Date:
August 30th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 1702)
---------------------------------------
Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4623547
47 A = 6722386
89 meter
Y = -238127
63 meter E =
0018721
Z = -4890663
79 I = 51
35374
XDOT = 2692
507802 Wp = 51
49947
YDOT = -6853
212484 meter/sec RA = 305
30972 deg
ZDOT = -2205
991063 TA = 196
91001
MA = 196
97249
Ha = 192
741 n
mi
Hp = 182
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15169119
01 X = -4596783
11
Y = -781258
62 feet Y = -289681
14 meter
Z = -16045484
86 Z = -4913059
96
XDOT = 8833
687015 XDOT = 2779
657789
YDOT = -22484
292927 feet/sec YDOT = -6822
615970 meter/sec
ZDOT = -7237
503488 ZDOT = -2192
699271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13220215
03 X = 4029521
54
Y = 7287229
25 feet Y = 2221147
48 meter
Z = -16133577
58 Z = -4917514
45
XDOT = -17273
123685 XDOT = -5264
848099
YDOT = 15386
072821 feet/sec YDOT = 4689
674996 meter/sec
ZDOT = -7185
549495 ZDOT = -2190
155486
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 09238
51965709
00020000 00000-0 20000-3 0 9003
2 25544 51
6410 305
8016 0008541 18
2704 341
8765 15
73760201 17039
Satellite: ISS
Catalog Number: 25544
Epoch time: 09238
51965709 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 305
8016 deg
Eccentricity:
0008541
Arg of perigee: 18
2704 deg
Mean anomaly: 341
8765 deg
Mean motion: 15
73760201 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1703
Checksum: 274
Coasting Arc #2 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2009/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1778607
04 A = 6731042
03 meter
Y = 6186498
77 meter E =
0016587
Z = 1959433
51 I = 51
36761
XDOT = -5300
784085 Wp = 80
05616
YDOT = 255
794445 meter/sec RA = 300
11999 deg
ZDOT = -5576
334283 TA = 78
05659
MA = 77
87068
Ha = 192
835 n
mi
Hp = 182
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5835324
92 X = -1857171
89
Y = 20296911
97 feet Y = 6166170
01 meter
Z = 6428587
64 Z = 1950602
39
XDOT = -17391
023901 XDOT = -5276
161697
YDOT = 839
220619 feet/sec YDOT = 196
655780 meter/sec
ZDOT = -18295
059982 ZDOT = -5602
025615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13875654
96 X = 4229299
63
Y = -15934976
37 feet Y = -4856980
80 meter
Z = 6394147
27 Z = 1948936
09
XDOT = 14867
418692 XDOT = 4531
589217
YDOT = 5507
594486 feet/sec YDOT = 1678
714799 meter/sec
ZDOT = -18396
091496 ZDOT = -5607
128688
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 09239
53562831
00020000 00000-0 20000-3 0 9016
2 25544 51
6414 300
5855 0008796 22
0986 338
0555 15
73820617 17193
Satellite: ISS
Catalog Number: 25544
Epoch time: 09239
53562831 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 300
5855 deg
Eccentricity:
0008796
Arg of perigee: 22
0986 deg
Mean anomaly: 338
0555 deg
Mean motion: 15
73820617 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1719
Checksum: 301
Coasting Arc #3 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2009/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4600018
28 A = 6722348
01 meter
Y = -691005
20 meter E =
0010389
Z = 4843399
99 I = 51
32419
XDOT = -1338
516289 Wp = 65
33972
YDOT = 7233
238591 meter/sec RA = 295
00139 deg
ZDOT = 2303
634894 TA = 2
15521
MA = 2
15074
Ha = 192
758 n
mi
Hp = 182
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15091923
49 X = 4583875
10
Y = -2267077
43 feet Y = -639655
51 meter
Z = 15890419
93 Z = 4865707
53
XDOT = -4391
457641 XDOT = -1430
490707
YDOT = 23731
097738 feet/sec YDOT = 7217
756184 meter/sec
ZDOT = 7557
857263 ZDOT = 2296
909248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14629559
