Date:
October 14th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12109 4 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 2443)
---------------------------------------
Vector Time (GMT): 2009/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 811333
60 A = 6726952
48 meter
Y = 6172444
06 meter E =
0012581
Z = 2545978
62 I = 51
95187
XDOT = -5367
151317 Wp = 112
47039
YDOT = -1496
381559 meter/sec RA = 63
84480 deg
ZDOT = 5312
743084 TA = 276
25898
MA = 276
40228
Ha = 190
131 n
mi
Hp = 182
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2661855
64 X = 729883
96
Y = 20250800
73 feet Y = 6181061
54 meter
Z = 8352948
22 Z = 2549722
09
XDOT = -17608
764165 XDOT = -5375
828164
YDOT = -4909
388316 feet/sec YDOT = -1556
448569 meter/sec
ZDOT = 17430
259463 ZDOT = 5286
648231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9516603
43 X = -2900660
73
Y = -18065524
45 feet Y = -5506371
85 meter
Z = 8367988
70 Z = 2550562
96
XDOT = 16992
515751 XDOT = 5179
318801
YDOT = -886
750637 feet/sec YDOT = -270
281594 meter/sec
ZDOT = 17327
274882 ZDOT = 5281
353384
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 09285
55835352
00001200 00000-0 20000-3 0 9000
2 25544 51
6405 64
1731 0008303 192
8324 167
2629 15
74844816 24443
Satellite: ISS
Catalog Number: 25544
Epoch time: 09285
55835352 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 64
1731 deg
Eccentricity:
0008303
Arg of perigee: 192
8324 deg
Mean anomaly: 167
2629 deg
Mean motion: 15
74844816 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2444
Checksum: 295
Coasting Arc #2 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2009/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4861818
59 A = 6721164
70 meter
Y = 1224425
11 meter E =
0013026
Z = -4488063
33 I = 51
91812
XDOT = 1239
198203 Wp = 148
78918
YDOT = 6878
486401 meter/sec RA = 58
67897 deg
ZDOT = 3212
210670 TA = 153
28618
MA = 153
21902
Ha = 189
963 n
mi
Hp = 182
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15950848
38 X = 4869567
88
Y = 4017142
75 feet Y = 1278835
91 meter
Z = -14724617
24 Z = -4464425
68
XDOT = 4065
610902 XDOT = 1146
585212
YDOT = 22567
212602 feet/sec YDOT = 6891
826197 meter/sec
ZDOT = 10538
748916 ZDOT = 3218
005401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16396099
76 X = -4997531
21
Y = 2115017
11 feet Y = 644657
21 meter
Z = -14631335
14 Z = -4459630
95
XDOT = -11812
370566 XDOT = -3600
410549
YDOT = -18352
269179 feet/sec YDOT = -5593
771646 meter/sec
ZDOT = 10561
908944 ZDOT = 3219
269846
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 09286
51019535
00001200 00000-0 20000-3 0 9015
2 25544 51
6408 59
2794 0008113 196
6579 163
4319 15
74834994 24599
Satellite: ISS
Catalog Number: 25544
Epoch time: 09286
51019535 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 59
2794 deg
Eccentricity:
0008113
Arg of perigee: 196
6579 deg
Mean anomaly: 163
4319 deg
Mean motion: 15
74834994 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2459
Checksum: 326
Coasting Arc #3 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2009/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1317052
07 A = 6725593
45 meter
Y = -5834885
61 meter E =
0008905
Z = -3065390
13 I = 51
91718
XDOT = 5764
575590 Wp = 169
89758
YDOT = 1290
605288 meter/sec RA = 53
60372 deg
ZDOT = -4944
118776 TA = 45
51143
MA = 45
43866
Ha = 189
758 n
mi
Hp = 182
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4321036
98 X = -1236816
21
Y = -19143325
50 feet Y = -5849165
28 meter
Z = -10057054
23 Z = -3071593
09
XDOT = 18912
649573 XDOT = 5773
733276
YDOT = 4234
269318 feet/sec YDOT = 1355
118993 meter/sec
ZDOT = -16220
