA = 333
11837
Ha = 185
427 n
mi
Hp = 183
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20950600
84 X = 6397276
82
Y = -5385580
38 feet Y = -1570051
20 meter
Z = 4286855
44 Z = 1337684
24
XDOT = 302
328227 XDOT = 7
616142
YDOT = 16473
497376 feet/sec YDOT = 5021
680101 meter/sec
ZDOT = 19166
395615 ZDOT = 5842
159478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13416685
52 X = -4089405
75
Y = 16936955
58 feet Y = 5162384
06 meter
Z = 4409236
48 Z = 1343935
28
XDOT = -8872
677411 XDOT = -2704
392075
YDOT = -12031
553563 feet/sec YDOT = -3667
217526 meter/sec
ZDOT = 19167
524146 ZDOT = 5842
261360
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 09302
56082508
00016717 00000-0 10270-3 0 9061
2 25544 51
6433 336
7200 0006274 266
0141 94
0306 15
75596458 27123
Satellite: ISS
Catalog Number: 25544
Epoch time: 09302
56082508 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 336
7200 deg
Eccentricity:
0006274
Arg of perigee: 266
0141 deg
Mean anomaly: 94
0306 deg
Mean motion: 15
75596458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 298
Coasting Arc #8 (Orbit 2726)
---------------------------------------
Vector Time (GMT): 2009/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 199788
01 A = 6716875
34 meter
Y = -4574639
17 meter E =
0006767
Z = -4920280
39 I = 51
46888
XDOT = 7132
141846 Wp = 121
51207
YDOT = -1972
808799 meter/sec RA = 331
33500 deg
ZDOT = 2122
480391 TA = 169
13213
MA = 169
11750
Ha = 185
212 n
mi
Hp = 183
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 655472
46 X = 274830
03
Y = -15008658
71 feet Y = -4571985
69 meter
Z = -16142652
20 Z = -4919127
28
XDOT = 23399
415505 XDOT = 7143
361159
YDOT = -6472
469812 feet/sec YDOT = -1892
990145 meter/sec
ZDOT = 6963
518342 ZDOT = 2157
156586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8685642
49 X = 2647383
83
Y = 12263389
55 feet Y = 3737881
14 meter
Z = -16138264
83 Z = -4918943
12
XDOT = -13470
408295 XDOT = -4105
780448
YDOT = 18889
949004 feet/sec YDOT = 5757
656456 meter/sec
ZDOT = 7100
177469 ZDOT = 2164
134092
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 09303
51216000
00016717 00000-0 10270-3 0 9074
2 25544 51
6442 331
8228 0006392 269
0132 91
0300 15
75675393 27276
Satellite: ISS
Catalog Number: 25544
Epoch time: 09303
51216000 = yrday
fracday
Element set: 907
Inclination: 51
6442 deg
RA of node: 331
8228 deg
Eccentricity:
0006392
Arg of perigee: 269
0132 deg
Mean anomaly: 91
0300 deg
Mean motion: 15
75675393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2727
Checksum: 284
Coasting Arc #9 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2009/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6033926
69 A = 6724617
35 meter
Y = 1741047
80 meter E =
0004084
Z = -2396710
17 I = 51
46952
XDOT = 543
052210 Wp = 212
92368
YDOT = -5501
631278 meter/sec RA = 326
21294 deg
ZDOT = -5362
851773 TA = 354
19204
MA = 354
19678
Ha = 185
138 n
mi
Hp = 183
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19796347
41 X = -6041303
79
Y = 5712099
07 feet Y = 1673531
52 meter
Z = -7863222
34 Z = -2426041
87
XDOT = 1781
667355 XDOT = 630
584611
YDOT = -18049
971383 feet/sec YDOT = -5495
069352 meter/sec
ZDOT = -17594
658049 ZDOT = -5360
000693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11708780
88 X = 3568836
41
Y = -16899607
27 feet Y = -5151000
30 meter
Z = -7978811
73 Z = -2431941
82
XDOT = 8703
399779 XDOT = 2652
796253
YDOT = 14333
204060 feet/sec YDOT = 4368
760597 meter/sec
ZDOT = -17583
607802 ZDOT = -5359
483658
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 09304
52688032
00016717 00000-0 10270-3 0 9085
2 25544 51
6435 326
5986 0006282 272
6668 87
3777 15
75751716 27430
Satellite: ISS
Catalog Number: 25544
Epoch time: 09304
52688032 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 326
5986 deg
Eccentricity:
0006282
Arg of perigee: 272
6668 deg
Mean anomaly: 87
3777 deg
Mean motion: 15
75751716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 349
Coasting Arc #10 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2009/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -715884
83 A = 6718663
95 meter
Y = 5058051
13 meter E =
0004881
Z = 4363915
93 I = 51
42453
XDOT = -6655
932317 Wp = 34