41 X = -4459089
71
Y = -4010827
76 feet Y = -1222500
30 meter
Z = 15978125
44 Z = 4870132
63
XDOT = 13386
002592 XDOT = 4080
053590
YDOT = -18826
488650 feet/sec YDOT = -5738
313741 meter/sec
ZDOT = 7531
751099 ZDOT = 2295
677735
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 09240
55159205
00020000 00000-0 20000-3 0 9028
2 25544 51
6411 295
3697 0008721 26
1498 334
0104 15
73819355 17357
Satellite: ISS
Catalog Number: 25544
Epoch time: 09240
55159205 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 295
3697 deg
Eccentricity:
0008721
Arg of perigee: 26
1498 deg
Mean anomaly: 334
0104 deg
Mean motion: 15
73819355 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1735
Checksum: 287
Coasting Arc #4 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2009/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 544383
18 A = 6730866
06 meter
Y = -6378283
64 meter E =
0015378
Z = -2061640
11 I = 51
34095
XDOT = 5186
954670 Wp = 34
21214
YDOT = -1335
674961 meter/sec RA = 289
80834 deg
ZDOT = 5534
428193 TA = 302
67316
MA = 302
82140
Ha = 193
012 n
mi
Hp = 181
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1786034
07 X = 625680
78
Y = -20926127
43 feet Y = -6371741
40 meter
Z = -6763911
12 Z = -2058798
25
XDOT = 17017
567814 XDOT = 5174
619892
YDOT = -4382
135700 feet/sec YDOT = -1277
740531 meter/sec
ZDOT = 18157
572813 ZDOT = 5559
596198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9837386
87 X = -2998435
52
Y = 18559779
57 feet Y = 5657020
81 meter
Z = -6753045
42 Z = -2058328
25
XDOT = -15928
499905 XDOT = -4855
006771
YDOT = -1838
866494 feet/sec YDOT = -560
486507 meter/sec
ZDOT = 18256
501185 ZDOT = 5564
581561
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 09241
50405178
00020000 00000-0 20000-3 0 9038
2 25544 51
6408 290
4800 0008871 29
8334 330
3333 15
73811141 17505
Satellite: ISS
Catalog Number: 25544
Epoch time: 09241
50405178 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 290
4800 deg
Eccentricity:
0008871
Arg of perigee: 29
8334 deg
Mean anomaly: 330
3333 deg
Mean motion: 15
73811141 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1750
Checksum: 265
Coasting Arc #5 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2009/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4416705
65 A = 6722510
73 meter
Y = 1602393
32 meter E =
0019823
Z = -4826351
97 I = 51
30436
XDOT = -51
416423 Wp = 56
40002
YDOT = -7308
625735 meter/sec RA = 284
68891 deg
ZDOT = -2375
689092 TA = 190
24696
MA = 190
28743
Ha = 193
113 n
mi
Hp = 181
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14490504
10 X = -4410850
36
Y = 5257195
93 feet Y = 1553035
98 meter
Z = -15834488
09 Z = -4847793
82
XDOT = -168
689053 XDOT = 41
854243
YDOT = -23978
430890 feet/sec YDOT = -7308
679144 meter/sec
ZDOT = -7794
255550 ZDOT = -2375
712492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15319268
32 X = 4669312
98
Y = 507219
06 feet Y = 154600
37 meter
Z = -15918749
27 Z = -4852034
78
XDOT = -8813
485006 XDOT = -2686
350230
YDOT = 21168
672251 feet/sec YDOT = 6452
211302 meter/sec
ZDOT = -7794
715044 ZDOT = -2375
829145
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 09242
52000039
00020000 00000-0 20000-3 0 9049
2 25544 51
6412 285
2637 0008892 34
2183 325
9551 15
73815237 17664
Satellite: ISS
Catalog Number: 25544
Epoch time: 09242
52000039 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 285
2637 deg
Eccentricity:
0008892
Arg of perigee: 34
2183 deg
Mean anomaly: 325
9551 deg
Mean motion: 15
73815237 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1766
Checksum: 285
