Date:
December 9th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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 3335)
---------------------------------------
Vector Time (GMT): 2009/342/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5115937
44 A = 6724738
73 meter
Y = -4178798
01 meter E =
0012120
Z = -1259794
31 I = 51
90861
XDOT = 2196
632121 Wp = 103
62804
YDOT = 4448
962849 meter/sec RA = 132
15988 deg
ZDOT = -5886
860591 TA = 90
14232
MA = 90
00344
Ha = 189
040 n
mi
Hp = 177
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16784571
66 X = 5168405
14
Y = -13709967
21 feet Y = -4121295
12 meter
Z = -4133183
42 Z = -1234813
84
XDOT = 7206
798296 XDOT = 2175
317201
YDOT = 14596
334805 feet/sec YDOT = 4473
408144 meter/sec
ZDOT = -19313
847084 ZDOT = -5876
240752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18679927
41 X = -5693641
87
Y = -11025014
93 feet Y = -3360424
55 meter
Z = -4034551
99 Z = -1229731
45
XDOT = 10356
760774 XDOT = 3156
740684
YDOT = -10556
570771 feet/sec YDOT = -3217
642771 meter/sec
ZDOT = -19271
684351 ZDOT = -5874
009390
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 09342
12393879
00016717 00000-0 10270-3 0 9007
2 25544 51
6431 132
9429 0007665 54
2272 305
9604 15
76382488 33362
Satellite: ISS
Catalog Number: 25544
Epoch time: 09342
12393879 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 132
9429 deg
Eccentricity:
0007665
Arg of perigee: 54
2272 deg
Mean anomaly: 305
9604 deg
Mean motion: 15
76382488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3336
Checksum: 323
Coasting Arc #2 (Orbit 3351)
---------------------------------------
Vector Time (GMT): 2009/343/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1504683
62 A = 6714990
36 meter
Y = -4356832
21 meter E =
0014346
Z = 4875444
49 I = 51
89527
XDOT = 5741
092221 Wp = 57
98305
YDOT = -4594
477282 meter/sec RA = 126
99523 deg
ZDOT = -2321
512373 TA = 54
57910
MA = 54
44522
Ha = 189
087 n
mi
Hp = 177
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4936626
05 X = -1479537
14
Y = -14294068
93 feet Y = -4373518
18 meter
Z = 15995552
78 Z = 4868195
48
XDOT = 18835
604399 XDOT = 5803
319353
YDOT = -15073
744362 feet/sec YDOT = -4529
928920 meter/sec
ZDOT = -7616
510410 ZDOT = -2293
471068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11501576
23 X = -3505680
43
Y = 9865385
41 feet Y = 3006969
47 meter
Z = 15966725
00 Z = 4866657
78
XDOT = -20168
872765 XDOT = -6147
472419
YDOT = -11300
176640 feet/sec YDOT = -3444
293840 meter/sec
ZDOT = -7505
779575 ZDOT = -2287
761614
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 09343
13822837
00016717 00000-0 10270-3 0 9011
2 25544 51
6430 127
7165 0007693 57
7443 302
4466 15
76402611 33526
Satellite: ISS
Catalog Number: 25544
Epoch time: 09343
13822837 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 127
7165 deg
Eccentricity:
0007693
Arg of perigee: 57
7443 deg
Mean anomaly: 302
4466 deg
Mean motion: 15
76402611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3352
Checksum: 301
Coasting Arc #3 (Orbit 3367)
---------------------------------------
Vector Time (GMT): 2009/344/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4853591
30 A = 6722109
39 meter
Y = 3740620
70 meter E =
0021141
Z = 2737488
73 I = 51
93634
XDOT = -1333
560865 Wp = 72
63002
YDOT = -5547
550253 meter/sec RA = 121
90211 deg
ZDOT = 5189
583796 TA = 318
57233
MA = 318
73244
Ha = 189
134 n
mi
Hp = 177
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15923855
99 X = -4908357
24
Y = 12272377
64 feet Y = 3686038
59 meter
Z = 8981262
22 Z = 2713776
91
XDOT = -4375
199689 XDOT = -1296
638438
YDOT = -18200
