Date:
October 16th 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 2474)
---------------------------------------
Vector Time (GMT): 2009/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1314619
34 A = 6725547
26 meter
Y = -5834451
53 meter E =
0008814
Z = -3067378
20 I = 51
91722
XDOT = 5765
157833 Wp = 169
15171
YDOT = 1293
777281 meter/sec RA = 53
60524 deg
ZDOT = -4942
473186 TA = 46
28337
MA = 46
21040
Ha = 189
713 n
mi
Hp = 182
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4313055
57 X = -1234378
85
Y = -19141901
36 feet Y = -5848703
97 meter
Z = -10063576
78 Z = -3073569
33
XDOT = 18914
559819 XDOT = 5774
272011
YDOT = 4244
676120 feet/sec YDOT = 1358
297254 meter/sec
ZDOT = -16215
463210 ZDOT = -4914
443712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11227224
71 X = 3422058
09
Y = 16076909
81 feet Y = 4900242
11 meter
Z = -10088251
07 Z = -3074898
93
XDOT = -18019
759758 XDOT = -5492
422774
YDOT = 2500
286404 feet/sec YDOT = 762
087296 meter/sec
ZDOT = -16104
858192 ZDOT = -4908
760777
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
52546835
00001200 00000-0 20000-3 0 9004
2 25544 51
6411 54
0597 0007942 200
2421 159
8428 15
74882219 24755
Satellite: ISS
Catalog Number: 25544
Epoch time: 09287
52546835 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 54
0597 deg
Eccentricity:
0007942
Arg of perigee: 200
2421 deg
Mean anomaly: 159
8428 deg
Mean motion: 15
74882219 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2475
Checksum: 301
Coasting Arc #2 (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 = -5209017
00 A = 6722352
77 meter
Y = -1002923
31 meter E =
0008543
Z = 4119893
43 I = 51
88823
XDOT = -1758
145008 Wp = 123
04968
YDOT = -6471
858105 meter/sec RA = 48
43200 deg
ZDOT = -3797
325222 TA = 5
72746
MA = 5
71770
Ha = 189
694 n
mi
Hp = 182
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17089950
79 X = -5217429
00
Y = -3290430
79 feet Y = -1061220
28 meter
Z = 13516710
72 Z = 4094567
28
XDOT = -5768
192283 XDOT = -1667
197885
YDOT = -21233
130266 feet/sec YDOT = -6491
010539 meter/sec
ZDOT = -12458
416082 ZDOT = -3805
644944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17064288
00 X = 5201194
98
Y = -3794047
77 feet Y = -1156425
76 meter
Z = 13416784
20 Z = 4089435
83
XDOT = 13378
211438 XDOT = 4077
678846
YDOT = 15984
597246 feet/sec YDOT = 4872
105241 meter/sec
ZDOT = -12491
507890 ZDOT = -3807
411605
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
54071774
00001200 00000-0 20000-3 0 9013
2 25544 51
6418 48
8394 0007864 203
4501 156
6305 15
74890369 24917
Satellite: ISS
Catalog Number: 25544
Epoch time: 09288
54071774 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 48
8394 deg
Eccentricity:
0007864
Arg of perigee: 203
4501 deg
Mean anomaly: 156
6305 deg
Mean motion: 15
74890369 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2491
Checksum: 312
Coasting Arc #3 (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 = 1703037
65 A = 6723853
34 meter
Y = 5446437
48 meter E =
0011353
Z = 3556008
59 I = 51
87467
XDOT = -6181
820695 Wp = 131
75808
YDOT = -1002
309406 meter/sec RA = 43
35743 deg
ZDOT = 4479
212325 TA = 270
48650
MA = 270
61659
Ha = 189
219 n
mi
Hp = 183
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5587393
85 X = 1624733
24
Y = 17868889
38 feet Y = 5465044
33 meter
Z = 11666694
85 Z = 3564091
45
XDOT = -20281
563959 XDOT = -6191
912919
YDOT = -3288
416685 feet/sec YDOT = -1071
494217 meter/sec
ZDOT = 14695
578494 ZDOT = 4449