Coasting Arc #6 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2009/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 633354
34 A = 6730660
13 meter
Y = 6362246
65 meter E =
0018880
Z = 2091419
58 I = 51
32525
XDOT = -4857
499936 Wp = 82
87956
YDOT = 2309
447872 meter/sec RA = 279
49339 deg
ZDOT = -5509
639998 TA = 73
65319
MA = 73
44567
Ha = 193
159 n
mi
Hp = 181
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2077934
20 X = 552003
94
Y = 20873512
63 feet Y = 6368874
31 meter
Z = 6861612
79 Z = 2094298
84
XDOT = -15936
679580 XDOT = -4856
199089
YDOT = 7576
928713 feet/sec YDOT = 2255
135781 meter/sec
ZDOT = -18076
246713 ZDOT = -5533
234228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5566841
89 X = 1696773
41
Y = -20220571
60 feet Y = -6163230
22 meter
Z = 6873268
93 Z = 2094972
37
XDOT = 16019
518798 XDOT = 4882
749330
YDOT = -1815
547960 feet/sec YDOT = -553
379018 meter/sec
ZDOT = -18168
939305 ZDOT = -5537
892700
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 09243
53593941
00020000 00000-0 20000-3 0 9051
2 25544 51
6406 280
0476 0009075 37
6731 322
5066 15
73865041 17821
Satellite: ISS
Catalog Number: 25544
Epoch time: 09243
53593941 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 280
0476 deg
Eccentricity:
0009075
Arg of perigee: 37
6731 deg
Mean anomaly: 322
5066 deg
Mean motion: 15
73865041 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1782
Checksum: 294
Coasting Arc #7 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2009/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4033758
84 A = 6722473
07 meter
Y = -2424953
67 meter E =
0012595
Z = 4788294
52 I = 51
29321
XDOT = 1413
128647 Wp = 75
36665
YDOT = 7175
311158 meter/sec RA = 274
37376 deg
ZDOT = 2441
168844 TA = 350
68343
MA = 350
70677
Ha = 193
143 n
mi
Hp = 181
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13234116
94 X = 4037314
96
Y = -7955884
76 feet Y = -2379825
89 meter
Z = 15709627
69 Z = 4807898
89
XDOT = 4636
248842 XDOT = 1320
929471
YDOT = 23541
047107 feet/sec YDOT = 7190
598101 meter/sec
ZDOT = 8009
084134 ZDOT = 2447
809716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15069860
86 X = -4593293
59
Y = 2985352
84 feet Y = 909935
55 meter
Z = 15786618
31 Z = 4811761
26
XDOT = 3949
549785 XDOT = 1203
822774
YDOT = -22593
357930 feet/sec YDOT = -6886
455497 meter/sec
ZDOT = 8035
593178 ZDOT = 2449
248801
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 09244
55187145
00020000 00000-0 20000-3 0 9060
2 25544 51
6398 274
8314 0009138 42
3207 317
8660 15
73860590 17982
Satellite: ISS
Catalog Number: 25544
Epoch time: 09244
55187145 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 274
8314 deg
Eccentricity:
0009138
Arg of perigee: 42
3207 deg
Mean anomaly: 317
8660 deg
Mean motion: 15
73860590 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1798
Checksum: 314
Coasting Arc #8 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2009/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1822058
40 A = 6730389
00 meter
Y = -6102083
97 meter E =
0015336
Z = -2166210
96 I = 51
32011
XDOT = 4340
609602 Wp = 44
46902
YDOT = -3229
063551 meter/sec RA = 269
17692 deg
ZDOT = 5479
246349 TA = 291
16770
MA = 291
33151
Ha = 193
222 n
mi
Hp = 181
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5977881
88 X = -1743165
51
Y = -20019960
54 feet Y = -6122018
25 meter
Z = -7106991
34 Z = -2174870
59
XDOT = 14240
845151 XDOT = 4349
778122
YDOT = -10594
040522 feet/sec YDOT = -3180
472883 meter/sec
ZDOT = 17976
530016 ZDOT = 5500
355100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -904044
73 X = -275552
83
Y = 20862079
83 feet Y = 6358761
