Date:
January 30th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9526 06 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
035/08:30:34
844 -2
4 4
6 4
6
N/A -2
8 -0
0 196
4
000/00:01:05
688 -2
8 0
0 191
3
Coasting Arc #1 (Orbit 2398)
---------------------------------------
Vector Time (GMT): 2009/028/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4553471
82 A = 6730966
57 meter
Y = 144966
60 meter E =
0003121
Z = 4954372
75 I = 51
34488
XDOT = -2405
630986 Wp = 350
62136
YDOT = 7028
815073 meter/sec RA = 301
38255 deg
ZDOT = 2008
516687 TA = 79
87195
MA = 79
83675
Ha = 195
463 n
mi
Hp = 190
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14939211
99 X = 4527445
54
Y = 475612
22 feet Y = 195740
58 meter
Z = 16254503
78 Z = 4976429
72
XDOT = -7892
490111 XDOT = -2493
806320
YDOT = 23060
416905 feet/sec YDOT = 7001
420866 meter/sec
ZDOT = 6589
621675 ZDOT = 1996
616372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10093439
21 X = 3076480
27
Y = 10896286
02 feet Y = 3321187
98 meter
Z = 16340397
51 Z = 4980553
16
XDOT = -21185
103215 XDOT = -6457
219460
YDOT = 9826
671575 feet/sec YDOT = 2995
169496 meter/sec
ZDOT = 6543
757021 ZDOT = 1994
537140
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 09028
57197910
00010596 00000-0 82463-4 0 9008
2 25544 51
6428 301
7247 0008353 320
1051 39
9496 15
70652307 23992
Satellite: ISS
Catalog Number: 25544
Epoch time: 09028
57197910 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 301
7247 deg
Eccentricity:
0008353
Arg of perigee: 320
1051 deg
Mean anomaly: 39
9496 deg
Mean motion: 15
70652307 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2399
Checksum: 310
Coasting Arc #2 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2009/029/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 570485
17 A = 6738401
69 meter
Y = -6122442
44 meter E =
0009386
Z = -2742175
74 I = 51
35603
XDOT = 5452
647780 Wp = 354
28198
YDOT = -1786
724387 meter/sec RA = 296
21272 deg
ZDOT = 5131
275026 TA = 334
28692
MA = 334
33355
Ha = 195
687 n
mi
Hp = 190
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1871670
51 X = 652225
62
Y = -20086753
41 feet Y = -6115605
91 meter
Z = -8996639
57 Z = -2739205
84
XDOT = 17889
264370 XDOT = 5447
295739
YDOT = -5861
956649 feet/sec YDOT = -1725
779628 meter/sec
ZDOT = 16834
891816 ZDOT = 5157
750385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15421345
91 X = 4700426
23
Y = -13013965
22 feet Y = -3966656
60 meter
Z = -8985495
86 Z = -2738779
14
XDOT = 15868
522274 XDOT = 4836
725589
YDOT = 7126
643986 feet/sec YDOT = 2172
201087 meter/sec
ZDOT = 16937
856762 ZDOT = 5162
658741
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 09029
52635394
00010596 00000-0 82463-4 0 9018
2 25544 51
6431 296
8480 0008425 323
8345 36
2246 15
70674931 24143
Satellite: ISS
Catalog Number: 25544
Epoch time: 09029
52635394 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 296
8480 deg
Eccentricity:
0008425
Arg of perigee: 323
8345 deg
Mean anomaly: 36
2246 deg
Mean motion: 15
70674931 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2414
Checksum: 311
Coasting Arc #3 (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 = -4527657
24 A = 6735158
34 meter
Y = 3190623
85 meter E =
0009072
Z = -3840358
75 I = 51
33338
XDOT = -1037
962089 Wp = 9
90170
YDOT = -6418
481492 meter/sec RA = 291
13039 deg
ZDOT = -4101
476071 TA = 216
96354
MA = 217
02608
Ha = 195
852 n
mi
Hp = 189
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14854518
51 X = -4544343
40
Y = 10467926
00 feet Y = 3139899
62 meter
Z = -12599602
19 Z = -3862394
26
XDOT = -3405
387430 XDOT = -946
188562
YDOT = -21058
010145 feet/sec YDOT = -6429
575494 meter/sec
ZDOT = -13456
286321 ZDOT = -4106