155970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12400585
74 X = -3779698
53
Y = -13999695
48 feet Y = -4267107
18 meter
Z = 11698801
05 Z = 3565794
56
XDOT = 18888
257908 XDOT = 5757
141010
YDOT = -4504
340818 feet/sec YDOT = -1372
923081 meter/sec
ZDOT = 14577
002485 ZDOT = 4443
070357
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
55594387
00001200 00000-0 20000-3 0 9026
2 25544 51
6429 43
6183 0007821 208
4027 151
6711 15
74984071 25077
Satellite: ISS
Catalog Number: 25544
Epoch time: 09289
55594387 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 43
6183 deg
Eccentricity:
0007821
Arg of perigee: 208
4027 deg
Mean anomaly: 151
6711 deg
Mean motion: 15
74984071 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2507
Checksum: 305
Coasting Arc #4 (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 = 5590391
72 A = 6723674
46 meter
Y = 726763
70 meter E =
0007499
Z = -3672023
14 I = 51
85137
XDOT = 2085
391703 Wp = 169
42789
YDOT = 5991
291081 meter/sec RA = 38
17938 deg
ZDOT = 4354
830471 TA = 146
62226
MA = 146
57496
Ha = 189
024 n
mi
Hp = 183
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18341180
18 X = 5599687
93
Y = 2384395
34 feet Y = 789330
47 meter
Z = -12047320
02 Z = -3644841
77
XDOT = 6841
836297 XDOT = 1997
085511
YDOT = 19656
466802 feet/sec YDOT = 6014
117727 meter/sec
ZDOT = 14287
501546 ZDOT = 4364
746640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17658635
69 X = -5382352
16
Y = 5729639
44 feet Y = 1746394
10 meter
Z = -11940099
20 Z = -3639342
24
XDOT = -14107
021445 XDOT = -4299
820136
YDOT = -13581
430317 feet/sec YDOT = -4139
619961 meter/sec
ZDOT = 14326
850550 ZDOT = 4366
824048
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
50770372
00001200 00000-0 20000-3 0 9034
2 25544 51
6433 38
7246 0007649 213
2271 146
8413 15
74964357 25227
Satellite: ISS
Catalog Number: 25544
Epoch time: 09290
50770372 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 38
7246 deg
Eccentricity:
0007649
Arg of perigee: 213
2271 deg
Mean anomaly: 146
8413 deg
Mean motion: 15
74964357 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2522
Checksum: 293
Coasting Arc #5 (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 = -1892805
41 A = 6722184
64 meter
Y = -5026967
27 meter E =
0004470
Z = -4041045
78 I = 51
82311
XDOT = 6607
344371 Wp = 146
40304
YDOT = 644
698231 meter/sec RA = 33
10223 deg
ZDOT = -3902
524796 TA = 83
48246
MA = 83
43157
Ha = 188
826 n
mi
Hp = 183
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6209991
51 X = -1816821
05
Y = -16492674
76 feet Y = -5047709
09 meter
Z = -13258024
21 Z = -4050056
47
XDOT = 21677
639012 XDOT = 6618
602491
YDOT = 2115
151676 feet/sec YDOT = 718
648195 meter/sec
ZDOT = -12803
559043 ZDOT = -3870
398050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12813800
30 X = 3905646
33
Y = 12059442
59 feet Y = 3675718
10 meter
Z = -13293753
70 Z = -4051936
13
XDOT = -19552
550048 XDOT = -5959
617255
YDOT = 6821
796223 feet/sec YDOT = 2079
283489 meter/sec
ZDOT = -12676
844209 ZDOT = -3863
902115
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
52289374
00001200 00000-0 20000-3 0 9045
2 25544 51
6438 33
5040 0007657 216
6423 143
4218 15
74998746 25384
Satellite: ISS
Catalog Number: 25544
Epoch time: 09291
52289374 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 33
5040 deg
Eccentricity:
0007657
Arg of perigee: 216
6423 deg
Mean anomaly: 143
4218 deg
Mean motion: 15
74998746 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2538
Checksum: 311
