Date:
December 17th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 95 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 3468)
---------------------------------------
Vector Time (GMT): 2009/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3050655
13 A = 6717727
68 meter
Y = 4442500
07 meter E =
0018217
Z = 3996553
59 I = 51
97772
XDOT = -3201
894927 Wp = 95
69598
YDOT = -5785
527960 meter/sec RA = 89
03615 deg
ZDOT = 3969
910065 TA = 313
43000
MA = 313
58146
Ha = 188
803 n
mi
Hp = 177
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10008711
04 X = -3119519
86
Y = 14575131
46 feet Y = 4408000
16 meter
Z = 13112052
48 Z = 3981566
86
XDOT = -10504
904615 XDOT = -3156
247383
YDOT = -18981
390946 feet/sec YDOT = -5821
078849 meter/sec
ZDOT = 13024
639322 ZDOT = 3954
465111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13540088
09 X = -4127018
85
Y = -11437816
72 feet Y = -3486246
54 meter
Z = 13052855
52 Z = 3978510
36
XDOT = 19075
008714 XDOT = 5814
062656
YDOT = -7722
815755 feet/sec YDOT = -2353
914242 meter/sec
ZDOT = 12963
384734 ZDOT = 3951
239667
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 09350
55474530
00016717 00000-0 10270-3 0 9007
2 25544 51
6450 89
4929 0007424 87
1594 273
0420 15
76649911 34694
Satellite: ISS
Catalog Number: 25544
Epoch time: 09350
55474530 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 89
4929 deg
Eccentricity:
0007424
Arg of perigee: 87
1594 deg
Mean anomaly: 273
0420 deg
Mean motion: 15
76649911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 325
Coasting Arc #2 (Orbit 3483)
---------------------------------------
Vector Time (GMT): 2009/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2748456
58 A = 6721462
58 meter
Y = 5488352
55 meter E =
0011734
Z = -2744839
81 I = 51
98857
XDOT = -3608
112855 Wp = 76
48484
YDOT = 4392
516765 meter/sec RA = 83
85721 deg
ZDOT = 5191
131984 TA = 252
30861
MA = 252
43675
Ha = 188
753 n
mi
Hp = 177
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9017246
00 X = 2700214
54
Y = 18006406
00 feet Y = 5518818
11 meter
Z = -9005379
94 Z = -2731604
09
XDOT = -11837
640602 XDOT = -3682
180202
YDOT = 14411
144243 feet/sec YDOT = 4351
753764 meter/sec
ZDOT = 17031
272913 ZDOT = 5173
424526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18665288
58 X = -5689179
96
Y = 7621762
42 feet Y = 2323113
19 meter
Z = -8952876
09 Z = -2728836
63
XDOT = -12869
642247 XDOT = -3922
666957
YDOT = -11675
289014 feet/sec YDOT = -3558
628091 meter/sec
ZDOT = 16961
297432 ZDOT = 5169
803457
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 09351
50549591
00016717 00000-0 10270-3 0 9014
2 25544 51
6452 84
5929 0007347 88
8057 271
3949 15
76624935 34841
Satellite: ISS
Catalog Number: 25544
Epoch time: 09351
50549591 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 84
5929 deg
Eccentricity:
0007347
Arg of perigee: 88
8057 deg
Mean anomaly: 271
3949 deg
Mean motion: 15
76624935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3484
Checksum: 349
Coasting Arc #3 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2009/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3316825
81 A = 6714094
35 meter
Y = -3138954
57 meter E =
0019694
Z = -4939474
10 I = 51
95929
XDOT = 3079
222252 Wp = 80
98049
YDOT = 6697
067399 meter/sec RA = 78
76599 deg
ZDOT = -2192
558057 TA = 167
81965
MA = 167
77197
Ha = 188
684 n
mi
Hp = 177
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10881974
45 X = 3375674
66
Y = -10298407
38 feet Y = -3101534
09 meter
Z = -16205623
68 Z = -4923218
51
XDOT = 10102
435210 XDOT = 3014
756642
YDOT = 21972
005901 feet/sec YDOT = 6731
