Date:
August 9th 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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 1372)
---------------------------------------
Vector Time (GMT): 2009/217/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4894622
13 A = 6724594
20 meter
Y = -514130
95 meter E =
0007079
Z = 4585371
47 I = 51
89472
XDOT = -2128
616010 Wp = 4
87195
YDOT = -6751
050173 meter/sec RA = 52
93971 deg
ZDOT = -3021
891584 TA = 115
09601
MA = 115
02253
Ha = 190
051 n
mi
Hp = 187
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16058471
54 X = -4910783
66
Y = -1686781
34 feet Y = -568956
22 meter
Z = 15043869
64 Z = 4561554
62
XDOT = -6983
648328 XDOT = -2038
286932
YDOT = -22149
114740 feet/sec YDOT = -6774
348307 meter/sec
ZDOT = -9914
342468 ZDOT = -3032
013307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11471414
15 X = 3496487
03
Y = 11486388
08 feet Y = 3501051
09 meter
Z = 14950160
52 Z = 4556808
93
XDOT = -7746
915401 XDOT = -2361
259814
YDOT = 20724
190860 feet/sec YDOT = 6316
733374 meter/sec
ZDOT = -9954
452864 ZDOT = -3034
117233
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 09217
56314942
00010596 00000-0 82463-4 0 9003
2 25544 51
6382 53
3504 0008003 296
2578 63
7762 15
73494970 13731
Satellite: ISS
Catalog Number: 25544
Epoch time: 09217
56314942 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 53
3504 deg
Eccentricity:
0008003
Arg of perigee: 296
2578 deg
Mean anomaly: 63
7762 deg
Mean motion: 15
73494970 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1373
Checksum: 314
Coasting Arc #2 (Orbit 1388)
---------------------------------------
Vector Time (GMT): 2009/218/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2510971
86 A = 6730763
88 meter
Y = 5710538
23 meter E =
0009772
Z = 2510351
27 I = 51
89610
XDOT = -5555
287256 Wp = 41
72084
YDOT = 95
353686 meter/sec RA = 47
86878 deg
ZDOT = 5335
082585 TA = 346
60107
MA = 346
62700
Ha = 190
129 n
mi
Hp = 186
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8238096
64 X = 2434734
45
Y = 18735361
64 feet Y = 5738190
97 meter
Z = 8236060
58 Z = 2522364
46
XDOT = -18226
008057 XDOT = -5581
856947
YDOT = 312
840178 feet/sec YDOT = 33
082335 meter/sec
ZDOT = 17503
551789 ZDOT = 5308
031047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5111490
32 X = 1557982
25
Y = -19798179
13 feet Y = -6034485
00 meter
Z = 8283566
60 Z = 2524831
10
XDOT = 13174
360349 XDOT = 4015
545034
YDOT = 10686
697412 feet/sec YDOT = 3257
305371 meter/sec
ZDOT = 17397
144521 ZDOT = 5302
649650
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 09218
57930103
00010596 00000-0 82463-4 0 9019
2 25544 51
6374 48
1343 0007904 299
8817 60
1560 15
73523142 13897
Satellite: ISS
Catalog Number: 25544
Epoch time: 09218
57930103 = yrday
fracday
Element set: 901
Inclination: 51
6374 deg
RA of node: 48
1343 deg
Eccentricity:
0007904
Arg of perigee: 299
8817 deg
Mean anomaly: 60
1560 deg
Mean motion: 15
73523142 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1389
Checksum: 306
Coasting Arc #3 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2009/219/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4740570
79 A = 6723940
38 meter
Y = -673482
79 meter E =
0004131
Z = -4723843
31 I = 51
85210
XDOT = 3598
344967 Wp = 79
93821
YDOT = 6234
433778 meter/sec RA = 42
71007 deg
ZDOT = 2724
951263 TA = 216
80318
MA = 216
83155
Ha = 190
400 n
mi
Hp = 186
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15553053
76 X = 4770696
59
Y = -2209589
20 feet Y = -620302
32 meter
Z = -15498173
59 Z = -4700740
91
XDOT = 11805
593724 XDOT = 3515
125958
YDOT = 20454
179061 feet/sec YDOT = 6274
207178 meter/sec
ZDOT = 8940