Coasting Arc #6 (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 = -5936249
67 A = 6725104
67 meter
Y = -364254
84 meter E =
0010775
Z = 3124250
57 I = 51
80703
XDOT = -2232
351931 Wp = 129
30271
YDOT = -5529
772960 meter/sec RA = 27
92211 deg
ZDOT = -4881
864789 TA = 14
41826
MA = 14
38754
Ha = 188
732 n
mi
Hp = 183
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19475884
75 X = -5946912
82
Y = -1195061
81 feet Y = -430697
01 meter
Z = 10250165
91 Z = 3095385
49
XDOT = -7323
989275 XDOT = -2146
635184
YDOT = -18142
299736 feet/sec YDOT = -5554
257310 meter/sec
ZDOT = -16016
616761 ZDOT = -4892
501514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17903884
54 X = 5457104
01
Y = -7906323
87 feet Y = -2409847
51 meter
Z = 10136326
84 Z = 3089552
42
XDOT = 14175
460350 XDOT = 4320
680315
YDOT = 11493
271283 feet/sec YDOT = 3503
149087 meter/sec
ZDOT = -16058
767775 ZDOT = -4894
712418
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
53806434
00001200 00000-0 20000-3 0 9050
2 25544 51
6437 28
2839 0007455 219
8984 140
1632 15
75024882 25547
Satellite: ISS
Catalog Number: 25544
Epoch time: 09292
53806434 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 28
2839 deg
Eccentricity:
0007455
Arg of perigee: 219
8984 deg
Mean anomaly: 140
1632 deg
Mean motion: 15
75024882 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2554
Checksum: 309
Coasting Arc #7 (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 = 1951564
10 A = 6720359
43 meter
Y = 4634768
94 meter E =
0009235
Z = 4459997
33 I = 51
76529
XDOT = -6986
347715 Wp = 160
17642
YDOT = -178
733398 meter/sec RA = 22
83685 deg
ZDOT = 3232
294281 TA = 257
46684
MA = 257
57017
Ha = 188
279 n
mi
Hp = 183
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6402769
35 X = 1877925
75
Y = 15205934
85 feet Y = 4656180
78 meter
Z = 14632537
16 Z = 4469299
40
XDOT = -22921
088303 XDOT = -6999
532209
YDOT = -586
395662 feet/sec YDOT = -256
932548 meter/sec
ZDOT = 10604
640029 ZDOT = 3198
321569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12773430
81 X = -3893341
71
Y = -10391134
81 feet Y = -3167217
89 meter
Z = 14669384
32 Z = 4471228
34
XDOT = 19753
682207 XDOT = 6020
922337
YDOT = -9452
452093 feet/sec YDOT = -2881
107398 meter/sec
ZDOT = 10470
667276 ZDOT = 3191
459386
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
55321253
00001200 00000-0 20000-3 0 9065
2 25544 51
6441 23
0624 0007446 224
9858 135
0704 15
75097342 25706
Satellite: ISS
Catalog Number: 25544
Epoch time: 09293
55321253 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 23
0624 deg
Eccentricity:
0007446
Arg of perigee: 224
9858 deg
Mean anomaly: 135
0704 deg
Mean motion: 15
75097342 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2570
Checksum: 283
Coasting Arc #8 (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 = 6247568
79 A = 6726485
17 meter
Y = -72373
71 meter E =
0001927
Z = -2492013
86 I = 51
75714
XDOT = 2186
896691 Wp = 235
64014
YDOT = 5104
932385 meter/sec RA = 17
65775 deg
ZDOT = 5330
390650 TA = 96
21517
MA = 96
19323
Ha = 188
068 n
mi
Hp = 184
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20497272
95 X = 6260019
83
Y = -237446
55 feet Y = -2440
07 meter
Z = -8175898
48 Z = -2461632
10
XDOT = 7174
857911 XDOT = 2103
755139
YDOT = 16748
465830 feet/sec YDOT = 5128
922631 meter/sec
ZDOT = 17488
158300 ZDOT = 5340
812975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17800529
63 X = -5425601
43
Y = 10260623
24 feet Y = 3127437
96 meter
Z = -8056094
02 Z = -2455497
