Date:
February 1st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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
035/08:34:45
300 -0
6 1
7 1
7
N/A -1
5 0
0 196
6
000/00:09:26
601 -0
6 0
2 189
6
Coasting Arc #1 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2009/030/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4527059
97 A = 6735198
47 meter
Y = 3195005
62 meter E =
0009054
Z = -3837448
09 I = 51
33302
XDOT = -1041
927053 Wp = 9
63848
YDOT = -6415
602724 meter/sec RA = 291
13229 deg
ZDOT = -4104
980578 TA = 217
18059
MA = 217
24332
Ha = 195
866 n
mi
Hp = 189
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14852558
97 X = -4543809
31
Y = 10482301
90 feet Y = 3144287
72 meter
Z = -12590052
79 Z = -3859480
85
XDOT = -3418
395843 XDOT = -950
168398
YDOT = -21048
565368 feet/sec YDOT = -6426
741148 meter/sec
ZDOT = -13467
784048 ZDOT = -4109
819227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17941448
23 X = -5468553
42
Y = -2533717
03 feet Y = -772276
95 meter
Z = -12675618
47 Z = -3863528
51
XDOT = 11845
263097 XDOT = 3610
436192
YDOT = -16283
906706 feet/sec YDOT = -4963
334764 meter/sec
ZDOT = -13487
072401 ZDOT = -4110
859668
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 09030
54434781
00010596 00000-0 82463-4 0 9008
2 25544 51
6427 291
6481 0008559 326
9467 33
1159 15
70676355 24308
Satellite: ISS
Catalog Number: 25544
Epoch time: 09030
54434781 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 291
6481 deg
Eccentricity:
0008559
Arg of perigee: 326
9467 deg
Mean anomaly: 33
1159 deg
Mean motion: 15
70676355 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2430
Checksum: 316
Coasting Arc #2 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2009/031/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2235761
52 A = 6733497
19 meter
Y = 4683490
40 meter E =
0011784
Z = 4292367
98 I = 51
31785
XDOT = -4392
023369 Wp = 25
42476
YDOT = 5282
045723 meter/sec RA = 285
94906 deg
ZDOT = -3461
662555 TA = 99
84477
MA = 99
71170
Ha = 195
978 n
mi
Hp = 189
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7335175
60 X = 2162372
53
Y = 15365782
15 feet Y = 4708081
68 meter
Z = 14082572
11 Z = 4303050
86
XDOT = -14409
525490 XDOT = -4433
945756
YDOT = 17329
546334 feet/sec YDOT = 5232
697140 meter/sec
ZDOT = -11357
160614 ZDOT = -3483
100575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5004081
17 X = -1525243
94
Y = 16238491
07 feet Y = 4949492
08 meter
Z = 14124499
24 Z = 4305147
37
XDOT = -21093
275868 XDOT = -6429
230485
YDOT = 3490
661611 feet/sec YDOT = 1063
953659 meter/sec
ZDOT = -11440
259834 ZDOT = -3486
991198
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 09031
56232811
00010596 00000-0 82463-4 0 9012
2 25544 51
6423 286
4457 0008646 331
2750 28
7934 15
70723126 24467
Satellite: ISS
Catalog Number: 25544
Epoch time: 09031
56232811 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 286
4457 deg
Eccentricity:
0008646
Arg of perigee: 331
2750 deg
Mean anomaly: 28
7934 deg
Mean motion: 15
70723126 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2446
Checksum: 299
Coasting Arc #3 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2009/032/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2808549
06 A = 6739670
48 meter
Y = -5745379
78 meter E =
0015852
Z = 2094222
16 I = 51
33137
XDOT = 3755
122543 Wp = 36
77900
YDOT = 3848
983447 meter/sec RA = 280
85867 deg
ZDOT = 5514
491138 TA = 346
71128
MA = 346
75298
Ha = 196
120 n
mi
Hp = 189
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9214399
82 X = 2862412
87
Y = -18849671
20 feet Y = -5713671
80 meter
Z = 6870807
62 Z = 2107996
76
XDOT = 12319
955851 XDOT = 3685
015359
YDOT = 12627
898448 feet/sec YDOT = 3890
583395 meter/sec
ZDOT = 18092
162525 ZDOT = 5532
563063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19349186