128815 ZDOT = 2742
229785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13809230
79 X = -4209053
54
Y = -7674148
85 feet Y = -2339080
57 meter
Z = -15407327
31 Z = -4696153
36
XDOT = 2405
498338 XDOT = 733
195893
YDOT = -22396
621857 feet/sec YDOT = -6826
490342 meter/sec
ZDOT = 9008
369378 ZDOT = 2745
750987
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 09219
53193726
00010596 00000-0 82463-4 0 9029
2 25544 51
6375 43
2445 0007758 304
0070 56
0355 15
73525747 14041
Satellite: ISS
Catalog Number: 25544
Epoch time: 09219
53193726 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 43
2445 deg
Eccentricity:
0007758
Arg of perigee: 304
0070 deg
Mean anomaly: 56
0355 deg
Mean motion: 15
73525747 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1404
Checksum: 300
Coasting Arc #4 (Orbit 1419)
---------------------------------------
Vector Time (GMT): 2009/220/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3735218
40 A = 6731158
45 meter
Y = -5122644
76 meter E =
0002130
Z = -2261253
26 I = 51
85462
XDOT = 5228
398380 Wp = 289
70538
YDOT = -1394
922373 meter/sec RA = 37
63436 deg
ZDOT = -5471
539444 TA = 275
58264
MA = 275
60693
Ha = 190
501 n
mi
Hp = 186
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12254653
54 X = -3666673
91
Y = -16806577
28 feet Y = -5164030
86 meter
Z = -7418809
90 Z = -2279232
27
XDOT = 17153
537991 XDOT = 5270
187389
YDOT = -4576
516972 feet/sec YDOT = -1336
221593 meter/sec
ZDOT = -17951
244894 ZDOT = -5446
038805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -42133
54 X = -12842
30
Y = 20774458
05 feet Y = 6332054
81 meter
Z = -7489755
09 Z = -2282877
35
XDOT = -15123
886437 XDOT = -4609
760586
YDOT = -6472
132195 feet/sec YDOT = -1972
705893 meter/sec
ZDOT = -17850
998961 ZDOT = -5440
984483
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 09220
54807365
00010596 00000-0 82463-4 0 9034
2 25544 51
6379 38
0297 0007861 309
2827 50
7638 15
73561459 14207
Satellite: ISS
Catalog Number: 25544
Epoch time: 09220
54807365 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 38
0297 deg
Eccentricity:
0007861
Arg of perigee: 309
2827 deg
Mean anomaly: 50
7638 deg
Mean motion: 15
73561459 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1420
Checksum: 321
Coasting Arc #5 (Orbit 1435)
---------------------------------------
Vector Time (GMT): 2009/221/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4342077
37 A = 6723514
21 meter
Y = 1742693
82 meter E =
0008772
Z = 4831587
07 I = 51
80349
XDOT = -4903
339646 Wp = 2
27080
YDOT = -5404
482590 meter/sec RA = 32
47558 deg
ZDOT = -2448
491599 TA = 111
65238
MA = 111
55893
Ha = 190
712 n
mi
Hp = 186
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14245660
65 X = -4384712
47
Y = 5717499
42 feet Y = 1693899
73 meter
Z = 15851663
60 Z = 4810389
95
XDOT = -16087
072330 XDOT = -4830
647174
YDOT = -17731
242093 feet/sec YDOT = -5458
908144 meter/sec
ZDOT = -8033
108922 ZDOT = -2472
135235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15016159
40 X = 4576925
38
Y = 3574570
89 feet Y = 1089529
21 meter
Z = 15768363
44 Z = 4806197
18
XDOT = 3175
068669 XDOT = 967
760930
YDOT = 22636
638397 feet/sec YDOT = 6899
647383 meter/sec
ZDOT = -8126
343596 ZDOT = -2476
909528
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 09221
56420394
00010596 00000-0 82463-4 0 9041
2 25544 51
6376 32
8139 0007730 311
9932 48
0572 15
73517359 14367
Satellite: ISS
Catalog Number: 25544
Epoch time: 09221
56420394 = yrday
fracday
Element set: 904
Inclination: 51
6376 deg
RA of node: 32
8139 deg
Eccentricity:
0007730
Arg of perigee: 311
9932 deg
Mean anomaly: 48
0572 deg
Mean motion: 15