862126 ZDOT = -4916
092024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11235181
67 X = 3424483
37
Y = 16075170
70 feet Y = 4899712
03 meter
Z = -10081775
20 Z = -3072925
08
XDOT = -18014
184146 XDOT = -5490
723328
YDOT = 2508
612086 feet/sec YDOT = 764
624964 meter/sec
ZDOT = -16110
267987 ZDOT = -4910
409683
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 09287
52547294
00001200 00000-0 20000-3 0 9026
2 25544 51
6411 54
0581 0008070 200
6255 159
4584 15
74867829 24759
Satellite: ISS
Catalog Number: 25544
Epoch time: 09287
52547294 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 54
0581 deg
Eccentricity:
0008070
Arg of perigee: 200
6255 deg
Mean anomaly: 159
4584 deg
Mean motion: 15
74867829 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2475
Checksum: 307
Coasting Arc #4 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2009/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5206959
02 A = 6722377
49 meter
Y = -994977
79 meter E =
0008487
Z = 4124505
02 I = 51
88812
XDOT = -1766
481795 Wp = 123
96082
YDOT = -6473
352008 meter/sec RA = 48
43061 deg
ZDOT = -3790
809994 TA = 4
73688
MA = 4
72885
Ha = 189
737 n
mi
Hp = 182
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17083198
90 X = -5215482
43
Y = -3264362
84 feet Y = -1053252
37 meter
Z = 13531840
61 Z = 4099188
60
XDOT = -5795
543947 XDOT = -1675
548998
YDOT = -21238
031522 feet/sec YDOT = -6492
597748 meter/sec
ZDOT = -12437
040663 ZDOT = -3799
170251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17047825
63 X = 5196177
25
Y = -3815330
25 feet Y = -1162912
66 meter
Z = 13431952
80 Z = 4094059
21
XDOT = 13403
823874 XDOT = 4085
485517
YDOT = 15979
391154 feet/sec YDOT = 4870
518424 meter/sec
ZDOT = -12470
292401 ZDOT = -3800
945124
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 09288
54073160
00001200 00000-0 20000-3 0 9036
2 25544 51
6418 48
8379 0007991 203
8449 156
2345 15
74875904 24914
Satellite: ISS
Catalog Number: 25544
Epoch time: 09288
54073160 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 48
8379 deg
Eccentricity:
0007991
Arg of perigee: 203
8449 deg
Mean anomaly: 156
2345 deg
Mean motion: 15
74875904 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2491
Checksum: 322
Coasting Arc #5 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2009/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1715383
20 A = 6723921
54 meter
Y = 5448466
47 meter E =
0011328
Z = 3547240
75 I = 51
87471
XDOT = -6177
326388 Wp = 132
24866
YDOT = -988
055770 meter/sec RA = 43
35611 deg
ZDOT = 4488
340577 TA = 269
86657
MA = 269
99638
Ha = 189
261 n
mi
Hp = 183
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5627897
65 X = 1637097
79
Y = 17875546
18 feet Y = 5467211
49 meter
Z = 11637928
96 Z = 3555383
63
XDOT = -20266
818858 XDOT = -6187
622677
YDOT = -3241
652788 feet/sec YDOT = -1057
191464 meter/sec
ZDOT = 14725
526826 ZDOT = 4458
305559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12440379
63 X = -3791827
71
Y = -13988977
11 feet Y = -4263840
22 meter
Z = 11670271
96 Z = 3557098
89
XDOT = 18856
471715 XDOT = 5747
452579
YDOT = -4538
025007 feet/sec YDOT = -1383
190022 meter/sec
ZDOT = 14607
035566 ZDOT = 4452
224441
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 09289
55596701
00001200 00000-0 20000-3 0 9040
2 25544 51
6429 43
6168 0007950 208
7820 151
2906 15
74969646 25070
Satellite: ISS
Catalog Number: 25544
Epoch time: 09289
55596701 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 43
6168 deg
Eccentricity:
0007950
Arg of perigee: 208
7820 deg
Mean anomaly: 151
2906 deg
Mean motion: 15
74969646 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2507