140960 meter/sec
ZDOT = -7193
431947 ZDOT = -2177
754812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9602016
49 X = 2926694
62
Y = 11591145
47 feet Y = 3532981
14 meter
Z = -16141357
67 Z = -4919885
82
XDOT = -21710
567844 XDOT = -6617
381079
YDOT = 8069
378359 feet/sec YDOT = 2459
546524 meter/sec
ZDOT = -7134
698307 ZDOT = -2174
656044
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 09352
51961009
00016717 00000-0 10270-3 0 9029
2 25544 51
6449 79
3651 0007353 93
3030 266
8976 15
76660537 35006
Satellite: ISS
Catalog Number: 25544
Epoch time: 09352
51961009 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 79
3651 deg
Eccentricity:
0007353
Arg of perigee: 93
3030 deg
Mean anomaly: 266
8976 deg
Mean motion: 15
76660537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 319
Coasting Arc #4 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2009/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2628634
65 A = 6724063
64 meter
Y = -6094472
90 meter E =
0020728
Z = 1025633
00 I = 51
98558
XDOT = 4041
233709 Wp = 114
23120
YDOT = -2759
720825 meter/sec RA = 73
60665 deg
ZDOT = -5956
088362 TA = 54
59201
MA = 54
39860
Ha = 188
695 n
mi
Hp = 176
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8624129
42 X = -2565272
13
Y = -19994989
84 feet Y = -6123513
71 meter
Z = 3364937
68 Z = 1013016
24
XDOT = 13258
640778 XDOT = 4100
726505
YDOT = -9054
202182 feet/sec YDOT = -2714
195919 meter/sec
ZDOT = -19540
972315 ZDOT = -5936
311998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20359858
78 X = 6205684
96
Y = -7745050
71 feet Y = -2360691
46 meter
Z = 3314871
41 Z = 1010372
81
XDOT = 7885
645450 XDOT = 2403
544733
YDOT = 12278
008465 feet/sec YDOT = 3742
336980 meter/sec
ZDOT = -19462
757045 ZDOT = -5932
248347
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 09353
53370537
00016717 00000-0 10270-3 0 9033
2 25544 51
6443 74
1372 0007535 96
3994 263
8029 15
76700226 35160
Satellite: ISS
Catalog Number: 25544
Epoch time: 09353
53370537 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 74
1372 deg
Eccentricity:
0007535
Arg of perigee: 96
3994 deg
Mean anomaly: 263
8029 deg
Mean motion: 15
76700226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 317
Coasting Arc #5 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2009/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3786291
02 A = 6712200
63 meter
Y = 1664997
03 meter E =
0009736
Z = 5278167
85 I = 51
93707
XDOT = -2933
244809 Wp = 98
57737
YDOT = -7132
586357 meter/sec RA = 68
48401 deg
ZDOT = 144
164842 TA = 350
05278
MA = 350
07204
Ha = 188
633 n
mi
Hp = 176
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12422214
63 X = -3830268
15
Y = 5462588
69 feet Y = 1622409
98 meter
Z = 17316823
64 Z = 5259667
52
XDOT = -9623
506592 XDOT = -2853
969294
YDOT = -23400
873876 feet/sec YDOT = -7164
944397 meter/sec
ZDOT = 472
981766 ZDOT = 130
106933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5118788
84 X = -1560206
84
Y = -12668024
58 feet Y = -3861213
89 meter
Z = 17243631
48 Z = 5255858
88
XDOT = 22731
383088 XDOT = 6928
525565
YDOT = -8609
844977 feet/sec YDOT = -2624
280749 meter/sec
ZDOT = 417
190515 ZDOT = 127
159669
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 09354
54777922
00016717 00000-0 10270-3 0 9045
2 25544 51
6448 68
9086 0007351 99
7036 260
4963 15
76771457 35320
Satellite: ISS
Catalog Number: 25544
Epoch time: 09354
54777922 = yrday
fracday
Element set: 904
Inclination: 51
6448 deg
RA of node: 68
9086 deg
Eccentricity:
0007351
Arg of perigee: 99
7036 deg
Mean anomaly: 260
4963 deg
Mean motion: 15