19297
YDOT = 1952
259338 meter/sec RA = 321
00440 deg
ZDOT = -3348
883916 TA = 89
62411
MA = 89
56818
Ha = 185
196 n
mi
Hp = 183
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2348703
52 X = -793591
48
Y = 16594655
94 feet Y = 5049611
30 meter
Z = 14317309
49 Z = 4360249
17
XDOT = -21837
048284 XDOT = -6660
999295
YDOT = 6405
050321 feet/sec YDOT = 1877
800372 meter/sec
ZDOT = -10987
151954 ZDOT = -3381
231900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8838452
99 X = -2693960
47
Y = -14254457
00 feet Y = -4344758
49 meter
Z = 14303026
57 Z = 4359562
50
XDOT = 11476
332531 XDOT = 3497
986156
YDOT = -18287
450985 feet/sec YDOT = -5574
015060 meter/sec
ZDOT = -11114
623449 ZDOT = -3387
737227
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 09305
54156022
00016717 00000-0 10270-3 0 9098
2 25544 51
6423 321
3739 0006219 277
5675 82
4782 15
75838852 27594
Satellite: ISS
Catalog Number: 25544
Epoch time: 09305
54156022 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 321
3739 deg
Eccentricity:
0006219
Arg of perigee: 277
5675 deg
Mean anomaly: 82
4782 deg
Mean motion: 15
75838852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 336
Coasting Arc #11 (Orbit 2774)
---------------------------------------
Vector Time (GMT): 2009/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5559637
55 A = 6721657
21 meter
Y = -1586947
57 meter E =
0006433
Z = 3421772
09 I = 51
41208
XDOT = -1069
812359 Wp = 81
20378
YDOT = 6112
298518 meter/sec RA = 315
88888 deg
ZDOT = 4566
649169 TA = 319
45773
MA = 319
50563
Ha = 185
199 n
mi
Hp = 183
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18240280
67 X = 5560346
90
Y = -5206520
91 feet Y = -1524772
48 meter
Z = 11226286
40 Z = 3448783
52
XDOT = -3509
883066 XDOT = -1160
266401
YDOT = 20053
472827 feet/sec YDOT = 6099
829468 meter/sec
ZDOT = 14982
444779 ZDOT = 4561
232139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10266184
63 X = -3129133
08
Y = 15875134
64 feet Y = 4838741
04 meter
Z = 11332729
53 Z = 3454215
96
XDOT = -9321
986785 XDOT = -2841
341572
YDOT = -16723
411070 feet/sec YDOT = -5097
295694 meter/sec
ZDOT = 14961
294411 ZDOT = 4560
202537
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 09306
55620130
00016717 00000-0 10270-3 0 9108
2 25544 51
6418 316
1487 0006165 281
8581 78
1892 15
75870771 27752
Satellite: ISS
Catalog Number: 25544
Epoch time: 09306
55620130 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 316
1487 deg
Eccentricity:
0006165
Arg of perigee: 281
8581 deg
Mean anomaly: 78
1892 deg
Mean motion: 15
75870771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2775
Checksum: 324
Coasting Arc #12 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2009/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1107506
65 A = 6721283
95 meter
Y = -5611719
65 meter E =
0001348
Z = -3527843
30 I = 51
39093
XDOT = 6072
124865 Wp = 327
39267
YDOT = -1604
134503 meter/sec RA = 310
67007 deg
ZDOT = 4458
257893 TA = 350
40247
MA = 350
40504
Ha = 185
439 n
mi
Hp = 183
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3633552
00 X = 1187313
81
Y = -18411153
72 feet Y = -5598888
52 meter
Z = -11574289
03 Z = -3522269
17
XDOT = 19921
669506 XDOT = 6067
953080
YDOT = -5262
908476 feet/sec YDOT = -1536
255903 meter/sec
ZDOT = 14626
830359 ZDOT = 4487
747158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9600313
75 X = 2926175
63
Y = 16140358
97 feet Y = 4919581
41 meter
Z = -11552499
13 Z = -3521201
74
XDOT = -10009
441510 XDOT = -3050
877772
YDOT = 16505
225389 feet/sec YDOT = 5030
792699 meter/sec
ZDOT = 14743
044335 ZDOT = 4493
679913
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 09307
50738909
00016717 00000-0 10270-3 0 9119
2 25544 51
6422 311
2504 0006168 285
9052 74
1432 15
75929228 27909
Satellite: ISS
Catalog Number: 25544
Epoch time: 09307
50738909 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 311
2504 deg
Eccentricity:
0006168
Arg of perigee: 285
9052 deg
Mean anomaly: 74
1432 deg
Mean motion: 15
75929228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 312
Coasting Arc #13 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2009/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5035149
21 A = 6718307
02 meter