Checksum: 322
Coasting Arc #6 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2009/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5584688
83 A = 6723676
90 meter
Y = 710201
72 meter E =
0007610
Z = -3683956
82 I = 51
85119
XDOT = 2105
654990 Wp = 170
17277
YDOT = 5993
824827 meter/sec RA = 38
17817 deg
ZDOT = 4341
537187 TA = 145
69762
MA = 145
64845
Ha = 189
066 n
mi
Hp = 183
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18322469
91 X = 5594228
63
Y = 2330058
13 feet Y = 772706
08 meter
Z = -12086472
49 Z = -3656802
56
XDOT = 6908
316897 XDOT = 2017
383538
YDOT = 19664
779617 feet/sec YDOT = 6016
878263 meter/sec
ZDOT = 14243
888408 ZDOT = 4351
551881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17618665
62 X = -5370169
28
Y = 5770828
81 feet Y = 1758948
62 meter
Z = -11979359
27 Z = -3651308
71
XDOT = -14167
882953 XDOT = -4318
370724
YDOT = -13563
279060 feet/sec YDOT = -4134
087457 meter/sec
ZDOT = 14283
626056 ZDOT = 4353
649222
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 09290
50773557
00001200 00000-0 20000-3 0 9054
2 25544 51
6433 38
7232 0007780 213
5901 146
4771 15
74950222 25220
Satellite: ISS
Catalog Number: 25544
Epoch time: 09290
50773557 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 38
7232 deg
Eccentricity:
0007780
Arg of perigee: 213
5901 deg
Mean anomaly: 146
4771 deg
Mean motion: 15
74950222 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2522
Checksum: 286
Coasting Arc #7 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2009/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1916420
77 A = 6722274
01 meter
Y = -5029141
97 meter E =
0004475
Z = -4027079
96 I = 51
82323
XDOT = 6598
542677 Wp = 149
10060
YDOT = 621
087559 meter/sec RA = 33
10116 deg
ZDOT = -3921
444553 TA = 80
55097
MA = 80
50039
Ha = 188
865 n
mi
Hp = 183
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6287469
72 X = -1840478
19
Y = -16499809
61 feet Y = -5050148
11 meter
Z = -13212204
61 Z = -4036205
48
XDOT = 21648
762065 XDOT = 6610
157382
YDOT = 2037
688842 feet/sec YDOT = 694
941090 meter/sec
ZDOT = -12865
631734 ZDOT = -3889
359699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12886638
01 X = 3927847
26
Y = 12031340
16 feet Y = 3667152
48 meter
Z = -13248387
00 Z = -4038108
36
XDOT = -19494
674415 XDOT = -5941
976762
YDOT = 6873
253860 feet/sec YDOT = 2094
967776 meter/sec
ZDOT = -12739
083024 ZDOT = -3882
872506
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 09291
52293489
00001200 00000-0 20000-3 0 9069
2 25544 51
6438 33
5027 0007786 217
0147 143
0480 15
74984394 25381
Satellite: ISS
Catalog Number: 25544
Epoch time: 09291
52293489 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 33
5027 deg
Eccentricity:
0007786
Arg of perigee: 217
0147 deg
Mean anomaly: 143
0480 deg
Mean motion: 15
74984394 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2538
Checksum: 312
Coasting Arc #8 (Orbit 2553)
---------------------------------------
Vector Time (GMT): 2009/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5926464
02 A = 6725087
80 meter
Y = -339926
15 meter E =
0010645
Z = 3145595
35 I = 51
80680
XDOT = -2266
481585 Wp = 129
73530
YDOT = -5531
718259 meter/sec RA = 27
92104 deg
ZDOT = -4863
803928 TA = 13
69797
MA = 13
66911
Ha = 188
769 n
mi
Hp = 183
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19443779
60 X = -5937503
64
Y = -1115243
28 feet Y = -406261
00 meter
Z = 10320194
70 Z = 3116776
89
XDOT = -7435
963204 XDOT = -2180
828287
YDOT = -18148
681951 feet/sec YDOT = -5556
584621 meter/sec
ZDOT = -15957
361968 ZDOT = -4874
606614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17839083