76771457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 349
Coasting Arc #6 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2009/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2427192
54 A = 6724105
38 meter
Y = 6214160
29 meter E =
0019394
Z = 788948
61 I = 51
96416
XDOT = -4716
751336 Wp = 70
00183
YDOT = 1066
330942 meter/sec RA = 63
35664 deg
ZDOT = 6000
414223 TA = 298
57337
MA = 298
76840
Ha = 188
598 n
mi
Hp = 176
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7963230
11 X = 2353691
76
Y = 20387665
01 feet Y = 6240891
55 meter
Z = 2588414
06 Z = 800561
95
XDOT = -15474
905959 XDOT = -4757
473459
YDOT = 3498
461095 feet/sec YDOT = 1013
357149 meter/sec
ZDOT = 19686
398368 ZDOT = 5977
401548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20467158
32 X = -6238389
86
Y = 7741098
14 feet Y = 2359486
71 meter
Z = 2634508
57 Z = 802998
21
XDOT = -2776
428961 XDOT = -846
255547
YDOT = -14132
091911 feet/sec YDOT = -4307
461615 meter/sec
ZDOT = 19595
330213 ZDOT = 5972
656649
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 09355
56183805
00016717 00000-0 10270-3 0 9050
2 25544 51
6442 63
6804 0007501 101
6684 258
5323 15
76743498 35482
Satellite: ISS
Catalog Number: 25544
Epoch time: 09355
56183805 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 63
6804 deg
Eccentricity:
0007501
Arg of perigee: 101
6684 deg
Mean anomaly: 258
5323 deg
Mean motion: 15
76743498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 326
Coasting Arc #7 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2009/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4486805
48 A = 6713465
65 meter
Y = -211774
46 meter E =
0020490
Z = -5007862
05 I = 51
91327
XDOT = 2522
910083 Wp = 104
52636
YDOT = 6992
832049 meter/sec RA = 58
19723 deg
ZDOT = 1966
327080 TA = 184
42317
MA = 184
44131
Ha = 188
494 n
mi
Hp = 176
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14720490
43 X = 4513167
32
Y = -694798
09 feet Y = -161452
52 meter
Z = -16429993
60 Z = -4986001
20
XDOT = 8277
264052 XDOT = 2434
975467
YDOT = 22942
362365 feet/sec YDOT = 7020
552882 meter/sec
ZDOT = 6451
204331 ZDOT = 1978
370351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 800039
11 X = 243851
92
Y = 14811188
98 feet Y = 4514450
40 meter
Z = -16343466
31 Z = -4981488
53
XDOT = -21803
590266 XDOT = -6645
734313
YDOT = 8343
149009 feet/sec YDOT = 2542
991818 meter/sec
ZDOT = 6499
013051 ZDOT = 1980
899178
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 09356
51249824
00016717 00000-0 10270-3 0 9061
2 25544 51
6435 58
7784 0007470 104
8013 255
3980 15
76789104 35637
Satellite: ISS
Catalog Number: 25544
Epoch time: 09356
51249824 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 58
7784 deg
Eccentricity:
0007470
Arg of perigee: 104
8013 deg
Mean anomaly: 255
3980 deg
Mean motion: 15
76789104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 332
Coasting Arc #8 (Orbit 3578)
---------------------------------------
Vector Time (GMT): 2009/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1883389
78 A = 6721165
24 meter
Y = -5904284
79 meter E =
0012462
Z = -2602742
62 I = 51
92302
XDOT = 5578
014253 Wp = 115
34879
YDOT = 537
871569 meter/sec RA = 53
09815 deg
ZDOT = -5281
222672 TA = 94
11646
MA = 93
97401
Ha = 188
457 n
mi
Hp = 176
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6179100
33 X = -1804583
40
Y = -19371013
09 feet Y = -5924905
14 meter
Z = -8539181
81 Z = -2611701
15
XDOT = 18300
571697 XDOT = 5597
240325
YDOT = 1764
670501 feet/sec YDOT = 600
356123 meter/sec
ZDOT = -17326
846037 ZDOT = -5254
077941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19216723