73517359 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1436
Checksum: 308
Coasting Arc #6 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2009/222/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4788318
49 A = 6731593
33 meter
Y = 4267169
91 meter E =
0013089
Z = 2015521
66 I = 51
80651
XDOT = -4637
290215 Wp = 35
91542
YDOT = 2556
358574 meter/sec RA = 27
39251 deg
ZDOT = 5596
867428 TA = 346
50826
MA = 346
54322
Ha = 190
699 n
mi
Hp = 186
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15709706
33 X = 4730455
41
Y = 13999901
28 feet Y = 4320392
15 meter
Z = 6612603
88 Z = 2038642
64
XDOT = -15214
206741 XDOT = -4692
719587
YDOT = 8387
003194 feet/sec YDOT = 2504
191704 meter/sec
ZDOT = 18362
425945 ZDOT = 5574
205010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5111158
83 X = -1557881
21
Y = -20382706
67 feet Y = -6212648
99 meter
Z = 6703727
54 Z = 2043296
15
XDOT = 15901
184228 XDOT = 4846
680953
YDOT = 2030
960368 feet/sec YDOT = 619
036720 meter/sec
ZDOT = 18273
399808 ZDOT = 5569
732262
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 09222
58032438
00010596 00000-0 82463-4 0 9053
2 25544 51
6385 27
5985 0007718 315
7296 44
3248 15
73568395 14521
Satellite: ISS
Catalog Number: 25544
Epoch time: 09222
58032438 = yrday
fracday
Element set: 905
Inclination: 51
6385 deg
RA of node: 27
5985 deg
Eccentricity:
0007718
Arg of perigee: 315
7296 deg
Mean anomaly: 44
3248 deg
Mean motion: 15
73568395 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1452
Checksum: 334
Coasting Arc #7 (Orbit 1466)
---------------------------------------
Vector Time (GMT): 2009/223/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3704011
83 A = 6722925
00 meter
Y = -2685464
21 meter E =
0007470
Z = -4931320
27 I = 51
75103
XDOT = 6000
939553 Wp = 70
88681
YDOT = 4301
344775 meter/sec RA = 22
23507 deg
ZDOT = 2170
084038 TA = 220
12891
MA = 220
18410
Ha = 190
961 n
mi
Hp = 185
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12152269
78 X = 3757721
25
Y = -8810578
12 feet Y = -2643743
39 meter
Z = -16178872
28 Z = -4913195
82
XDOT = 19688
121893 XDOT = 5941
853328
YDOT = 14112
023541 feet/sec YDOT = 4368
120397 meter/sec
ZDOT = 7119
698287 ZDOT = 2199
093074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15071262
02 X = -4593720
66
Y = 677407
25 feet Y = 206473
73 meter
Z = -16107701
15 Z = -4909627
31
XDOT = -8678
252376 XDOT = -2645
131324
YDOT = -21461
110107 feet/sec YDOT = -6541
346361 meter/sec
ZDOT = 7233
975173 ZDOT = 2204
915633
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 09223
53293140
00010596 00000-0 82463-4 0 9069
2 25544 51
6395 22
7102 0007683 319
9570 40
1026 15
73570563 14676
Satellite: ISS
Catalog Number: 25544
Epoch time: 09223
53293140 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 22
7102 deg
Eccentricity:
0007683
Arg of perigee: 319
9570 deg
Mean anomaly: 40
1026 deg
Mean motion: 15
73570563 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1467
Checksum: 295
Coasting Arc #8 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2009/224/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5637134
46 A = 6731856
49 meter
Y = -3215731
78 meter E =
0000621
Z = -1790220
15 I = 51
75340
XDOT = 3810
851329 Wp = 357
65771
YDOT = -3514
634307 meter/sec RA = 17
14438 deg
ZDOT = -5685
864054 TA = 202
13362
MA = 202
13630
Ha = 191
071 n
mi
Hp = 185
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18494535
64 X = -5592060
07
Y = -10550301
12 feet Y = -3278517
44 meter
Z = -5873425
69 Z = -1817495
96
XDOT = 12502
793073 XDOT = 3877
490229
YDOT = -11530
952450 feet/sec YDOT = -3471
646340 meter/sec
ZDOT = -18654
409626 ZDOT = -5667