46
XDOT = -13615
700044 XDOT = -4150
065373
YDOT = -9847
468049 feet/sec YDOT = -3001
508261 meter/sec
ZDOT = 17529
433426 ZDOT = 5342
971308
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
50489839
00001200 00000-0 20000-3 0 9077
2 25544 51
6438 18
1683 0007327 230
2206 129
8313 15
75077243 25858
Satellite: ISS
Catalog Number: 25544
Epoch time: 09294
50489839 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 18
1683 deg
Eccentricity:
0007327
Arg of perigee: 230
2206 deg
Mean anomaly: 129
8313 deg
Mean motion: 15
75077243 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2585
Checksum: 307
Coasting Arc #9 (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 = -1825381
35 A = 6718829
35 meter
Y = -4310140
47 meter E =
0005670
Z = -4824643
99 I = 51
70213
XDOT = 7291
254360 Wp = 97
22031
YDOT = -353
965725 meter/sec RA = 12
56126 deg
ZDOT = -2445
534637 TA = 148
92002
MA = 148
88646
Ha = 187
845 n
mi
Hp = 184
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5988783
94 X = -1753611
14
Y = -14140880
80 feet Y = -4330151
57 meter
Z = -15828884
47 Z = -4833337
65
XDOT = 23921
438188 XDOT = 7306
550802
YDOT = -1161
304873 feet/sec YDOT = -272
345047 meter/sec
ZDOT = -8023
407601 ZDOT = -2410
075742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12222708
81 X = 3725481
65
Y = 9238200
55 feet Y = 2815803
53 meter
Z = -15863311
96 Z = -4835137
48
XDOT = -19437
964036 XDOT = -5924
691438
YDOT = 12198
033469 feet/sec YDOT = 3717
960601 meter/sec
ZDOT = -7883
589261 ZDOT = -2402
918007
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
52001016
00001200 00000-0 20000-3 0 9088
2 25544 51
6430 12
9472 0007313 233
6136 126
4354 15
75114626 26016
Satellite: ISS
Catalog Number: 25544
Epoch time: 09295
52001016 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 12
9472 deg
Eccentricity:
0007313
Arg of perigee: 233
6136 deg
Mean anomaly: 126
4354 deg
Mean motion: 15
75114626 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2601
Checksum: 256
Coasting Arc #10 (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 = -6459439
37 A = 6727557
95 meter
Y = 566977
46 meter E =
0011916
Z = 1763623
69 I = 51
70228
XDOT = -1979
407158 Wp = 144
87650
YDOT = -4794
669528 meter/sec RA = 7
38652 deg
ZDOT = -5698
965191 TA = 15
58644
MA = 15
54978
Ha = 187
599 n
mi
Hp = 184
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21192386
38 X = -6473866
86
Y = 1860162
27 feet Y = 494663
50 meter
Z = 5786166
95 Z = 1732208
07
XDOT = -6494
117974 XDOT = -1897
960123
YDOT = -15730
543072 feet/sec YDOT = -4816
348904 meter/sec
ZDOT = -18697
392360 ZDOT = -5708
383611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17177014
11 X = 5235553
90
Y = -12607368
47 feet Y = -3842725
91 meter
Z = 5662298
00 Z = 1725868
43
XDOT = 12703
216161 XDOT = 3871
940286
YDOT = 8879
224362 feet/sec YDOT = 2706
387585 meter/sec
ZDOT = -18734
692011 ZDOT = -5710
334125
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
53510212
00001200 00000-0 20000-3 0 9094
2 25544 51
6430 7
7258 0007073 237
9593 122
0884 15
75169769 26172
Satellite: ISS
Catalog Number: 25544
Epoch time: 09296
53510212 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 7
7258 deg
Eccentricity:
0007073
Arg of perigee: 237
9593 deg
Mean anomaly: 122
0884 deg
Mean motion: 15
75169769 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2617
Checksum: 308
Coasting Arc #11 (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 = 1594600
99 A = 6717437
04 meter
Y = 4092201
14 meter E =
0006596