54 X = 5857257
33
Y = -6597437
05 feet Y = -2010898
81 meter
Z = -8574754
57 Z = -2613585
19
XDOT = -1798
083794 XDOT = -548
055940
YDOT = 17037
857731 feet/sec YDOT = 5193
139037 meter/sec
ZDOT = -17219
389357 ZDOT = -5248
469876
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 09357
52651927
00016717 00000-0 10270-3 0 9075
2 25544 51
6437 53
5491 0007587 108
2924 251
9067 15
76824333 35794
Satellite: ISS
Catalog Number: 25544
Epoch time: 09357
52651927 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 53
5491 deg
Eccentricity:
0007587
Arg of perigee: 108
2924 deg
Mean anomaly: 251
9067 deg
Mean motion: 15
76824333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 343
Coasting Arc #9 (Orbit 3594)
---------------------------------------
Vector Time (GMT): 2009/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5239243
21 A = 6716902
38 meter
Y = -1058073
51 meter E =
0017428
Z = 4052827
21 I = 51
89023
XDOT = -1713
646250 Wp = 90
80074
YDOT = -6441
290085 meter/sec RA = 47
91210 deg
ZDOT = -3882
931564 TA = 39
03478
MA = 38
90913
Ha = 188
409 n
mi
Hp = 176
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17189118
13 X = -5246710
21
Y = -3471369
80 feet Y = -1116703
88 meter
Z = 13296677
19 Z = 4027356
67
XDOT = -5622
198982 XDOT = -1622
628611
YDOT = -21132
841486 feet/sec YDOT = -6459
943898 meter/sec
ZDOT = -12739
276785 ZDOT = -3891
035876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2752017
42 X = 838814
91
Y = -17395805
03 feet Y = -5302241
37 meter
Z = 13195839
57 Z = 4022091
90
XDOT = 19616
404364 XDOT = 5979
080050
YDOT = -6619
763254 feet/sec YDOT = -2017
703840 meter/sec
ZDOT = -12771
472218 ZDOT = -3892
744732
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 09358
54051985
00016717 00000-0 10270-3 0 9087
2 25544 51
6440 48
3202 0007398 111
3494 248
8461 15
76884740 35956
Satellite: ISS
Catalog Number: 25544
Epoch time: 09358
54051985 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 48
3202 deg
Eccentricity:
0007398
Arg of perigee: 111
3494 deg
Mean anomaly: 248
8461 deg
Mean motion: 15
76884740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 337
Coasting Arc #10 (Orbit 3610)
---------------------------------------
Vector Time (GMT): 2009/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 995444
81 A = 6716790
04 meter
Y = 5256885
75 meter E =
0018218
Z = 4049822
98 I = 51
86868
XDOT = -6416
818403 Wp = 107
62829
YDOT = -1791
276501 meter/sec RA = 42
82322 deg
ZDOT = 3882
807971 TA = 302
48101
MA = 302
65698
Ha = 188
338 n
mi
Hp = 176
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3265895
04 X = 916913
97
Y = 17247000
50 feet Y = 5267578
00 meter
Z = 13286820
80 Z = 4054468
54
XDOT = -21052
553814 XDOT = -6415
173221
YDOT = -5876
891407 feet/sec YDOT = -1863
024260 meter/sec
ZDOT = 12738
871297 ZDOT = 3851
638717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17030665
05 X = -5190946
71
Y = 4194066
74 feet Y = 1278351
54 meter
Z = 13305298
03 Z = 4055454
84
XDOT = 4933
214687 XDOT = 1503
643836
YDOT = -20193
217458 feet/sec YDOT = -6154
892681 meter/sec
ZDOT = 12615
467030 ZDOT = 3845
194351
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 09359
55450457
00016717 00000-0 10270-3 0 9097
2 25544 51
6437 43
0911 0007627 114
7527 245
4432 15
76885817 36116
Satellite: ISS
Catalog Number: 25544
Epoch time: 09359
55450457 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 43
0911 deg
Eccentricity:
0007627
Arg of perigee: 114
7527 deg
Mean anomaly: 245
4432 deg
Mean motion: 15
76885817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3611
Checksum: 327