93 meter
Z = -7141396
65 Z = -2176697
70
XDOT = -15293
154473 XDOT = -4661
353483
YDOT = 5481
079917 feet/sec YDOT = 1670
633159 meter/sec
ZDOT = 18059
392147 ZDOT = 5504
502726
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 09245
50429977
00020000 00000-0 20000-3 0 9079
2 25544 51
6406 269
9417 0009134 46
0461 314
1454 15
73901714 18133
Satellite: ISS
Catalog Number: 25544
Epoch time: 09245
50429977 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 269
9417 deg
Eccentricity:
0009134
Arg of perigee: 46
0461 deg
Mean anomaly: 314
1454 deg
Mean motion: 15
73901714 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1813
Checksum: 294
Coasting Arc #9 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2009/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3528555
93 A = 6722515
43 meter
Y = 3162033
06 meter E =
0020526
Z = -4788363
21 I = 51
29438
XDOT = -2696
425473 Wp = 62
16387
YDOT = -6757
238577 meter/sec RA = 264
05725 deg
ZDOT = -2473
849323 TA = 183
46489
MA = 183
47913
Ha = 193
342 n
mi
Hp = 181
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11576627
07 X = -3540391
34
Y = 10374124
22 feet Y = 3122508
26 meter
Z = -15709853
04 Z = -4805533
63
XDOT = -8846
540267 XDOT = -2608
647089
YDOT = -22169
417903 feet/sec YDOT = -6786
900918 meter/sec
ZDOT = -8116
303554 ZDOT = -2486
734863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14129769
89 X = 4306753
86
Y = -6314199
16 feet Y = -1924567
90 meter
Z = -15777221
62 Z = -4808897
15
XDOT = 1052
289887 XDOT = 320
737958
YDOT = 22773
511509 feet/sec YDOT = 6941
366308 meter/sec
ZDOT = -8167
382998 ZDOT = -2489
418338
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 09246
52021463
00020000 00000-0 20000-3 0 9081
2 25544 51
6400 264
7249 0009142 49
2288 310
9667 15
73877429 18296
Satellite: ISS
Catalog Number: 25544
Epoch time: 09246
52021463 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 264
7249 deg
Eccentricity:
0009142
Arg of perigee: 49
2288 deg
Mean anomaly: 310
9667 deg
Mean motion: 15
73877429 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1829
Checksum: 309
Coasting Arc #10 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2009/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2882039
12 A = 6730380
07 meter
Y = 5678868
68 meter E =
0020700
Z = 2161798
45 I = 51
32418
XDOT = -3684
181695 Wp = 87
15404
YDOT = 3971
284093 meter/sec RA = 258
85898 deg
ZDOT = -5474
490088 TA = 68
53164
MA = 68
31102
Ha = 193
380 n
mi
Hp = 180
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9455508
92 X = 2807821
29
Y = 18631458
93 feet Y = 5710682
51 meter
Z = 7092514
59 Z = 2175618
63
XDOT = -12087
210285 XDOT = -3701
721584
YDOT = 13029
147286 feet/sec YDOT = 3929
986971 meter/sec
ZDOT = -17960
925484 ZDOT = -5492
430568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3545890
76 X = -1080787
50
Y = -20571475
15 feet Y = -6270185
62 meter
Z = 7147219
25 Z = 2178472
43
XDOT = 13772
028715 XDOT = 4197
714352
YDOT = -8690
710465 feet/sec YDOT = -2648
928550 meter/sec
ZDOT = -18031
271843 ZDOT = -5495
931658
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 09247
53612068
00020000 00000-0 20000-3 0 9091
2 25544 51
6386 259
5078 0009309 52
7438 307
4573 15
73909185 18452
Satellite: ISS
Catalog Number: 25544
Epoch time: 09247
53612068 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 259
5078 deg
Eccentricity:
0009309
Arg of perigee: 52
7438 deg
Mean anomaly: 307
4573 deg
Mean motion: 15
73909185 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1845
Checksum: 325
Coasting Arc #11 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2009/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2878259