295422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17932957
74 X = -5465965
52
Y = -2545473
20 feet Y = -775860
23 meter
Z = -12685178
88 Z = -3866442
52
XDOT = 11860
298954 XDOT = 3615
019121
YDOT = -16282
500446 feet/sec YDOT = -4962
906136 meter/sec
ZDOT = -13475
499738 ZDOT = -4107
332320
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
54433960
00010596 00000-0 82463-4 0 9028
2 25544 51
6430 291
6462 0008541 327
1357 32
9272 15
70686983 24304
Satellite: ISS
Catalog Number: 25544
Epoch time: 09030
54433960 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 291
6462 deg
Eccentricity:
0008541
Arg of perigee: 327
1357 deg
Mean anomaly: 32
9272 deg
Mean motion: 15
70686983 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2430
Checksum: 302
Coasting Arc #4 (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 = 2229549
57 A = 6733469
99 meter
Y = 4690949
00 meter E =
0011791
Z = 4287368
64 I = 51
31830
XDOT = -4396
034207 Wp = 25
71211
YDOT = 5273
458502 meter/sec RA = 285
94707 deg
ZDOT = -3469
753787 TA = 99
65154
MA = 99
51831
Ha = 195
953 n
mi
Hp = 189
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7314795
18 X = 2156101
93
Y = 15390252
64 feet Y = 4715470
49 meter
Z = 14066170
09 Z = 4298021
21
XDOT = -14422
684407 XDOT = -4437
820967
YDOT = 17301
373039 feet/sec YDOT = 5224
065826 meter/sec
ZDOT = -11383
706651 ZDOT = -3491
210962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5035561
33 X = -1534839
09
Y = 16242883
88 feet Y = 4950831
01 meter
Z = 14107979
70 Z = 4300112
21
XDOT = -21083
563122 XDOT = -6426
270039
YDOT = 3463
382248 feet/sec YDOT = 1055
638909 meter/sec
ZDOT = -11466
881059 ZDOT = -3495
105347
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
56231115
00010596 00000-0 82463-4 0 9030
2 25544 51
6426 286
4438 0008625 331
4286 28
6401 15
70739152 24466
Satellite: ISS
Catalog Number: 25544
Epoch time: 09031
56231115 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 286
4438 deg
Eccentricity:
0008625
Arg of perigee: 331
4286 deg
Mean anomaly: 28
6401 deg
Mean motion: 15
70739152 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2446
Checksum: 296
Coasting Arc #5 (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 = 2817576
08 A = 6739583
95 meter
Y = -5735901
69 meter E =
0015828
Z = 2107817
27 I = 51
33168
XDOT = 3746
132043 Wp = 37
01952
YDOT = 3867
436710 meter/sec RA = 280
85671 deg
ZDOT = 5507
729632 TA = 346
63265
MA = 346
67453
Ha = 196
084 n
mi
Hp = 189
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9244016
02 X = 2871267
18
Y = -18818575
09 feet Y = -5704093
72 meter
Z = 6915410
98 Z = 2121635
30
XDOT = 12290
459460 XDOT = 3675
852026
YDOT = 12688
440650 feet/sec YDOT = 3908
935155 meter/sec
ZDOT = 18069
979106 ZDOT = 5525
757462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19350634
51 X = 5898073
40
Y = -8025098
33 feet Y = -2446049
97 meter
Z = 6968805
55 Z = 2124091
93
XDOT = 160
739751 XDOT = 48
993476
YDOT = 16165
723905 feet/sec YDOT = 4927
312646 meter/sec
ZDOT = 18140
450276 ZDOT = 5529
209244
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
58027025
00010596 00000-0 82463-4 0 9047
2 25544 51
6425 281
2408 0008663 335
2365 24
8380 15
70717223 24624
Satellite: ISS
Catalog Number: 25544
Epoch time: 09032
58027025 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 281
2408 deg
Eccentricity:
0008663
Arg of perigee: 335
2365 deg
Mean anomaly: 24
8380 deg
Mean motion: 15
70717223 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2462
Checksum: 291
Coasting Arc #6 (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 = -3958759
12 A = 6729864
30 meter
Y = -1811367
67 meter E =
0012139
Z = -5140290
65 I = 51
29484
XDOT = 1750
564262 Wp = 62
18395
YDOT = -7380
083904 meter/sec RA = 275
69267 deg
ZDOT = 1260
307153 TA = 219