90 X = 5437352
77
Y = -7962686
11 feet Y = -2427026
73 meter
Z = 10206540
41 Z = 3110953
52
XDOT = 14274
063643 XDOT = 4350
734598
YDOT = 11452
105324 feet/sec YDOT = 3490
601703 meter/sec
ZDOT = -16000
167499 ZDOT = -4876
851054
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 09292
53811482
00001200 00000-0 20000-3 0 9071
2 25544 51
6437 28
2826 0007583 220
2960 139
7643 15
75010452 25549
Satellite: ISS
Catalog Number: 25544
Epoch time: 09292
53811482 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 28
2826 deg
Eccentricity:
0007583
Arg of perigee: 220
2960 deg
Mean anomaly: 139
7643 deg
Mean motion: 15
75010452 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2554
Checksum: 292
Coasting Arc #9 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2009/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1987592
63 A = 6720465
02 meter
Y = 4635661
14 meter E =
0009253
Z = 4443383
67 I = 51
76547
XDOT = -6972
959949 Wp = 160
41537
YDOT = -147
342466 meter/sec RA = 22
83608 deg
ZDOT = 3262
329182 TA = 256
89011
MA = 256
99339
Ha = 188
315 n
mi
Hp = 183
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6520973
19 X = 1914022
34
Y = 15208862
01 feet Y = 4657476
25 meter
Z = 14578030
42 Z = 4452860
94
XDOT = -22877
165188 XDOT = -6986
642366
YDOT = -483
407042 feet/sec YDOT = -225
394691 meter/sec
ZDOT = 10703
179732 ZDOT = 3228
420301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12879161
12 X = -3925568
31
Y = -10337500
33 feet Y = -3150870
10 meter
Z = 14615568
47 Z = 4454825
27
XDOT = 19670
585999 XDOT = 5995
594612
YDOT = -9514
854420 feet/sec YDOT = -2900
127627 meter/sec
ZDOT = 10569
459807 ZDOT = 3221
571349
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 09293
55327233
00001200 00000-0 20000-3 0 9081
2 25544 51
6441 23
0611 0007575 225
3606 134
6940 15
75082795 25704
Satellite: ISS
Catalog Number: 25544
Epoch time: 09293
55327233 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 23
0611 deg
Eccentricity:
0007575
Arg of perigee: 225
3606 deg
Mean anomaly: 134
6940 deg
Mean motion: 15
75082795 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2570
Checksum: 287
Coasting Arc #10 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2009/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6234509
48 A = 6726456
80 meter
Y = -102705
97 meter E =
0002133
Z = -2523508
33 I = 51
75688
XDOT = 2235
482023 Wp = 233
92347
YDOT = 5104
204944 meter/sec RA = 17
65677 deg
ZDOT = 5310
841001 TA = 97
54375
MA = 97
51952
Ha = 188
104 n
mi
Hp = 184
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20454427
42 X = 6247453
67
Y = -336961
84 feet Y = -32915
61 meter
Z = -8279226
79 Z = -2493188
82
XDOT = 7334
258605 XDOT = 2152
439965
YDOT = 16746
079213 feet/sec YDOT = 5128
739056 meter/sec
ZDOT = 17424
019032 ZDOT = 5321
499602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17714992
93 X = -5399529
84
Y = 10326740
57 feet Y = 3147590
53 meter
Z = -8159668
84 Z = -2487067
06
XDOT = -13749
046235 XDOT = -4190
709293
YDOT = -9773
439325 feet/sec YDOT = -2978
944306 meter/sec
ZDOT = 17466
225859 ZDOT = 5323
705642
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 09294
50496694
00001200 00000-0 20000-3 0 9096
2 25544 51
6438 18
1672 0007460 230
5581 129
4923 15
75063398 25852
Satellite: ISS
Catalog Number: 25544
Epoch time: 09294
50496694 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 18
1672 deg
Eccentricity:
0007460
Arg of perigee: 230
5581 deg
Mean anomaly: 129
4923 deg
Mean motion: 15
75063398 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2585
Checksum: 320
Coasting Arc #11 (Orbit 2600)
---------------------------------------