189199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10006938
90 X = 3050114
98
Y = 18760187
31 feet Y = 5718105
09 meter
Z = -5980834
19 Z = -1822958
26
XDOT = -15446
888780 XDOT = -4708
211700
YDOT = 2315
142491 feet/sec YDOT = 705
655431 meter/sec
ZDOT = -18581
107451 ZDOT = -5663
521551
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 09224
54903662
00010596 00000-0 82463-4 0 9079
2 25544 51
6394 17
4946 0007826 324
5099 35
5542 15
73603742 14834
Satellite: ISS
Catalog Number: 25544
Epoch time: 09224
54903662 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 17
4946 deg
Eccentricity:
0007826
Arg of perigee: 324
5099 deg
Mean anomaly: 35
5542 deg
Mean motion: 15
73603742 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1483
Checksum: 323
Coasting Arc #9 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2009/225/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2919849
26 A = 6722645
13 meter
Y = 3418319
64 meter E =
0009873
Z = 5000558
80 I = 51
69330
XDOT = -6823
417159 Wp = 4
24918
YDOT = -3001
246109 meter/sec RA = 11
98560 deg
ZDOT = -1922
707008 TA = 104
36480
MA = 104
25518
Ha = 191
324 n
mi
Hp = 185
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9579557
96 X = -2982148
30
Y = 11214959
46 feet Y = 3385319
57 meter
Z = 16406032
80 Z = 4986223
03
XDOT = -22386
539236 XDOT = -6780
009415
YDOT = -9846
607969 feet/sec YDOT = -3077
306752 meter/sec
ZDOT = -6308
093858 ZDOT = -1955
749897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14084511
19 X = 4292959
01
Y = -4583893
91 feet Y = -1397170
86 meter
Z = 16349789
59 Z = 4983415
87
XDOT = 13685
547811 XDOT = 4171
354973
YDOT = 18970
434459 feet/sec YDOT = 5782
188423 meter/sec
ZDOT = -6438
171308 ZDOT = -1962
354615
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 09225
56513620
00010596 00000-0 82463-4 0 9084
2 25544 51
6399 12
2796 0007688 328
6286 31
4417 15
73556144 14990
Satellite: ISS
Catalog Number: 25544
Epoch time: 09225
56513620 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 12
2796 deg
Eccentricity:
0007688
Arg of perigee: 328
6286 deg
Mean anomaly: 31
4417 deg
Mean motion: 15
73556144 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1499
Checksum: 334
Coasting Arc #10 (Orbit 1514)
---------------------------------------
Vector Time (GMT): 2009/226/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6224140
53 A = 6732118
15 meter
Y = 1997731
08 meter E =
0015892
Z = 1566008
45 I = 51
69783
XDOT = -2821
537986 Wp = 33
56105
YDOT = 4252
875679 meter/sec RA = 6
88802 deg
ZDOT = 5774
227572 TA = 343
70891
MA = 343
75993
Ha = 191
237 n
mi
Hp = 185
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20420408
55 X = 6193731
59
Y = 6554235
82 feet Y = 2067162
92 meter
Z = 5137823
01 Z = 1596171
56
XDOT = -9257
014390 XDOT = -2896
934764
YDOT = 13953
004196 feet/sec YDOT = 4220
901585 meter/sec
ZDOT = 18944
316181 ZDOT = 5760
337749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14324736
93 X = -4366179
82
Y = -15922282
70 feet Y = -4853111
77 meter
Z = 5256533
42 Z = 1602191
39
XDOT = 13953
996577 XDOT = 4253
178157
YDOT = -6302
109853 feet/sec YDOT = -1920
883083 meter/sec
ZDOT = 18889
856694 ZDOT = 5757
628320
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 09226
58122334
00010596 00000-0 82463-4 0 9096
2 25544 51
6410 7
0647 0007742 331
8019 28
2724 15
73630516 15152
Satellite: ISS
Catalog Number: 25544
Epoch time: 09226
58122334 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 7
0647 deg
Eccentricity:
0007742
Arg of perigee: 331
8019 deg
Mean anomaly: 28
2724 deg
Mean motion: 15
73630516 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1515
Checksum: 288