18 X = 5897631
95
Y = -8067839
57 feet Y = -2459077
50 meter
Z = 6924032
39 Z = 2110445
07
XDOT = 219
694963 XDOT = 66
963025
YDOT = 16139
851070 feet/sec YDOT = 4919
426606 meter/sec
ZDOT = 18162
804073 ZDOT = 5536
022681
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 09032
58029963
00010596 00000-0 82463-4 0 9028
2 25544 51
6422 281
2427 0008687 335
1127 24
9615 15
70695730 24623
Satellite: ISS
Catalog Number: 25544
Epoch time: 09032
58029963 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 281
2427 deg
Eccentricity:
0008687
Arg of perigee: 335
1127 deg
Mean anomaly: 24
9615 deg
Mean motion: 15
70695730 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2462
Checksum: 311
Coasting Arc #4 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2009/033/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3965413
52 A = 6729920
47 meter
Y = -1783332
13 meter E =
0012184
Z = -5145071
88 I = 51
29438
XDOT = 1731
157464 Wp = 61
97821
YDOT = -7388
918893 meter/sec RA = 275
69507 deg
ZDOT = 1234
699420 TA = 219
85217
MA = 219
94170
Ha = 196
172 n
mi
Hp = 189
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13009886
88 X = -3920183
67
Y = -5850827
21 feet Y = -1827422
67 meter
Z = -16880157
08 Z = -5164225
87
XDOT = 5679
650474 XDOT = 1807
655018
YDOT = -24241
859886 feet/sec YDOT = -7369
132395 meter/sec
ZDOT = 4050
851115 ZDOT = 1243
294946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6035069
62 X = -1839489
22
Y = -12827292
84 feet Y = -3909758
86 meter
Z = -16954867
50 Z = -5167843
61
XDOT = 19090
534450 XDOT = 5818
794900
YDOT = -14345
752112 feet/sec YDOT = -4372
585244 meter/sec
ZDOT = 4083
791208 ZDOT = 1244
739560
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 09033
53463694
00010596 00000-0 82463-4 0 9038
2 25544 51
6419 276
3653 0008703 337
9837 22
0950 15
70738392 24771
Satellite: ISS
Catalog Number: 25544
Epoch time: 09033
53463694 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 276
3653 deg
Eccentricity:
0008703
Arg of perigee: 337
9837 deg
Mean anomaly: 22
0950 deg
Mean motion: 15
70738392 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2477
Checksum: 329
Coasting Arc #5 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2009/034/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -101365
11 A = 6741573
57 meter
Y = 6740381
53 meter E =
0005883
Z = -42534
04 I = 51
33158
XDOT = -4803
647337 Wp = 94
70514
YDOT = -105
612995 meter/sec RA = 270
57227 deg
ZDOT = -6003
729031 TA = 85
75787
MA = 85
69064
Ha = 196
390 n
mi
Hp = 189
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -332562
69 X = -176523
02
Y = 22114112
62 feet Y = 6738827
77 meter
Z = -139547
39 Z = -43208
71
XDOT = -15759
997824 XDOT = -4772
944575
YDOT = -346
499327 feet/sec YDOT = -159
158216 meter/sec
ZDOT = -19697
273725 ZDOT = -6026
990366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14304972
71 X = -4360155
68
Y = 16867475
45 feet Y = 5141206
52 meter
Z = -141689
68 Z = -43187
01
XDOT = -10632
883639 XDOT = -3240
902933
YDOT = -9164
351914 feet/sec YDOT = -2793
294463 meter/sec
ZDOT = -19787
862129 ZDOT = -6031
340377
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 09034
55258913
00010596 00000-0 82463-4 0 9048
2 25544 51
6419 271
1633 0008558 341
5519 18
5331 15
70701126 24934
Satellite: ISS
Catalog Number: 25544
Epoch time: 09034
55258913 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 271
1633 deg
Eccentricity:
0008558
Arg of perigee: 341
5519 deg
Mean anomaly: 18
5331 deg
Mean motion: 15
70701126 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2493
Checksum: 302
Coasting Arc #6 (Orbit 2505)
---------------------------------------
Vector Time (GMT): 2009/035/08:39:28
601
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3893266
70 A = 6731308
47 meter
Y = 2230104
84 meter E =
0014562
Z = -5029229
21 I = 51
29439