Vector Time (GMT): 2009/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1874544
54 A = 6718938
74 meter
Y = -4307561
12 meter E =
0005426
Z = -4807975
73 I = 51
70233
XDOT = 7275
000011 Wp = 97
82446
YDOT = -392
129853 meter/sec RA = 12
56085 deg
ZDOT = -2488
184113 TA = 147
87310
MA = 147
84002
Ha = 187
877 n
mi
Hp = 184
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6150080
51 X = -1802880
50
Y = -14132418
38 feet Y = -4328122
59 meter
Z = -15774198
58 Z = -4816908
49
XDOT = 23868
110273 XDOT = 7290
931608
YDOT = -1286
515267 feet/sec YDOT = -310
687389 meter/sec
ZDOT = -8163
333704 ZDOT = -2452
802642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12358000
96 X = 3766718
69
Y = 9149394
82 feet Y = 2788735
54 meter
Z = -15809568
85 Z = -4818756
59
XDOT = -19335
953478 XDOT = -5893
598620
YDOT = 12269
815349 feet/sec YDOT = 3739
839718 meter/sec
ZDOT = -8023
821959 ZDOT = -2445
660933
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 09295
52008807
00001200 00000-0 20000-3 0 9106
2 25544 51
6430 12
9461 0007443 233
9694 126
0780 15
75100246 26012
Satellite: ISS
Catalog Number: 25544
Epoch time: 09295
52008807 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 12
9461 deg
Eccentricity:
0007443
Arg of perigee: 233
9694 deg
Mean anomaly: 126
0780 deg
Mean motion: 15
75100246 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2601
Checksum: 270
Coasting Arc #12 (Orbit 2616)
---------------------------------------
Vector Time (GMT): 2009/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6444273
38 A = 6727532
47 meter
Y = 603321
61 meter E =
0011795
Z = 1806652
03 I = 51
70204
XDOT = -2043
511153 Wp = 144
90019
YDOT = -4788
805718 meter/sec RA = 7
38560 deg
ZDOT = -5681
169548 TA = 15
06598
MA = 15
03088
Ha = 187
631 n
mi
Hp = 184
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21142629
19 X = -6459317
43
Y = 1979401
61 feet Y = 531173
79 meter
Z = 5927336
07 Z = 1775308
60
XDOT = -6704
432917 XDOT = -1962
211373
YDOT = -15711
304849 feet/sec YDOT = -4811
202766 meter/sec
ZDOT = -18639
007704 ZDOT = -5690
899748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17073296
86 X = 5203940
88
Y = -12683891
30 feet Y = -3866050
07 meter
Z = 5803752
96 Z = 1768983
90
XDOT = 12867
703155 XDOT = 3922
075922
YDOT = 8761
003236 feet/sec YDOT = 2670
353786 meter/sec
ZDOT = -18677
536672 ZDOT = -5692
913178
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
53518939
00001200 00000-0 20000-3 0 9111
2 25544 51
6430 7
7248 0007204 238
3418 121
7043 15
75155601 26171
Satellite: ISS
Catalog Number: 25544
Epoch time: 09296
53518939 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 7
7248 deg
Eccentricity:
0007204
Arg of perigee: 238
3418 deg
Mean anomaly: 121
7043 deg
Mean motion: 15
75155601 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2617
Checksum: 284
Coasting Arc #13 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2009/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1656926
82 A = 6717536
79 meter
Y = 4084154
43 meter E =
0006695
Z = 5073048
13 I = 51
63907
XDOT = -7459
439161 Wp = 201
18514
YDOT = 994
938014 meter/sec RA = 2
27321 deg
ZDOT = 1629
896086 TA = 233
12264
MA = 233
18403
Ha = 187
280 n
mi
Hp = 184
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5436111
61 X = 1586489
58
Y = 13399456
80 feet Y = 4102289
25 meter
Z = 16643858
70 Z = 5080926
59
XDOT = -24473
225594 XDOT = -7477
928199
YDOT = 3264
232331 feet/sec YDOT = 911
418766 meter/sec
ZDOT = 5347
428105 ZDOT = 1593
612624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11666160
08 X = -3555845
59
Y = -8482794
77 feet Y = -2585555
85 meter
Z = 16675061