Coasting Arc #11 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2009/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5885654
60 A = 6721001
23 meter
Y = 1977172
20 meter E =
0010807
Z = -2582888
57 I = 51
86089
XDOT = 437
517212 Wp = 91
34155
YDOT = 5577
967402 meter/sec RA = 37
63398 deg
ZDOT = 5285
502067 TA = 239
42656
MA = 239
53323
Ha = 188
276 n
mi
Hp = 176
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19309890
41 X = 5875655
39
Y = 6486785
45 feet Y = 2042933
40 meter
Z = -8474043
85 Z = -2554319
90
XDOT = 1435
423925 XDOT = 349
434638
YDOT = 18300
417986 feet/sec YDOT = 5582
367000 meter/sec
ZDOT = 17340
886048 ZDOT = 5287
414100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5000231
83 X = -1524070
66
Y = 19795255
58 feet Y = 6033593
90 meter
Z = -8360933
59 Z = -2548412
56
XDOT = -16703
569497 XDOT = -5091
247983
YDOT = 3082
032260 feet/sec YDOT = 939
403433 meter/sec
ZDOT = 17348
541242 ZDOT = 5287
835370
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 09360
50509831
00016717 00000-0 10270-3 0 9107
2 25544 51
6444 38
1888 0007667 117
9066 242
2876 15
76933569 36260
Satellite: ISS
Catalog Number: 25544
Epoch time: 09360
50509831 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 38
1888 deg
Eccentricity:
0007667
Arg of perigee: 117
9066 deg
Mean anomaly: 242
2876 deg
Mean motion: 15
76933569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 341
Coasting Arc #12 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2009/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 344328
09 A = 6712926
99 meter
Y = -4463096
47 meter E =
0019385
Z = -5018932
08 I = 51
80972
XDOT = 6960
198893 Wp = 91
90820
YDOT = 2665
997957 meter/sec RA = 32
52754 deg
ZDOT = -1900
141931 TA = 159
81089
MA = 159
73413
Ha = 188
220 n
mi
Hp = 176
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1129685
32 X = 418590
93
Y = -14642704
95 feet Y = -4458830
20 meter
Z = -16466312
61 Z = -5017079
44
XDOT = 22835
298204 XDOT = 6939
100573
YDOT = 8746
712457 feet/sec YDOT = 2743
713259 meter/sec
ZDOT = -6234
061454 ZDOT = -1866
379887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14693695
26 X = 4478638
31
Y = -140299
10 feet Y = -42763
16 meter
Z = -16459042
62 Z = -5016716
19
XDOT = -6592
941644 XDOT = -2009
528613
YDOT = 22513
949382 feet/sec YDOT = 6862
251772 meter/sec
ZDOT = -6100
387526 ZDOT = -1859
398118
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 09361
51904706
00016717 00000-0 10270-3 0 9110
2 25544 51
6451 32
9592 0007600 121
5026 238
6882 15
76921848 36427
Satellite: ISS
Catalog Number: 25544
Epoch time: 09361
51904706 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 32
9592 deg
Eccentricity:
0007600
Arg of perigee: 121
5026 deg
Mean anomaly: 238
6882 deg
Mean motion: 15
76921848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 311
Coasting Arc #13 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2009/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6158044
12 A = 6723572
12 meter
Y = -2587679
75 meter E =
0020980
Z = 676418
98 I = 51
81909
XDOT = 1284
043212 Wp = 126
38618
YDOT = -4656
999261 meter/sec RA = 27
36021 deg
ZDOT = -6010
007802 TA = 46
24990
MA = 46
07642
Ha = 188
141 n
mi
Hp = 176
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20203556
83 X = -6131936
50
Y = -8489762
95 feet Y = -2656396
75 meter
Z = 2219222
37 Z = 646565
98
XDOT = 4212
740196 XDOT = 1365
218953
YDOT = -15278
868966 feet/sec YDOT = -4642
185623 meter/sec
ZDOT = -19717
873366 ZDOT = -6003
573329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6212998
14 X = 1893721
83
Y = -21027816
95 feet Y = -6409278
61 meter