Coasting Arc #11 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2009/227/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1980825
11 A = 6722092
67 meter
Y = -3954925
27 meter E =
0010804
Z = -5069244
79 I = 51
63418
XDOT = 7349
162363 Wp = 67
00618
YDOT = 1546
322988 meter/sec RA = 1
72969 deg
ZDOT = 1672
255567 TA = 219
04816
MA = 219
12620
Ha = 191
471 n
mi
Hp = 184
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6498770
03 X = 2049527
86
Y = -12975476
62 feet Y = -3932389
93 meter
Z = -16631380
53 Z = -5059455
47
XDOT = 24111
425074 XDOT = 7323
201441
YDOT = 5073
238148 feet/sec YDOT = 1628
360327 meter/sec
ZDOT = 5486
402780 ZDOT = 1707
894667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12090259
23 X = -3685111
01
Y = 8105349
41 feet Y = 2470510
50 meter
Z = -16593033
68 Z = -5057556
67
XDOT = -17947
948229 XDOT = -5470
534620
YDOT = -15300
009733 feet/sec YDOT = -4663
442967 meter/sec
ZDOT = 5626
635380 ZDOT = 1714
998464
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 09227
53380046
00010596 00000-0 82463-4 0 9100
2 25544 51
6410 2
1767 0007850 335
9555 24
1241 15
73639733 15307
Satellite: ISS
Catalog Number: 25544
Epoch time: 09227
53380046 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 2
1767 deg
Eccentricity:
0007850
Arg of perigee: 335
9555 deg
Mean anomaly: 24
1241 deg
Mean motion: 15
73639733 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1530
Checksum: 287
Coasting Arc #12 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2009/228/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6554312
51 A = 6732309
74 meter
Y = -701519
79 meter E =
0002542
Z = -1372609
88 I = 51
63919
XDOT = 1723
507579 Wp = 75
96260
YDOT = -4720
584008 meter/sec RA = 356
62298 deg
ZDOT = -5825
640566 TA = 119
10656
MA = 119
08110
Ha = 191
615 n
mi
Hp = 184
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21503649
97 X = -6539313
05
Y = -2301574
11 feet Y = -774729
96 meter
Z = -4503313
26 Z = -1404414
00
XDOT = 5654
552426 XDOT = 1804
465447
YDOT = -15487
480340 feet/sec YDOT = -4700
857539 meter/sec
ZDOT = -19112
993983 ZDOT = -5817
071652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17833277
76 X = 5435583
06
Y = 12187527
93 feet Y = 3714758
51 meter
Z = -4628434
20 Z = -1410746
74
XDOT = -11517
605281 XDOT = -3510
566090
YDOT = 9617
407448 feet/sec YDOT = 2931
385790 meter/sec
ZDOT = -19079
476011 ZDOT = -5815
424288
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 09228
54987366
00010596 00000-0 82463-4 0 9111
2 25544 51
6412 356
9605 0007950 339
9268 20
1581 15
73647249 15467
Satellite: ISS
Catalog Number: 25544
Epoch time: 09228
54987366 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 356
9605 deg
Eccentricity:
0007950
Arg of perigee: 339
9268 deg
Mean anomaly: 20
1581 deg
Mean motion: 15
73647249 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1546
Checksum: 338
Coasting Arc #13 (Orbit 1561)
---------------------------------------
Vector Time (GMT): 2009/229/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1015484
46 A = 6721856
40 meter
Y = 4250363
42 meter E =
0010625
Z = 5108408
10 I = 51
57497
XDOT = -7559
813288 Wp = 8
47294
YDOT = -37
212208 meter/sec RA = 351
46250 deg
ZDOT = -1461
113996 TA = 95
60521
MA = 95
48402
Ha = 191
826 n
mi
Hp = 184
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3331641
93 X = -1087752
58
Y = 13944761
86 feet Y = 4238603
19 meter
Z = 16759869
08 Z = 5103299
76
XDOT = -24802
537034 XDOT = -7551
737608
YDOT = -122
087296 feet/sec YDOT = -121
705206 meter/sec
ZDOT = -4793
681090 ZDOT = -1497
819332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9433076
32 X = 2875201
66
Y = -10827775