XDOT = -1877
809043 Wp = 42
31311
YDOT = -7244
035841 meter/sec RA = 266
27340 deg
ZDOT = -1750
889072 TA = 210
67057
MA = 210
75577
Ha = 196
553 n
mi
Hp = 189
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12773184
71 X = -3893483
94
Y = 7316616
92 feet Y = 2186567
19 meter
Z = -16500095
83 Z = -5048142
86
XDOT = -6160
790822 XDOT = -1788
160071
YDOT = -23766
521789 feet/sec YDOT = -7264
533224 meter/sec
ZDOT = -5744
386718 ZDOT = -1759
794084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5894139
02 X = -1796533
57
Y = -13398340
31 feet Y = -4083814
13 meter
Z = -16573590
30 Z = -5051630
32
XDOT = 23315
027155 XDOT = 7106
420277
YDOT = -3076
409810 feet/sec YDOT = -937
689710 meter/sec
ZDOT = -5779
589031 ZDOT = -1761
618737
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 09035
37966978
00010596 00000-0 82463-4 0 9057
2 25544 51
6411 266
9357 0008351 337
2770 22
8021 15
70438493 25066
Satellite: ISS
Catalog Number: 25544
Epoch time: 09035
37966978 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 266
9357 deg
Eccentricity:
0008351
Arg of perigee: 337
2770 deg
Mean anomaly: 22
8021 deg
Mean motion: 15
70438493 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2506
Checksum: 323
Coasting Arc #7 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2009/036/08:39:28
601
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2952033
54 A = 6739422
83 meter
Y = 5478287
23 meter E =
0011653
Z = 2585379
61 I = 51
32453
XDOT = -3547
269310 Wp = 65
64779
YDOT = 4388
826485 meter/sec RA = 261
10508 deg
ZDOT = -5226
096059 TA = 84
91742
MA = 84
78443
Ha = 196
713 n
mi
Hp = 189
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9685149
40 X = 2877995
93
Y = 17973383
29 feet Y = 5510884
40 meter
Z = 8482216
57 Z = 2599540
95
XDOT = -11638
022671 XDOT = -3570
695252
YDOT = 14399
037024 feet/sec YDOT = 4349
028298 meter/sec
ZDOT = -17145
984447 ZDOT = -5243
384954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18780969
52 X = -5724439
51
Y = 7948225
40 feet Y = 2422619
10 meter
Z = 8537770
22 Z = 2602312
36
XDOT = -12701
124947 XDOT = -3871
302884
YDOT = -11440
457940 feet/sec YDOT = -3487
051580 meter/sec
ZDOT = -17212
999258 ZDOT = -5246
522174
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 09036
39781405
00010596 00000-0 82463-4 0 9061
2 25544 51
6408 261
7349 0008361 340
7672 19
3173 15
70431457 25227
Satellite: ISS
Catalog Number: 25544
Epoch time: 09036
39781405 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 261
7349 deg
Eccentricity:
0008361
Arg of perigee: 340
7672 deg
Mean anomaly: 19
3173 deg
Mean motion: 15
70431457 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2522
Checksum: 308
Coasting Arc #8 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2009/037/08:39:28
601
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1938694
54 A = 6735681
82 meter
Y = -5130559
62 meter E =
0010738
Z = 3897632
73 I = 51
31781
XDOT = 4510
901183 Wp = 54
77735
YDOT = 4766
726490 meter/sec RA = 256
02158 deg
ZDOT = 4029
129328 TA = 353
13003
MA = 353
14474
Ha = 196
783 n
mi
Hp = 189
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6360546
39 X = 1976987
66
Y = -16832544
69 feet Y = -5108666
22 meter
Z = 12787508
97 Z = 3907143
29
XDOT = 14799
544563 XDOT = 4437
691274
YDOT = 15638
866438 feet/sec YDOT = 4816
760342 meter/sec
ZDOT = 13218
928242 ZDOT = 4050
865342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16317223
59 X = 4973489
75
Y = 7523315
39 feet Y = 2293106
53 meter
Z = 12824173
92 Z = 3908808
21
XDOT = -16143
899719 XDOT = -4920
660634
YDOT = 12327
004321 feet/sec YDOT = 3757
270917 meter/sec
ZDOT = 13303
945806 ZDOT = 4055
042682
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 09037
41594828
00010596 00000-0 82463-4 0 9077
2 25544 51
6408 256
5336 0008439 344
8635 15
2273 15
70445830 25388
Satellite: ISS