624189 feet/sec YDOT = -5562
256817 meter/sec
ZDOT = 17026
193558 ZDOT = 5183
194597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17402631
39 X = 5304322
05
Y = 10149003
40 feet Y = 3093416
24 meter
Z = 8887612
97 Z = 2708944
43
XDOT = -14416
567559 XDOT = -4394
169792
YDOT = 9755
849377 feet/sec YDOT = 2973
582890 meter/sec
ZDOT = 17000
727707 ZDOT = 5181
821805
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 09344
15250409
00016717 00000-0 10270-3 0 9025
2 25544 51
6429 122
4891 0007725 61
1461 299
0478 15
76417079 33682
Satellite: ISS
Catalog Number: 25544
Epoch time: 09344
15250409 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 122
4891 deg
Eccentricity:
0007725
Arg of perigee: 61
1461 deg
Mean anomaly: 299
0478 deg
Mean motion: 15
76417079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 321
Coasting Arc #4 (Orbit 3382)
---------------------------------------
Vector Time (GMT): 2009/345/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 878314
62 A = 6718099
15 meter
Y = 5299802
17 meter E =
0013962
Z = -4045267
41 I = 51
93857
XDOT = -5378
419539 Wp = 86
21684
YDOT = 3869
067337 meter/sec RA = 116
72029 deg
ZDOT = 3913
598891 TA = 223
96448
MA = 224
07563
Ha = 189
048 n
mi
Hp = 177
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2881609
66 X = 838637
52
Y = 17387802
41 feet Y = 5309402
48 meter
Z = -13271874
71 Z = -4041096
45
XDOT = -17645
733395 XDOT = -5440
296243
YDOT = 12693
790475 feet/sec YDOT = 3808
576395 meter/sec
ZDOT = 12839
891374 ZDOT = 3887
320118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14814916
35 X = 4515586
50
Y = -9570787
45 feet Y = -2917176
01 meter
Z = -13255198
46 Z = -4040184
49
XDOT = 17951
462908 XDOT = 5471
605894
YDOT = 10205
069318 feet/sec YDOT = 3110
505128 meter/sec
ZDOT = 12736
082175 ZDOT = 3881
957847
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 09345
10337437
00016717 00000-0 10270-3 0 9039
2 25544 51
6433 117
5883 0007730 64
4255 295
7708 15
76450912 33835
Satellite: ISS
Catalog Number: 25544
Epoch time: 09345
10337437 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 117
5883 deg
Eccentricity:
0007730
Arg of perigee: 64
4255 deg
Mean anomaly: 295
7708 deg
Mean motion: 15
76450912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3383
Checksum: 318
Coasting Arc #5 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2009/346/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4541255
68 A = 6718166
20 meter
Y = -2904229
93 meter E =
0014910
Z = -4025229
11 I = 51
95217
XDOT = 712
751505 Wp = 69
77446
YDOT = 6567
194991 meter/sec RA = 111
63885 deg
ZDOT = -3940
819386 TA = 159
66984
MA = 159
61042
Ha = 189
043 n
mi
Hp = 177
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14899132
81 X = 4592947
95
Y = -9528313
41 feet Y = -2853157
50 meter
Z = -13206132
27 Z = -4003042
02
XDOT = 2338
423572 XDOT = 658
407133
YDOT = 21545
915324 feet/sec YDOT = 6574
861930 meter/sec
ZDOT = -12929
197461 ZDOT = -3937
488139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14828667
31 X = -4519777
80
Y = -9756607
60 feet Y = -2973814
00 meter
Z = -13118463
26 Z = -3998507
60
XDOT = 17953
022222 XDOT = 5472
081173
YDOT = -9949
435664 feet/sec YDOT = -3032
587990 meter/sec
ZDOT = -12915
811258 ZDOT = -3936
739272
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 09346
11762281
00016717 00000-0 10270-3 0 9041
2 25544 51
6440 112
3607 0007784 67
7782 292
4207 15
76481802 33997
Satellite: ISS
Catalog Number: 25544
Epoch time: 09346
11762281 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 112
3607 deg
Eccentricity:
0007784
Arg of perigee: 67
7782 deg
Mean anomaly: 292
4207 deg
Mean motion: 15