Z = 2101023
56 Z = 640391
98
XDOT = 14129
553149 XDOT = 4306
687800
YDOT = 2167
094409 feet/sec YDOT = 660
530376 meter/sec
ZDOT = -19692
463008 ZDOT = -6002
262725
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 09362
53297736
00016717 00000-0 10270-3 0 9122
2 25544 51
6444 27
7297 0007644 124
2246 235
9644 15
76967737 36585
Satellite: ISS
Catalog Number: 25544
Epoch time: 09362
53297736 = yrday
fracday
Element set: 912
Inclination: 51
6444 deg
RA of node: 27
7297 deg
Eccentricity:
0007644
Arg of perigee: 124
2246 deg
Mean anomaly: 235
9644 deg
Mean motion: 15
76967737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 351
Coasting Arc #14 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2009/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1931614
21 A = 6711598
33 meter
Y = 3687615
01 meter E =
0009354
Z = 5257086
69 I = 51
75098
XDOT = -7021
526639 Wp = 113
78470
YDOT = -3172
409298 meter/sec RA = 22
21596 deg
ZDOT = -357
825518 TA = 339
58319
MA = 339
62056
Ha = 188
109 n
mi
Hp = 176
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6337316
97 X = -1998244
31
Y = 12098474
43 feet Y = 3665641
16 meter
Z = 17247659
75 Z = 5247541
61
XDOT = -23036
504721 XDOT = -6983
792082
YDOT = -10408
166989 feet/sec YDOT = -3250
717112 meter/sec
ZDOT = -1173
968235 ZDOT = -391
845135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12819327
52 X = -3907331
03
Y = -4847678
20 feet Y = -1477572
31 meter
Z = 17209918
50 Z = 5245583
16
XDOT = 7042
127427 XDOT = 2146
440440
YDOT = -23230
894540 feet/sec YDOT = -7080
776656 meter/sec
ZDOT = -1308
668471 ZDOT = -398
882150
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 09363
54688969
00016717 00000-0 10270-3 0 9137
2 25544 51
6437 22
5003 0007636 127
5710 232
6149 15
77000064 36742
Satellite: ISS
Catalog Number: 25544
Epoch time: 09363
54688969 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 22
5003 deg
Eccentricity:
0007636
Arg of perigee: 127
5710 deg
Mean anomaly: 232
6149 deg
Mean motion: 15
77000064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 313
Coasting Arc #15 (Orbit 3689)
---------------------------------------
Vector Time (GMT): 2009/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5922744
55 A = 6722819
10 meter
Y = 2892403
22 meter E =
0017933
Z = 1300744
95 I = 51
76088
XDOT = -3184
501247 Wp = 82
84016
YDOT = 3854
529436 meter/sec RA = 17
08230 deg
ZDOT = 5862
621644 TA = 291
43033
MA = 291
62152
Ha = 187
938 n
mi
Hp = 176
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19431576
60 X = 5883642
22
Y = 9489511
87 feet Y = 2958415
98 meter
Z = 4267535
92 Z = 1329423
15
XDOT = -10447
838736 XDOT = -3255
846115
YDOT = 12646
093951 feet/sec YDOT = 3818
518518 meter/sec
ZDOT = 19234
322978 ZDOT = 5846
978733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6592272
66 X = -2009324
71
Y = 20571748
36 feet Y = 6270268
90 meter
Z = 4381093
27 Z = 1335357
23
XDOT = -12537
017095 XDOT = -3821
282811
YDOT = -8145
794539 feet/sec YDOT = -2482
838175 meter/sec
ZDOT = 19172
439260 ZDOT = 5843
759487
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 09364
56078431
00016717 00000-0 10270-3 0 9148
2 25544 51
6439 17
2710 0007549 131
1784 229
0033 15
77021489 36909
Satellite: ISS
Catalog Number: 25544
Epoch time: 09364
56078431 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 17
2710 deg
Eccentricity:
0007549
Arg of perigee: 131
1784 deg
Mean anomaly: 229
0033 deg
Mean motion: 15
77021489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3690
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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