Catalog Number: 25544
Epoch time: 09037
41594828 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 256
5336 deg
Eccentricity:
0008439
Arg of perigee: 344
8635 deg
Mean anomaly: 15
2273 deg
Mean motion: 15
70445830 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2538
Checksum: 325
Coasting Arc #9 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2009/038/08:39:28
601
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4522729
92 A = 6734162
66 meter
Y = -2548002
48 meter E =
0008302
Z = -4292060
45 I = 51
32155
XDOT = 566
741313 Wp = 50
92435
YDOT = -6839
748759 meter/sec RA = 250
84023 deg
ZDOT = 3472
903441 TA = 254
36503
MA = 254
45666
Ha = 196
867 n
mi
Hp = 188
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14838352
77 X = -4473052
16
Y = -8359588
20 feet Y = -2598300
23 meter
Z = -14081563
14 Z = -4313910
73
XDOT = 1859
387510 XDOT = 626
312153
YDOT = -22440
120601 feet/sec YDOT = -6833
078279 meter/sec
ZDOT = 11394
040161 ZDOT = 3475
800834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9192175
90 X = 2801775
21
Y = -14253189
00 feet Y = -4344372
01 meter
Z = -14166875
23 Z = -4318063
57
XDOT = 21260
871211 XDOT = 6480
313545
YDOT = 2407
119394 feet/sec YDOT = 733
689991 meter/sec
ZDOT = 11404
809741 ZDOT = 3476
186009
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 09038
37043947
00010596 00000-0 82463-4 0 9085
2 25544 51
6409 251
6577 0008532 347
9544 12
1412 15
70471011 25537
Satellite: ISS
Catalog Number: 25544
Epoch time: 09038
37043947 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 251
6577 deg
Eccentricity:
0008532
Arg of perigee: 347
9544 deg
Mean anomaly: 12
1412 deg
Mean motion: 15
70471011 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2553
Checksum: 302
Coasting Arc #10 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2009/039/08:39:28
601
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1049673
78 A = 6740440
86 meter
Y = 6335537
58 meter E =
0004444
Z = -2056940
94 I = 51
35321
XDOT = -5262
115699 Wp = 41
41685
YDOT = -921
433932 meter/sec RA = 245
75263 deg
ZDOT = -5526
929761 TA = 161
57282
MA = 161
55672
Ha = 197
055 n
mi
Hp = 188
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3443811
62 X = 988742
65
Y = 20785884
44 feet Y = 6346935
03 meter
Z = -6748493
89 Z = -2051989
55
XDOT = -17264
159116 XDOT = -5224
573055
YDOT = -3023
077206 feet/sec YDOT = -980
067848 meter/sec
ZDOT = -18132
971657 ZDOT = -5552
401112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20908917
79 X = -6373038
14
Y = 2645107
45 feet Y = 806228
75 meter
Z = -6728711
89 Z = -2050911
38
XDOT = 3902
839685 XDOT = 1189
585536
YDOT = -15499
254121 feet/sec YDOT = -4724
172656 meter/sec
ZDOT = -18232
278615 ZDOT = -5557
198522
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 09039
38855446
00010596 00000-0 82463-4 0 9093
2 25544 51
6408 246
4563 0008473 350
9755 9
1252 15
70461343 25697
Satellite: ISS
Catalog Number: 25544
Epoch time: 09039
38855446 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 246
4563 deg
Eccentricity:
0008473
Arg of perigee: 350
9755 deg
Mean anomaly: 9
1252 deg
Mean motion: 15
70461343 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2569
Checksum: 330
Coasting Arc #11 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2009/040/08:39:28
601
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4212329
44 A = 6730378
45 meter
Y = -941782
65 meter E =
0010958
Z = 5163737
55 I = 51
33309
XDOT = 2941
799019 Wp = 12
43117
YDOT = 7024
761153 meter/sec RA = 240
59431 deg
ZDOT = -1107
588832 TA = 88
25324
MA = 88
12773
Ha = 197
000 n
mi
Hp = 188
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13819978
47 X = 4197463
89
Y = -3089838
08 feet Y = -894761
07 meter
Z = 16941396
15 Z = 5184164
23
XDOT = 9651
571586 XDOT = 2868
408620
YDOT = 23047
116645 feet/sec YDOT = 7057