76481802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 322
Coasting Arc #6 (Orbit 3414)
---------------------------------------
Vector Time (GMT): 2009/347/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -437870
92 A = 6721850
95 meter
Y = -6109648
37 meter E =
0020754
Z = 2750513
06 I = 51
97432
XDOT = 5024
941286 Wp = 90
23958
YDOT = -2707
716564 meter/sec RA = 106
45853 deg
ZDOT = -5181
395440 TA = 58
42696
MA = 58
22451
Ha = 189
079 n
mi
Hp = 177
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1436584
40 X = -382880
95
Y = -20044778
13 feet Y = -6114237
77 meter
Z = 9023992
98 Z = 2748518
69
XDOT = 16486
027841 XDOT = 5080
016703
YDOT = -8883
584529 feet/sec YDOT = -2651
216144 meter/sec
ZDOT = -16999
328870 ZDOT = -5156
850383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17506880
21 X = -5336097
09
Y = 9874799
39 feet Y = 3009838
85 meter
Z = 9015921
30 Z = 2748052
81
XDOT = -14375
318220 XDOT = -4381
596994
YDOT = -9953
919272 feet/sec YDOT = -3033
954594 meter/sec
ZDOT = -16902
313921 ZDOT = -5151
825283
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 09347
13185813
00016717 00000-0 10270-3 0 9055
2 25544 51
6438 107
1333 0007767 71
7618 288
4391 15
76475396 34155
Satellite: ISS
Catalog Number: 25544
Epoch time: 09347
13185813 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 107
1333 deg
Eccentricity:
0007767
Arg of perigee: 71
7618 deg
Mean anomaly: 288
4391 deg
Mean motion: 15
76475396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3415
Checksum: 334
Coasting Arc #7 (Orbit 3430)
---------------------------------------
Vector Time (GMT): 2009/348/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4250117
42 A = 6714684
94 meter
Y = 1749741
39 meter E =
0013229
Z = 4884430
92 I = 51
95864
XDOT = -364
844155 Wp = 96
70167
YDOT = -7350
870495 meter/sec RA = 101
36863 deg
ZDOT = 2309
024010 TA = 330
92247
MA = 330
99608
Ha = 189
145 n
mi
Hp = 177
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13943954
79 X = -4293095
50
Y = 5740621
36 feet Y = 1701973
09 meter
Z = 16025035
82 Z = 4863679
37
XDOT = -1196
995260 XDOT = -293
835312
YDOT = -24117
029184 feet/sec YDOT = -7354
553687 meter/sec
ZDOT = 7575
538092 ZDOT = 2307
423033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11342049
22 X = 3457056
60
Y = 10068238
38 feet Y = 3068799
06 meter
Z = 15942988
35 Z = 4859422
85
XDOT = -20364
714605 XDOT = -6207
165012
YDOT = 10920
232628 feet/sec YDOT = 3328
486905 meter/sec
ZDOT = 7568
999725 ZDOT = 2307
031116
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 09348
14607837
00016717 00000-0 10270-3 0 9063
2 25544 51
6445 101
9058 0007734 75
0176 285
1844 15
76517293 34317
Satellite: ISS
Catalog Number: 25544
Epoch time: 09348
14607837 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 101
9058 deg
Eccentricity:
0007734
Arg of perigee: 75
0176 deg
Mean anomaly: 285
1844 deg
Mean motion: 15
76517293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3431
Checksum: 324
Coasting Arc #8 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2009/349/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 233824
09 A = 6724312
65 meter
Y = 6606182
76 meter E =
0015912
Z = -1211759
26 I = 51
99695
XDOT = -4781
221857 Wp = 55
79634
YDOT = 1241
884101 meter/sec RA = 96
20800 deg
ZDOT = 5911
260507 TA = 290
97578
MA = 291
14596
Ha = 188
979 n
mi
Hp = 177
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 767139
41 X = 165821
80
Y = 21673827
95 feet Y = 6608417
48 meter
Z = -3975588
11 Z = -1210787
49
XDOT = -15686
423415 XDOT = -4823
469647
YDOT = 4074
422903 feet/sec YDOT = 1188
180533 meter/sec
ZDOT = 19393
899300 ZDOT = 5887