89637
MA = 219
98565
Ha = 196
126 n
mi
Hp = 189
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12988054
86 X = -3913239
49
Y = -5942807
32 feet Y = -1855382
18 meter
Z = -16864470
65 Z = -5159411
62
XDOT = 5743
321068 XDOT = 1826
837182
YDOT = -24212
873700 feet/sec YDOT = -7360
081644 meter/sec
ZDOT = 4134
865989 ZDOT = 1268
996411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5958872
73 X = -1816264
41
Y = -12883212
63 feet Y = -3926803
21 meter
Z = -16939054
46 Z = -5163023
80
XDOT = 19115
757914 XDOT = 5826
483012
YDOT = -14288
268674 feet/sec YDOT = -4355
064292 meter/sec
ZDOT = 4168
171689 ZDOT = 1270
458731
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
53459259
00010596 00000-0 82463-4 0 9052
2 25544 51
6422 276
3633 0008678 338
0647 22
0142 15
70765435 24776
Satellite: ISS
Catalog Number: 25544
Epoch time: 09033
53459259 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 276
3633 deg
Eccentricity:
0008678
Arg of perigee: 338
0647 deg
Mean anomaly: 22
0142 deg
Mean motion: 15
70765435 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2477
Checksum: 318
Coasting Arc #7 (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 = -127357
86 A = 6741478
85 meter
Y = 6739569
40 meter E =
0005808
Z = -75327
01 I = 51
33196
XDOT = -4802
842638 Wp = 94
96604
YDOT = -153
403062 meter/sec RA = 270
57022 deg
ZDOT = -6003
395970 TA = 85
85397
MA = 85
78760
Ha = 196
333 n
mi
Hp = 188
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -417840
75 X = -202345
45
Y = 22111448
17 feet Y = 6737725
94 meter
Z = -247135
85 Z = -76127
53
XDOT = -15757
357736 XDOT = -4771
607157
YDOT = -503
290885 feet/sec YDOT = -206
936306 meter/sec
ZDOT = -19696
181003 ZDOT = -6026
652103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14368657
22 X = -4379566
72
Y = 16811636
22 feet Y = 5124186
72 meter
Z = -249768
30 Z = -76129
38
XDOT = -10535
314169 XDOT = -3211
163759
YDOT = -9279
121389 feet/sec YDOT = -2828
276199 meter/sec
ZDOT = -19786
752592 ZDOT = -6031
002190
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
55252531
00010596 00000-0 82463-4 0 9060
2 25544 51
6422 271
1612 0008531 341
5857 18
4994 15
70733685 24930
Satellite: ISS
Catalog Number: 25544
Epoch time: 09034
55252531 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 271
1612 deg
Eccentricity:
0008531
Arg of perigee: 341
5857 deg
Mean anomaly: 18
4994 deg
Mean motion: 15
70733685 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2493
Checksum: 310
Coasting Arc #8 (Orbit 2505)
---------------------------------------
Vector Time (GMT): 2009/035/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2413360
01 A = 6738717
51 meter
Y = 5277485
75 meter E =
0005696
Z = -3431674
25 I = 51
31463
XDOT = -3956
866855 Wp = 5
43426
YDOT = -4770
082958 meter/sec RA = 266
31173 deg
ZDOT = -4548
115054 TA = 215
26470
MA = 215
30239
Ha = 196
438 n
mi
Hp = 191
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7917847
79 X = -2455524
10
Y = 17314585
79 feet Y = 5250262
63 meter
Z = -11258773
80 Z = -3443500
29
XDOT = -12981
846637 XDOT = -3881
139254
YDOT = -15649
878472 feet/sec YDOT = -4813
907227 meter/sec
ZDOT = -14921
637315 ZDOT = -4567
153662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15992884
69 X = -4874631
25
Y = -10280287
30 feet Y = -3133431
57 meter
Z = -11304446
68 Z = -3445595
35
XDOT = 16604
789531 XDOT = 5061
139849
YDOT = -9323
869775 feet/sec YDOT = -2841
915507 meter/sec
ZDOT = -14996
124139 ZDOT = -4570
818638
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
37959474
00010596 00000-0 82463-4 0 9072
2 25544 51
6415 266
9336 0007046 320
8407 39
2244 15
69907506 25065
Satellite: ISS
Catalog Number: 25544
Epoch time: 09035
37959474 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 266