34 feet Y = -3300305
92 meter
Z = 16739945
79 Z = 5102335
48
XDOT = 21179
822644 XDOT = 6455
609942
YDOT = 10762
950865 feet/sec YDOT = 3280
547424 meter/sec
ZDOT = -4938
059171 ZDOT = -1505
120435
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 09229
56593912
00010596 00000-0 82463-4 0 9125
2 25544 51
6421 351
7455 0008053 344
2983 15
7930 15
73647470 15623
Satellite: ISS
Catalog Number: 25544
Epoch time: 09229
56593912 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 351
7455 deg
Eccentricity:
0008053
Arg of perigee: 344
2983 deg
Mean anomaly: 15
7930 deg
Mean motion: 15
73647470 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1562
Checksum: 318
Coasting Arc #14 (Orbit 1577)
---------------------------------------
Vector Time (GMT): 2009/230/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6586370
89 A = 6732519
16 meter
Y = -640624
52 meter E =
0018319
Z = 1174975
93 I = 51
58230
XDOT = -574
223835 Wp = 33
28244
YDOT = 4943
219446 meter/sec RA = 346
34933 deg
ZDOT = 5885
902062 TA = 339
61050
MA = 339
68354
Ha = 191
879 n
mi
Hp = 184
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21608828
38 X = 6587337
25
Y = -2101786
47 feet Y = -566966
51 meter
Z = 3854907
89 Z = 1206974
15
XDOT = -1883
936466 XDOT = -658
049122
YDOT = 16217
911568 feet/sec YDOT = 4936
329133 meter/sec
ZDOT = 19310
702304 ZDOT = 5882
909198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20287979
51 X = -6183776
15
Y = -7666213
43 feet Y = -2336661
85 meter
Z = 3980746
69 Z = 1213331
59
XDOT = 8407
271254 XDOT = 2562
536278
YDOT = -12181
544446 feet/sec YDOT = -3712
934747 meter/sec
ZDOT = 19299
132795 ZDOT = 5882
375676
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 09230
58199560
00010596 00000-0 82463-4 0 9131
2 25544 51
6427 346
5304 0008104 348
3926 11
7048 15
73657724 15789
Satellite: ISS
Catalog Number: 25544
Epoch time: 09230
58199560 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 346
5304 deg
Eccentricity:
0008104
Arg of perigee: 348
3926 deg
Mean anomaly: 11
7048 deg
Mean motion: 15
73657724 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1578
Checksum: 320
Coasting Arc #15 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2009/231/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -9342
58 A = 6721506
97 meter
Y = -4325672
18 meter E =
0014029
Z = -5154566
83 I = 51
51694
XDOT = 7443
011922 Wp = 65
79365
YDOT = -1489
795643 meter/sec RA = 341
18906 deg
ZDOT = 1245
042841 TA = 216
09227
MA = 216
18705
Ha = 191
988 n
mi
Hp = 183
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -30651
52 X = 64067
91
Y = -14191837
85 feet Y = -4325366
09 meter
Z = -16911308
51 Z = -5154434
00
XDOT = 24419
330452 XDOT = 7453
069838
YDOT = -4887
780980 feet/sec YDOT = -1406
507302 meter/sec
ZDOT = 4084
786224 ZDOT = 1281
224572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6120993
29 X = -1865678
75
Y = 12804456
26 feet Y = 3902798
27 meter
Z = -16910969
74 Z = -5154463
58
XDOT = -23212
854032 XDOT = -7075
277909
YDOT = -5549
885937 feet/sec YDOT = -1691
605233 meter/sec
ZDOT = 4227
044790 ZDOT = 1288
403252
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 09231
53454088
00010596 00000-0 82463-4 0 9147
2 25544 51
6428 341
6424 0008167 351
9640 8
1391 15
73697079 15936
Satellite: ISS
Catalog Number: 25544
Epoch time: 09231
53454088 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 341
6424 deg
Eccentricity:
0008167
Arg of perigee: 351
9640 deg
Mean anomaly: 8
1391 deg
Mean motion: 15
73697079 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1593
Checksum: 323
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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