247717 meter/sec
ZDOT = -3633
821627 ZDOT = -1093
476293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2773694
85 X = 845422
19
Y = 13789310
06 feet Y = 4202981
71 meter
Z = 17020909
29 Z = 5187973
15
XDOT = -22257
624598 XDOT = -6784
123977
YDOT = 8938
228603 feet/sec YDOT = 2724
372078 meter/sec
ZDOT = -3578
275670 ZDOT = -1090
658424
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 09040
40665757
00010596 00000-0 82463-4 0 9104
2 25544 51
6405 241
2544 0008647 354
5823 5
5243 15
70538639 25856
Satellite: ISS
Catalog Number: 25544
Epoch time: 09040
40665757 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 241
2544 deg
Eccentricity:
0008647
Arg of perigee: 354
5823 deg
Mean anomaly: 5
5243 deg
Mean motion: 15
70538639 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2585
Checksum: 310
Coasting Arc #12 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2009/041/08:39:28
601
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3925771
04 A = 6742071
21 meter
Y = -5464463
47 meter E =
0018990
Z = -171525
48 I = 51
38797
XDOT = 3819
155305 Wp = 24
90588
YDOT = -2924
465435 meter/sec RA = 235
47242 deg
ZDOT = 6015
300518 TA = 333
22514
MA = 333
32305
Ha = 197
207 n
mi
Hp = 188
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12879826
25 X = -3863541
52
Y = -17928029
77 feet Y = -5508015
79 meter
Z = -562747
64 Z = -190444
98
XDOT = 12530
037090 XDOT = 3822
352995
YDOT = -9594
702872 feet/sec YDOT = -2881
739382 meter/sec
ZDOT = 19735
237919 ZDOT = 6033
861232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18002004
68 X = 5487011
03
Y = -12772745
57 feet Y = -3893132
85 meter
Z = -636913
35 Z = -194131
19
XDOT = 8591
344103 XDOT = 2618
641683
YDOT = 11158
322147 feet/sec YDOT = 3401
056590 meter/sec
ZDOT = 19807
321511 ZDOT = 6037
271596
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 09041
36112256
00010596 00000-0 82463-4 0 9112
2 25544 51
6407 236
3776 0008695 358
3570 1
7561 15
70525378 26009
Satellite: ISS
Catalog Number: 25544
Epoch time: 09041
36112256 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 236
3776 deg
Eccentricity:
0008695
Arg of perigee: 358
3570 deg
Mean anomaly: 1
7561 deg
Mean motion: 15
70525378 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2600
Checksum: 301
Coasting Arc #13 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2009/042/08:39:28
601
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2093110
27 A = 6730699
39 meter
Y = 3871315
51 meter E =
0018018
Z = -5107020
03 I = 51
36742
XDOT = -5653
194293 Wp = 50
46972
YDOT = -4993
690117 meter/sec RA = 230
35829 deg
ZDOT = -1460
596191 TA = 205
40081
MA = 205
48948
Ha = 197
344 n
mi
Hp = 188
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6867159
69 X = -2111436
08
Y = 12701166
38 feet Y = 3847806
43 meter
Z = -16755315
06 Z = -5117232
78
XDOT = -18547
225370 XDOT = -5589
838744
YDOT = -16383
497759 feet/sec YDOT = -5056
553252 meter/sec
ZDOT = -4791
982254 ZDOT = -1487
904551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12777596
24 X = -3894611
33
Y = -6624663
92 feet Y = -2019197
56 meter
Z = -16794789
51 Z = -5119051
84
XDOT = 15687
640661 XDOT = 4781
592873
YDOT = -17773
621451 feet/sec YDOT = -5417
399818 meter/sec
ZDOT = -4898
809201 ZDOT = -1493
157044
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 09042
37920708
00010596 00000-0 82463-4 0 9124
2 25544 51
6405 231
1755 0008804 1
8095 358
3097 15
70551080 26162
Satellite: ISS
Catalog Number: 25544
Epoch time: 09042
37920708 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 231
1755 deg
Eccentricity:
0008804
Arg of perigee: 1
8095 deg
Mean anomaly: 358
3097 deg
Mean motion: 15
70551080 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2616
Checksum: 296
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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