Y = 1120669
11 meter E =
0005829
Z = -4309644
78 I = 51
36193
XDOT = 1441
885353 Wp = 26
15081
YDOT = -6738
162302 meter/sec RA = 305
55050 deg
ZDOT = -3433
396693 TA = 209
01664
MA = 209
04905
Ha = 185
526 n
mi
Hp = 182
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16519518
40 X = -5026370
32
Y = 3676735
92 feet Y = 1064412
45 meter
Z = -14139254
54 Z = -4334084
96
XDOT = 4730
594989 XDOT = 1533
804867
YDOT = -22106
831701 feet/sec YDOT = -6721
524135 meter/sec
ZDOT = -11264
424845 ZDOT = -3426
168904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9490350
26 X = 2892658
76
Y = -13914483
99 feet Y = -4241134
72 meter
Z = -14235581
53 Z = -4339005
25
XDOT = 10587
104219 XDOT = 3226
949366
YDOT = 18727
680295 feet/sec YDOT = 5708
196954 meter/sec
ZDOT = -11236
149151 ZDOT = -3424
778261
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 09308
52195048
00016717 00000-0 10270-3 0 9124
2 25544 51
6411 306
0242 0006149 289
5187 70
5312 15
75994055 28061
Satellite: ISS
Catalog Number: 25544
Epoch time: 09308
52195048 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 306
0242 deg
Eccentricity:
0006149
Arg of perigee: 289
5187 deg
Mean anomaly: 70
5312 deg
Mean motion: 15
75994055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 309
Coasting Arc #14 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2009/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1365237
98 A = 6723746
76 meter
Y = 6128096
79 meter E =
0007831
Z = 2397794
43 I = 51
36445
XDOT = -5470
690507 Wp = 99
08446
YDOT = 880
318686 meter/sec RA = 300
33371 deg
ZDOT = -5351
083470 TA = 53
73806
MA = 53
66573
Ha = 185
641 n
mi
Hp = 182
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4479127
25 X = -1445310
34
Y = 20105304
42 feet Y = 6112382
00 meter
Z = 7866779
61 Z = 2390967
88
XDOT = -17948
459669 XDOT = -5454
132449
YDOT = 2888
184664 feet/sec YDOT = 819
235192 meter/sec
ZDOT = -17556
048130 ZDOT = -5377
620556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10736509
00 X = -3272487
94
Y = -17590703
05 feet Y = -5361646
29 meter
Z = 7840064
33 Z = 2389651
61
XDOT = 9527
615372 XDOT = 2904
017165
YDOT = -13706
428732 feet/sec YDOT = -4177
719477 meter/sec
ZDOT = -17660
656684 ZDOT = -5382
968157
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 09309
53646975
00016717 00000-0 10270-3 0 9137
2 25544 51
6409 300
7982 0006236 294
6299 65
4215 15
76090165 28221
Satellite: ISS
Catalog Number: 25544
Epoch time: 09309
53646975 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 300
7982 deg
Eccentricity:
0006236
Arg of perigee: 294
6299 deg
Mean anomaly: 65
4215 deg
Mean motion: 15
76090165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 332
Coasting Arc #15 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2009/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4531711
80 A = 6715357
11 meter
Y = -332767
92 meter E =
0000776
Z = 4945267
08 I = 51
32202
XDOT = -1647
012508 Wp = 236
58264
YDOT = 7255
735569 meter/sec RA = 295
19855 deg
ZDOT = 1997
321691 TA = 194
01956
MA = 194
02171
Ha = 185
610 n
mi
Hp = 182
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14867820
87 X = 4511072
30
Y = -1091758
26 feet Y = -282207
45 meter
Z = 16224629
53 Z = 4967232
48
XDOT = -5403
584344 XDOT = -1737
727844
YDOT = 23804
906723 feet/sec YDOT = 7236
810327 meter/sec
ZDOT = 6552
892688 ZDOT = 1989
100557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9660997
43 X = -2944672
02
Y = 11229041
01 feet Y = 3422611
70 meter
Z = 16311235
51 Z = 4971664
58
XDOT = -12190
244479 XDOT = -3715
586517
YDOT = -19960
862169 feet/sec YDOT = -6084
070789 meter/sec
ZDOT = 6520
716831 ZDOT = 1987
514490
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 09310
55094863
00016717 00000-0 10270-3 0 9145
2 25544 51
6405 295
5721 0006230 297
8540 62
1992 15
76123073 28385
Satellite: ISS
Catalog Number: 25544
Epoch time: 09310
55094863 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 295
5721 deg
Eccentricity:
0006230
Arg of perigee: 297
8540 deg
Mean anomaly: 62
1992 deg
Mean motion: 15
76123073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 314
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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