9336 deg
Eccentricity:
0007046
Arg of perigee: 320
8407 deg
Mean anomaly: 39
2244 deg
Mean motion: 15
69907506 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2506
Checksum: 327
Coasting Arc #9 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2009/036/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4189802
08 A = 6734109
70 meter
Y = 2367223
27 meter E =
0009730
Z = 4712421
85 I = 51
30185
XDOT = -1038
645589 Wp = 15
22488
YDOT = 7144
361017 meter/sec RA = 261
13818 deg
ZDOT = -2654
918561 TA = 101
07670
MA = 100
96727
Ha = 196
516 n
mi
Hp = 191
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13746069
82 X = 4140128
30
Y = 7766480
54 feet Y = 2413797
95 meter
Z = 15460701
59 Z = 4732655
10
XDOT = -3407
629885 XDOT = -1105
560924
YDOT = 23439
504649 feet/sec YDOT = 7132
372349 meter/sec
ZDOT = -8710
362732 ZDOT = -2660
126178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9450223
19 X = -2880428
03
Y = 12550604
95 feet Y = 3825424
39 meter
Z = 15539676
51 Z = 4736493
40
XDOT = -21901
957269 XDOT = -6675
716575
YDOT = -5639
765290 feet/sec YDOT = -1719
000460 meter/sec
ZDOT = -8730
123754 ZDOT = -2660
941720
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
39808027
00010596 00000-0 82463-4 0 9083
2 25544 51
6409 261
7353 0007102 324
4570 35
6117 15
69919331 25220
Satellite: ISS
Catalog Number: 25544
Epoch time: 09036
39808027 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 261
7353 deg
Eccentricity:
0007102
Arg of perigee: 324
4570 deg
Mean anomaly: 35
6117 deg
Mean motion: 15
69919331 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2522
Checksum: 303
Coasting Arc #10 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2009/037/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -760427
36 A = 6743330
33 meter
Y = -6604222
46 meter E =
0015717
Z = 1068846
34 I = 51
33866
XDOT = 4948
696392 Wp = 29
45789
YDOT = 386
601882 meter/sec RA = 256
04122 deg
ZDOT = 5886
303623 TA = 342
27171
MA = 342
32649
Ha = 196
701 n
mi
Hp = 191
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2494840
42 X = -691713
48
Y = -21667396
53 feet Y = -6612341
89 meter
Z = 3506713
71 Z = 1065318
63
XDOT = 16235
880550 XDOT = 4915
411614
YDOT = 1268
378878 feet/sec YDOT = 441
754497 meter/sec
ZDOT = 19312
019762 ZDOT = 5910
263020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21812621
56 X = 6648487
05
Y = -97154
84 feet Y = -29612
80 meter
Z = 3492483
86 Z = 1064509
08
XDOT = -3055
613683 XDOT = -931
351051
YDOT = 14293
499662 feet/sec YDOT = 4356
658697 meter/sec
ZDOT = 19405
373253 ZDOT = 5914
757767
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
41655351
00010596 00000-0 82463-4 0 9098
2 25544 51
6410 256
5361 0007178 328
6110 31
4622 15
69919518 25381
Satellite: ISS
Catalog Number: 25544
Epoch time: 09037
41655351 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 256
5361 deg
Eccentricity:
0007178
Arg of perigee: 328
6110 deg
Mean anomaly: 31
4622 deg
Mean motion: 15
69919518 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2538
Checksum: 309
Coasting Arc #11 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2009/038/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3874779
24 A = 6731644
51 meter
Y = 1672216
37 meter E =
0013511
Z = -5254793
33 I = 51
30844
XDOT = -2719
288264 Wp = 59
23235
YDOT = -7183
463381 meter/sec RA = 250
90635 deg
ZDOT = -274
539884 TA = 208
10810
MA = 208
18111
Ha = 196
757 n
mi
Hp = 190
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12712530
32 X = -3867664
17
Y = 5486274
17 feet Y = 1628926
46 meter
Z = -17240135
61 Z = -5273599
07
XDOT = -8921
549421 XDOT = -2637
425859
YDOT = -23567
793246 feet/sec YDOT = -7213
414307 meter/sec
ZDOT = -900
721403 ZDOT = -287
551434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4279305