02 A = 6722494
26 meter
Y = -3755966
72 meter E =
0014075
Z = 4762315
64 I = 51
30392
XDOT = 3890
716828 Wp = 83
80130
YDOT = 6166
692422 meter/sec RA = 253
73979 deg
ZDOT = 2507
262113 TA = 341
55076
MA = 341
60175
Ha = 193
346 n
mi
Hp = 180
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9443107
02 X = 2896910
57
Y = -12322725
47 feet Y = -3723675
68 meter
Z = 15624395
15 Z = 4776343
78
XDOT = 12764
818991 XDOT = 3809
290855
YDOT = 20231
930520 feet/sec YDOT = 6209
745625 meter/sec
ZDOT = 8225
925566 ZDOT = 2525
964889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12392711
31 X = -3777298
41
Y = 9258616
91 feet Y = 2822026
43 meter
Z = 15679358
30 Z = 4779068
41
XDOT = -5955
890054 XDOT = -1815
355288
YDOT = -22054
506779 feet/sec YDOT = -6722
213666 meter/sec
ZDOT = 8299
876732 ZDOT = 2529
802428
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 09248
55201837
00020000 00000-0 20000-3 0 9104
2 25544 51
6380 254
2907 0009277 56
3077 303
8969 15
73900683 18613
Satellite: ISS
Catalog Number: 25544
Epoch time: 09248
55201837 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 254
2907 deg
Eccentricity:
0009277
Arg of perigee: 56
3077 deg
Mean anomaly: 303
8969 deg
Mean motion: 15
73900683 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1861
Checksum: 309
Coasting Arc #12 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2009/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3877108
20 A = 6730182
37 meter
Y = -5035986
23 meter E =
0015207
Z = -2207803
53 I = 51
34039
XDOT = 2884
565585 Wp = 53
57834
YDOT = -4598
495029 meter/sec RA = 248
54312 deg
ZDOT = 5458
513080 TA = 281
57251
MA = 281
74319
Ha = 193
392 n
mi
Hp = 180
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12720171
26 X = -3809781
65
Y = -16522264
55 feet Y = -5078966
07 meter
Z = -7243449
92 Z = -2226474
62
XDOT = 9463
797850 XDOT = 2909
255840
YDOT = -15086
925947 feet/sec YDOT = -4566
099631 meter/sec
ZDOT = 17908
507480 ZDOT = 5472
586665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7950962
24 X = 2423453
29
Y = 19248275
85 feet Y = 5866874
48 meter
Z = -7317214
33 Z = -2230286
93
XDOT = -11553
117603 XDOT = -3521
390245
YDOT = 11557
998942 feet/sec YDOT = 3522
878077 meter/sec
ZDOT = 17963
595005 ZDOT = 5475
303758
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 09249
50441354
00020000 00000-0 20000-3 0 9111
2 25544 51
6386 249
4009 0009320 60
1442 300
0647 15
73938035 18766
Satellite: ISS
Catalog Number: 25544
Epoch time: 09249
50441354 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 249
4009 deg
Eccentricity:
0009320
Arg of perigee: 60
1442 deg
Mean anomaly: 300
0647 deg
Mean motion: 15
73938035 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1876
Checksum: 279
Coasting Arc #13 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2009/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2166101
05 A = 6722447
20 meter
Y = 4223025
94 meter E =
0020903
Z = -4780610
69 I = 51
32535
XDOT = -4915
097178 Wp = 68
24101
YDOT = -5351
039734 meter/sec RA = 243
42463 deg
ZDOT = -2501
023355 TA = 177
12604
MA = 177
11401
Ha = 193
469 n
mi
Hp = 180
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7106630
73 X = -2189939
17
Y = 13855071
98 feet Y = 4198669
69 meter
Z = -15684418
27 Z = -4791191
88
XDOT = -16125
646910 XDOT = -4842
746029
YDOT = -17555
904640 feet/sec YDOT = -5405
598888 meter/sec
ZDOT = -8205
457200 ZDOT = -2524
724914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10172724
54 X = 3100646
44
Y = -11733860
55 feet Y = -3576480
69 meter
Z = -15725787
37 Z = -4793219