930615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18925479
41 X = 5768486
12
Y = -10592519
54 feet Y = -3228599
96 meter
Z = -3971571
53 Z = -1210535
00
XDOT = 10062
604414 XDOT = 3067
081825
YDOT = 10819
834689 feet/sec YDOT = 3297
885613 meter/sec
ZDOT = 19301
626505 ZDOT = 5883
135759
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 09349
09689829
00016717 00000-0 10270-3 0 9070
2 25544 51
6454 97
0052 0007699 77
8242 282
3785 15
76539855 34467
Satellite: ISS
Catalog Number: 25544
Epoch time: 09349
09689829 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 97
0052 deg
Eccentricity:
0007699
Arg of perigee: 77
8242 deg
Mean anomaly: 282
3785 deg
Mean motion: 15
76539855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 371
Coasting Arc #9 (Orbit 3461)
---------------------------------------
Vector Time (GMT): 2009/350/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4144674
66 A = 6712842
90 meter
Y = -355805
66 meter E =
0022658
Z = -5287883
15 I = 51
96104
XDOT = 159
566580 Wp = 84
89887
YDOT = 7676
726515 meter/sec RA = 91
09214 deg
ZDOT = -390
933128 TA = 181
39632
MA = 181
40266
Ha = 188
929 n
mi
Hp = 177
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13598013
96 X = 4174033
07
Y = -1167341
41 feet Y = -309292
47 meter
Z = -17348698
00 Z = -5267676
90
XDOT = 523
512400 XDOT = 75
611316
YDOT = 25186
110614 feet/sec YDOT = 7678
041527 meter/sec
ZDOT = -1282
589003 ZDOT = -390
360647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7489257
78 X = -2282725
77
Y = -11530272
59 feet Y = -3514427
09 meter
Z = -17268752
81 Z = -5263515
86
XDOT = 21119
373913 XDOT = 6437
185169
YDOT = -11797
749605 feet/sec YDOT = -3595
954080 meter/sec
ZDOT = -1280
136145 ZDOT = -390
185497
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
11109258
00016717 00000-0 10270-3 0 9089
2 25544 51
6459 91
7776 0007687 80
9118 279
2917 15
76569347 34629
Satellite: ISS
Catalog Number: 25544
Epoch time: 09350
11109258 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 91
7776 deg
Eccentricity:
0007687
Arg of perigee: 80
9118 deg
Mean anomaly: 279
2917 deg
Mean motion: 15
76569347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3462
Checksum: 352
Coasting Arc #10 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2009/351/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -46299
34 A = 6724839
94 meter
Y = -6698395
85 meter E =
0016760
Z = -544414
92 I = 52
00083
XDOT = 4761
608707 Wp = 117
67506
YDOT = 445
925515 meter/sec RA = 85
96348 deg
ZDOT = -6039
466020 TA = 68
22522
MA = 68
04696
Ha = 188
975 n
mi
Hp = 177
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -151900
71 X = 31251
42
Y = -21976364
34 feet Y = -6698479
90 meter
Z = -1786138
18 Z = -544452
54
XDOT = 15622
075812 XDOT = 4785
607123
YDOT = 1463
010221 feet/sec YDOT = 499
307784 meter/sec
ZDOT = -19814
521063 ZDOT = -6016
275680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19130144
40 X = -5830868
01
Y = 10817585
31 feet Y = 3297200
00 meter
Z = -1786442
36 Z = -544507
63
XDOT = -5591
739225 XDOT = -1704
362116
YDOT = -13065
530925 feet/sec YDOT = -3982
373826 meter/sec
ZDOT = -19722
740560 ZDOT = -6011
491323
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
12527466
00016717 00000-0 10270-3 0 9097
2 25544 51
6461 86
5502 0007617 85
7575 274
4459 15
76535181 34788
Satellite: ISS
Catalog Number: 25544
Epoch time: 09351
12527466 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 86
5502 deg
Eccentricity:
0007617
Arg of perigee: 85
7575 deg
Mean anomaly: 274
4459 deg
Mean motion: 15
76535181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 339
Coasting Arc #11 (Orbit 3493)