83 X = -1304332
42
Y = -13071656
11 feet Y = -3984240
78 meter
Z = -17313268
18 Z = -5277084
14
XDOT = 23346
789154 XDOT = 7116
101334
YDOT = -6355
070820 feet/sec YDOT = -1937
025586 meter/sec
ZDOT = -951
952094 ZDOT = -290
154998
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
37135896
00010596 00000-0 82463-4 0 9103
2 25544 51
6413 251
6624 0007185 332
0763 28
0012 15
69969356 25530
Satellite: ISS
Catalog Number: 25544
Epoch time: 09038
37135896 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 251
6624 deg
Eccentricity:
0007185
Arg of perigee: 332
0763 deg
Mean anomaly: 28
0012 deg
Mean motion: 15
69969356 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2553
Checksum: 313
Coasting Arc #12 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2009/039/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3758162
76 A = 6742695
19 meter
Y = 5385279
23 meter E =
0009470
Z = 1521026
91 I = 51
35571
XDOT = -3276
689779 Wp = 90
31182
YDOT = 3919
167307 meter/sec RA = 245
76271 deg
ZDOT = -5749
120702 TA = 72
89587
MA = 72
79218
Ha = 196
940 n
mi
Hp = 190
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12329930
32 X = 3690275
74
Y = 17668238
95 feet Y = 5426925
56 meter
Z = 4990245
75 Z = 1539118
76
XDOT = -10750
294550 XDOT = -3292
343772
YDOT = 12858
160455 feet/sec YDOT = 3882
438149 meter/sec
ZDOT = -18861
944561 ZDOT = -5765
076205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18558892
31 X = -5656750
37
Y = 10910943
67 feet Y = 3325655
63 meter
Z = 5061148
74 Z = 1542638
14
XDOT = -11209
156068 XDOT = -3416
550770
YDOT = -10241
864900 feet/sec YDOT = -3121
720422 meter/sec
ZDOT = -18923
802529 ZDOT = -5767
975011
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
38980712
00010596 00000-0 82463-4 0 9111
2 25544 51
6407 246
4633 0007139 335
5883 24
4939 15
69950510 25692
Satellite: ISS
Catalog Number: 25544
Epoch time: 09039
38980712 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 246
4633 deg
Eccentricity:
0007139
Arg of perigee: 335
5883 deg
Mean anomaly: 24
4939 deg
Mean motion: 15
69950510 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2569
Checksum: 333
Coasting Arc #13 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2009/040/08:31:07
688
Vector Time (MET): N/A
Weight (LBS) : 640039
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436998
95 A = 6734807
21 meter
Y = -4793182
87 meter E =
0006517
Z = 4500995
30 I = 51
34282
XDOT = 5393
673946 Wp = 58
80798
YDOT = 4531
709864 meter/sec RA = 240
67370 deg
ZDOT = 3103
907404 TA =
10585
MA =
10572
Ha = 197
006 n
mi
Hp = 190
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4714563
48 X = 1468626
04
Y = -15725665
57 feet Y = -4776936
69 meter
Z = 14767044
94 Z = 4508052
80
XDOT = 17695
780662 XDOT = 5327
521044
YDOT = 14867
814516 feet/sec YDOT = 4591
655168 meter/sec
ZDOT = 10183
423241 ZDOT = 3129
948314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15422433
81 X = 4700757
83
Y = 5556132
72 feet Y = 1693509
25 meter
Z = 14794161
25 Z = 4509260
35
XDOT = -15485
159630 XDOT = -4719
876655
YDOT = 15596
805471 feet/sec YDOT = 4753
906308 meter/sec
ZDOT = 10285
246772 ZDOT = 3134
943216
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
40824084
00010596 00000-0 82463-4 0 9126
2 25544 51
6408 241
2636 0007311 339
8208 20
2663 15
69986611 25856
Satellite: ISS
Catalog Number: 25544
Epoch time: 09040
40824084 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 241
2636 deg
Eccentricity:
0007311
Arg of perigee: 339
8208 deg
Mean anomaly: 20
2663 deg
Mean motion: 15
69986611 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2585
Checksum: 302
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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