99
XDOT = 10471
778678 XDOT = 3191
798141
YDOT = 20195
987254 feet/sec YDOT = 6155
736915 meter/sec
ZDOT = -8299
037332 ZDOT = -2529
546579
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 09250
52029345
00020000 00000-0 20000-3 0 9128
2 25544 51
6378 244
1829 0009271 63
2407 296
9704 15
73924217 18921
Satellite: ISS
Catalog Number: 25544
Epoch time: 09250
52029345 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 244
1829 deg
Eccentricity:
0009271
Arg of perigee: 63
2407 deg
Mean anomaly: 296
9704 deg
Mean motion: 15
73924217 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1892
Checksum: 301
Coasting Arc #14 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2009/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4698476
43 A = 6730162
27 meter
Y = 4292014
79 meter E =
0021757
Z = 2170236
66 I = 51
36641
XDOT = -2036
959732 Wp = 92
04175
YDOT = 5021
708133 meter/sec RA = 238
22866 deg
ZDOT = -5474
905926 TA = 63
55183
MA = 63
32876
Ha = 193
389 n
mi
Hp = 180
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15414948
90 X = 4639590
45
Y = 14081413
36 feet Y = 4344226
79 meter
Z = 7120199
01 Z = 2192918
80
XDOT = -6682
938753 XDOT = -2066
365583
YDOT = 16475
420385 feet/sec YDOT = 4998
764925 meter/sec
ZDOT = -17962
289785 ZDOT = -5484
873283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11786376
70 X = -3592487
62
Y = -17196090
39 feet Y = -5241368
35 meter
Z = 7209707
72 Z = 2197518
91
XDOT = 8882
978547 XDOT = 2707
531861
YDOT = -13698
837615 feet/sec YDOT = -4175
405705 meter/sec
ZDOT = -18001
194532 ZDOT = -5486
764093
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
53616306
00020000 00000-0 20000-3 0 9130
2 25544 51
6377 238
9658 0009286 65
7147 294
4985 15
73973033 19087
Satellite: ISS
Catalog Number: 25544
Epoch time: 09251
53616306 = yrday
fracday
Element set: 913
Inclination: 51
6377 deg
RA of node: 238
9658 deg
Eccentricity:
0009286
Arg of perigee: 65
7147 deg
Mean anomaly: 294
4985 deg
Mean motion: 15
73973033 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1908
Checksum: 329
Coasting Arc #15 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2009/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1373875
18 A = 6722301
21 meter
Y = -4521265
32 meter E =
0014891
Z = 4768591
09 I = 51
35636
XDOT = 5809
450495 Wp = 91
83870
YDOT = 4410
309849 meter/sec RA = 233
11354 deg
ZDOT = 2500
629677 TA = 333
58989
MA = 333
66572
Ha = 193
357 n
mi
Hp = 180
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4507464
50 X = 1401165
43
Y = -14833547
64 feet Y = -4505749
09 meter
Z = 15644983
88 Z = 4775331
89
XDOT = 19059
876952 XDOT = 5747
554134
YDOT = 14469
520503 feet/sec YDOT = 4474
928548 meter/sec
ZDOT = 8204
165607 ZDOT = 2528
701796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7426989
27 X = -2263746
33
Y = 13578269
18 feet Y = 4138656
45 meter
Z = 15671226
15 Z = 4776589
73
XDOT = -14566
672790 XDOT = -4439
921866
YDOT = -17591
320958 feet/sec YDOT = -5361
834628 meter/sec
ZDOT = 8314
895293 ZDOT = 2534
380085
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
55202415
00020000 00000-0 20000-3 0 9146
2 25544 51
6375 233
7494 0009162 69
6674 290
5482 15
73972105 19243
Satellite: ISS
Catalog Number: 25544
Epoch time: 09252
55202415 = yrday
fracday
Element set: 914
Inclination: 51
6375 deg
RA of node: 233
7494 deg
Eccentricity:
0009162
Arg of perigee: 69
6674 deg
Mean anomaly: 290
5482 deg
Mean motion: 15
73972105 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1924
Checksum: 301
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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