81 Z = 5082558
84
XDOT = 18362
068018 XDOT = 5596
758332
YDOT = -14987
176242 feet/sec YDOT = -4568
091319 meter/sec
ZDOT = 5204
375118 ZDOT = 1586
293536
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
55027001
00001200 00000-0 20000-3 0 9120
2 25544 51
6431 2
5027 0007281 242
7400 117
3022 15
75193906 26331
Satellite: ISS
Catalog Number: 25544
Epoch time: 09297
55027001 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 2
5027 deg
Eccentricity:
0007281
Arg of perigee: 242
7400 deg
Mean anomaly: 117
3022 deg
Mean motion: 15
75193906 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2633
Checksum: 253
Coasting Arc #14 (Orbit 2647)
---------------------------------------
Vector Time (GMT): 2009/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6549274
54 A = 6728440
30 meter
Y = -1138062
98 meter E =
0005159
Z = -1018467
51 I = 51
64480
XDOT = 1721
656364 Wp = 354
81563
YDOT = 4607
637675 meter/sec RA = 357
10585 deg
ZDOT = 5925
163850 TA = 354
04910
MA = 354
05523
Ha = 187
013 n
mi
Hp = 184
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21487121
20 X = 6566461
40
Y = -3733802
43 feet Y = -1064729
03 meter
Z = -3341428
83 Z = -986608
91
XDOT = 5648
478884 XDOT = 1641
221190
YDOT = 15116
921506 feet/sec YDOT = 4626
440483 meter/sec
ZDOT = 19439
513945 ZDOT = 5933
332428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15940752
08 X = -4858741
23
Y = 14911527
91 feet Y = 4545033
71 meter
Z = -3215830
10 Z = -980185
01
XDOT = -11828
394045 XDOT = -3605
294505
YDOT = -8447
494012 feet/sec YDOT = -2574
796175 meter/sec
ZDOT = 19471
878983 ZDOT = 5935
028714
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
50189201
00001200 00000-0 20000-3 0 9138
2 25544 51
6424 357
6073 0007074 248
2082 111
8330 15
75165110 26488
Satellite: ISS
Catalog Number: 25544
Epoch time: 09298
50189201 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 357
6073 deg
Eccentricity:
0007074
Arg of perigee: 248
2082 deg
Mean anomaly: 111
8330 deg
Mean motion: 15
75165110 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2648
Checksum: 278
Coasting Arc #15 (Orbit 2663)
---------------------------------------
Vector Time (GMT): 2009/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1328931
79 A = 6716764
67 meter
Y = -4004755
71 meter E =
0008193
Z = -5232861
35 I = 51
57608
XDOT = 7498
047819 Wp = 96
58446
YDOT = -1601
985873 meter/sec RA = 351
97426 deg
ZDOT = -680
012375 TA = 166
95145
MA = 166
93024
Ha = 186
760 n
mi
Hp = 184
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4360012
44 X = -1258630
48
Y = -13138962
31 feet Y = -4019223
58 meter
Z = -17168180
29 Z = -5239146
60
XDOT = 24599
894420 XDOT = 7518
707653
YDOT = -5255
859165 feet/sec YDOT = -1518
022774 meter/sec
ZDOT = -2231
011730 ZDOT = -643
536129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10912257
53 X = 3326056
09
Y = 8468081
84 feet Y = 2581071
35 meter
Z = -17193099
76 Z = -5240456
81
XDOT = -16776
648741 XDOT = -5113
522536
YDOT = 17393
363912 feet/sec YDOT = 5301
497320 meter/sec
ZDOT = -2087
220129 ZDOT = -636
184695
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
51693637
00001200 00000-0 20000-3 0 9144
2 25544 51
6424 352
3850 0007050 251
2217 108
8182 15
75216873 26643
Satellite: ISS
Catalog Number: 25544
Epoch time: 09299
51693637 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 352
3850 deg
Eccentricity:
0007050
Arg of perigee: 251
2217 deg
Mean anomaly: 108
8182 deg
Mean motion: 15
75216873 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2664
Checksum: 299
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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