Z = 5086297
49 I = 51
63890
XDOT = -7477
326617 Wp = 201
27733
YDOT = 950
205940 meter/sec RA = 2
27325 deg
ZDOT = 1574
316862 TA = 233
57801
MA = 233
63885
Ha = 187
248 n
mi
Hp = 184
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5231630
56 X = 1524014
04
Y = 13425856
77 feet Y = 4109638
16 meter
Z = 16687327
72 Z = 5093872
80
XDOT = -24531
911473 XDOT = -7495
044125
YDOT = 3117
473555 feet/sec YDOT = 866
490978 meter/sec
ZDOT = 5165
081569 ZDOT = 1537
948374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11507110
89 X = -3507367
40
Y = -8614382
37 feet Y = -2625663
75 meter
Z = 16717335
61 Z = 5095443
89
XDOT = 18479
525030 XDOT = 5632
559229
YDOT = -14905
409983 feet/sec YDOT = -4543
168963 meter/sec
ZDOT = 5021
691813 ZDOT = 1530
611665
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
55017335
00001200 00000-0 20000-3 0 9107
2 25544 51
6431 2
5037 0007152 242
3873 117
6565 15
75208650 26337
Satellite: ISS
Catalog Number: 25544
Epoch time: 09297
55017335 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 2
5037 deg
Eccentricity:
0007152
Arg of perigee: 242
3873 deg
Mean anomaly: 117
6565 deg
Mean motion: 15
75208650 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2633
Checksum: 276
Coasting Arc #12 (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 = 6564587
23 A = 6728445
66 meter
Y = -1095916
05 meter E =
0005251
Z = -964428
73 I = 51
64498
XDOT = 1643
089256 Wp = 357
84586
YDOT = 4621
042333 meter/sec RA = 357
10671 deg
ZDOT = 5937
080132 TA = 351
61661
MA = 351
62538
Ha = 186
985 n
mi
Hp = 184
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21537359
67 X = 6581039
14
Y = -3595525
08 feet Y = -1022414
97 meter
Z = -3164136
25 Z = -932497
53
XDOT = 5390
712783 XDOT = 1562
452140
YDOT = 15160
900042 feet/sec YDOT = 4638
965428 meter/sec
ZDOT = 19478
609356 ZDOT = 5944
866534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16057702
17 X = -4894387
62
Y = 14822842
49 feet Y = 4518002
39 meter
Z = -3038249
80 Z = -926058
54
XDOT = -11643
189945 XDOT = -3548
844295
YDOT = -8617
165727 feet/sec YDOT = -2626
512113 meter/sec
ZDOT = 19509
467706 ZDOT = 5946
485757
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
50178655
00001200 00000-0 20000-3 0 9117
2 25544 51
6424 357
6082 0006938 247
8940 112
1487 15
75179014 26489
Satellite: ISS
Catalog Number: 25544
Epoch time: 09298
50178655 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 357
6082 deg
Eccentricity:
0006938
Arg of perigee: 247
8940 deg
Mean anomaly: 112
1487 deg
Mean motion: 15
75179014 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2648
Checksum: 318
Coasting Arc #13 (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 = -1254290
76 A = 6716696
64 meter
Y = -4020462
30 meter E =
0008398
Z = -5239320
34 I = 51
57600
XDOT = 7514
783284 Wp = 97
29533
YDOT = -1549
695970 meter/sec RA = 351
97393 deg
ZDOT = -611
737899 TA = 166
89324
MA = 166
87141
Ha = 186
737 n
mi
Hp = 184
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4115127
18 X = -1183787
99
Y = -13190493
11 feet Y = -4034094
36 meter
Z = -17189371
19 Z = -5245242
48
XDOT = 24654
800800 XDOT = 7534
525489
YDOT = -5084
304363 feet/sec YDOT = -1465
550855 meter/sec
ZDOT = -2007
014104 ZDOT = -575
182580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10738664
13 X = 3273144
83
Y = 8648492
94 feet Y = 2636060
65 meter
Z = -17212859
28 Z = -5246479
51
XDOT = -16904
302684 XDOT = -5152
431458
YDOT = 17294
318440 feet/sec YDOT = 5271
308261 meter/sec
ZDOT = -1862
908936 ZDOT = -567