---------------------------------------
Vector Time (GMT): 2009/352/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4217581
96 A = 6713431
52 meter
Y = -1107159
19 meter E =
0011966
Z = 5095478
22 I = 51
96007
XDOT = 44
848423 Wp = 74
29261
YDOT = -7546
219870 meter/sec RA = 80
81398 deg
ZDOT = -1596
295229 TA = 30
97711
MA = 30
90659
Ha = 188
927 n
mi
Hp = 176
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13837211
15 X = -4229640
94
Y = -3632412
05 feet Y = -1154390
89 meter
Z = 16717448
24 Z = 5074959
76
XDOT = 147
140496 XDOT = 136
982751
YDOT = -24757
939206 feet/sec YDOT = -7545
202953 meter/sec
ZDOT = -5237
189070 ZDOT = -1595
854719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3847201
15 X = 1172626
91
Y = 13877000
05 feet Y = 4229709
62 meter
Z = 16636220
08 Z = 5070719
88
XDOT = -20495
899274 XDOT = -6247
150099
YDOT = 11983
515808 feet/sec YDOT = 3652
575618 meter/sec
ZDOT = -5235
613414 ZDOT = -1595
814969
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
13944027
00016717 00000-0 10270-3 0 9107
2 25544 51
6463 81
3226 0007528 87
5088 272
6938 15
76634256 34949
Satellite: ISS
Catalog Number: 25544
Epoch time: 09352
13944027 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 81
3226 deg
Eccentricity:
0007528
Arg of perigee: 87
5088 deg
Mean anomaly: 272
6938 deg
Mean motion: 15
76634256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3494
Checksum: 330
Coasting Arc #12 (Orbit 3509)
---------------------------------------
Vector Time (GMT): 2009/353/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -161777
58 A = 6722651
63 meter
Y = 6340640
12 meter E =
0021350
Z = 2201927
15 I = 51
98443
XDOT = -4975
541236 Wp = 77
84199
YDOT = -2057
366235 meter/sec RA = 75
71501 deg
ZDOT = 5518
646332 TA = 306
75756
MA = 306
95338
Ha = 188
850 n
mi
Hp = 177
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -530766
34 X = -243364
23
Y = 20802625
07 feet Y = 6338374
54 meter
Z = 7224170
43 Z = 2200943
96
XDOT = -16323
954187 XDOT = -4978
974097
YDOT = -6749
889221 feet/sec YDOT = -2113
025647 meter/sec
ZDOT = 18105
795051 ZDOT = 5494
466608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18110649
66 X = 5520126
02
Y = -10251318
43 feet Y = -3124601
86 meter
Z = 7220415
52 Z = 2200782
65
XDOT = 1956
411348 XDOT = 596
314179
YDOT = 16234
379183 feet/sec YDOT = 4948
238775 meter/sec
ZDOT = 18010
050748 ZDOT = 5489
463468
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
15359601
00016717 00000-0 10270-3 0 9119
2 25544 51
6458 76
0946 0007560 90
6590 269
5441 15
76610831 35108
Satellite: ISS
Catalog Number: 25544
Epoch time: 09353
15359601 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 76
0946 deg
Eccentricity:
0007560
Arg of perigee: 90
6590 deg
Mean anomaly: 269
5441 deg
Mean motion: 15
76610831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3510
Checksum: 311
Coasting Arc #13 (Orbit 3524)
---------------------------------------
Vector Time (GMT): 2009/354/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4491722
55 A = 6716441
85 meter
Y = 2436252
87 meter E =
0016320
Z = -4374593
63 I = 51
95461
XDOT = -407
388522 Wp = 103
16071
YDOT = 6878
200342 meter/sec RA = 70
53844 deg
ZDOT = 3419
220465 TA = 201
16957
MA = 201
23719
Ha = 188
764 n
mi
Hp = 177
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14736622
52 X = 4485396
97
Y = 7992955
60 feet Y = 2486447
14 meter
Z = -14352341
31 Z = -4352788
02
XDOT = -1336
576517 XDOT = -500
881354
YDOT = 22566
274089 feet/sec YDOT = 6873
121510 meter/sec
ZDOT = 11217
914913 ZDOT = 3417
015149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1097544
90 X = -334531
69
Y = -16802447
25 feet Y = -5121385
92 meter
Z = -14265982
10 Z = -4348271
34
XDOT = 18641
222021 XDOT = 5681
844472
YDOT = -10715
280967 feet/sec YDOT = -3266
017639 meter/sec
ZDOT = 11209
330313 ZDOT = 3416
603879
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
10435337
00016717 00000-0 10270-3 0 9127
2 25544 51
6453 71
1930 0007478 94
3650 265
8369 15
76641642 35256
Satellite: ISS
Catalog Number: 25544
Epoch time: 09354
10435337 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 71
1930 deg
Eccentricity:
0007478
Arg of perigee: 94
3650 deg
Mean anomaly: 265
8369 deg
Mean motion: 15
76641642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3525
Checksum: 317
Coasting Arc #14 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2009/355/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 630726
77 A = 6718736
12 meter
Y = -5582658
66 meter E =
0013012
Z = -3696015
72 I = 51
95045
XDOT = 5321
515280 Wp = 89
27461
YDOT = 3468
514522 meter/sec RA = 65
45519 deg
ZDOT = -4343
807675 TA = 134
98616
MA = 134
88062
Ha = 188
728 n
mi
Hp = 177
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2069313
56 X = 711060
64
Y = -18315809
26 feet Y = -5575155
93 meter
Z = -12126035
83 Z = -3692757
14
XDOT = 17459
039631 XDOT = 5303
435553
YDOT = 11379
640819 feet/sec YDOT = 3527
922226 meter/sec
ZDOT = -14251
337515 ZDOT = -4317
999429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16518199
88 X = -5034747
32
Y = 8198162
52 feet Y = 2498799
94 meter
Z = -12113252
09 Z = -3692119
24
XDOT = 564
967106 XDOT = 172
201974
YDOT = -19705
195510 feet/sec YDOT = -6006
143592 meter/sec
ZDOT = -14149
112041 ZDOT = -4312
649350
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
11848249
00016717 00000-0 10270-3 0 9130
2 25544 51
6444 65
9648 0007403 98
3374 261
8630 15
76638921 35419
Satellite: ISS
Catalog Number: 25544
Epoch time: 09355
11848249 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 65
9648 deg
Eccentricity:
0007403
Arg of perigee: 98
3374 deg
Mean anomaly: 261
8630 deg
Mean motion: 15
76638921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 333
Coasting Arc #15 (Orbit 3556)
---------------------------------------
Vector Time (GMT): 2009/356/02:16:09
706
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4802874
03 A = 6720340
90 meter
Y = -3514763
20 meter E =
0020512
Z = 3100926
62 I = 51
94318
XDOT = 1090
107229 Wp = 96
89920
YDOT = -5845
117354 meter/sec RA = 60
27003 deg
ZDOT = -4911
695828 TA = 47
16846
MA = 46
99626
Ha = 188
669 n
mi
Hp = 176
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15757460
73 X = -4778278
05
Y = -11531375
32 feet Y = -3568334
53 meter
Z = 10173643
75 Z = 3077653
76
XDOT = 3576
467288 XDOT = 1179
247373
YDOT = -19176
894205 feet/sec YDOT = -5832
428272 meter/sec
ZDOT = -16114
487626 ZDOT = -4906
184123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -699292
19 X = -213144
26
Y = 19561403
43 feet Y = 5962315
77 meter
Z = 10081453
20 Z = 3072826
94
XDOT = -16518
725852 XDOT = -5034
907640
YDOT = 7746
076803 feet/sec YDOT = 2361
004210 meter/sec
ZDOT = -16092
787502 ZDOT = -4905
081630
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
13259763
00016717 00000-0 10270-3 0 9141
2 25544 51
6449 60
7362 0007381 100
5742 259
6255 15
76714765 35576
Satellite: ISS
Catalog Number: 25544
Epoch time: 09356
13259763 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 60
7362 deg
Eccentricity:
0007381
Arg of perigee: 100
5742 deg
Mean anomaly: 259
6255 deg
Mean motion: 15
76714765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 331
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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