814644
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
51682149
00001200 00000-0 20000-3 0 9128
2 25544 51
6424 352
3859 0006919 250
8906 109
1509 15
75231256 26644
Satellite: ISS
Catalog Number: 25544
Epoch time: 09299
51682149 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 352
3859 deg
Eccentricity:
0006919
Arg of perigee: 250
8906 deg
Mean anomaly: 109
1509 deg
Mean motion: 15
75231256 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2664
Checksum: 314
Coasting Arc #14 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2009/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6526544
72 A = 6728488
12 meter
Y = 1604551
85 meter E =
0010570
Z = 93398
09 I = 51
58743
XDOT = -1226
135502 Wp = 166
64834
YDOT = -4628
695150 meter/sec RA = 346
81913 deg
ZDOT = -6036
140947 TA = 12
33555
MA = 12
30969
Ha = 186
324 n
mi
Hp = 184
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21412548
28 X = -6544455
74
Y = 5264277
73 feet Y = 1531468
04 meter
Z = 306424
17 Z = 61648
09
XDOT = -4022
754273 XDOT = -1144
962557
YDOT = -15186
007709 feet/sec YDOT = -4641
952804 meter/sec
ZDOT = -19803
612030 ZDOT = -6041
900321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14460564
75 X = 4407580
14
Y = -16648211
51 feet Y = -5074374
87 meter
Z = 181274
10 Z = 55252
35
XDOT = 10734
512898 XDOT = 3271
879531
YDOT = 9100
517434 feet/sec YDOT = 2773
837714 meter/sec
ZDOT = -19826
480167 ZDOT = -6043
111155
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
53183630
00001200 00000-0 20000-3 0 9135
2 25544 51
6430 347
1638 0006718 255
7052 104
3366 15
75298237 26809
Satellite: ISS
Catalog Number: 25544
Epoch time: 09300
53183630 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 347
1638 deg
Eccentricity:
0006718
Arg of perigee: 255
7052 deg
Mean anomaly: 104
3366 deg
Mean motion: 15
75298237 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2680
Checksum: 286
Coasting Arc #15 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2009/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730759
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 883452
75 A = 6716392
66 meter
Y = 4102029
63 meter E =
0004100
Z = 5247793
76 I = 51
51732
XDOT = -7394
555609 Wp = 264
85757
YDOT = 2110
767144 meter/sec RA = 341
66505 deg
ZDOT = -405
695866 TA = 188
99778
MA = 189
00513
Ha = 186
020 n
mi
Hp = 184
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2898467
03 X = 812024
19
Y = 13458102
45 feet Y = 4111509
74 meter
Z = 17217171
13 Z = 5251911
99
XDOT = -24260
353047 XDOT = -7415
638156
YDOT = 6925
089054 feet/sec YDOT = 2027
958968 meter/sec
ZDOT = -1331
023182 ZDOT = -441
670552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10205879
57 X = -3110752
09
Y = -9208547
56 feet Y = -2806765
29 meter
Z = 17233551
25 Z = 5252786
42
XDOT = 14810
167562 XDOT = 4514
139073
YDOT = -19166
628711 feet/sec YDOT = -5841
988431 meter/sec
ZDOT = -1472
810479 ZDOT = -448
912634
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
54683166
00001200 00000-0 20000-3 0 9147
2 25544 51
6424 341
9418 0006705 259
4828 100
5581 15
75324796 26962
Satellite: ISS
Catalog Number: 25544
Epoch time: 09301
54683166 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 341
9418 deg
Eccentricity:
0006705
Arg of perigee: 259
4828 deg
Mean anomaly: 100
5581 deg
Mean motion: 15
75324796 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2696
Checksum: 311
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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