Date:
September 29th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2144)
---------------------------------------
Vector Time (GMT): 2009/266/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1671985
12 A = 6721516
39 meter
Y = -4497806
04 meter E =
0014204
Z = 4694184
75 I = 51
73623
XDOT = 7200
992341 Wp = 93
51142
YDOT = -199
770955 meter/sec RA = 160
88747 deg
ZDOT = -2750
032802 TA = 23
53632
MA = 23
47139
Ha = 192
510 n
mi
Hp = 180
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5485515
49 X = 1699352
28
Y = -14756581
49 feet Y = -4478955
76 meter
Z = 15400868
59 Z = 4702373
97
XDOT = 23625
302956 XDOT = 7216
050367
YDOT = -655
416519 feet/sec YDOT = -119
161108 meter/sec
ZDOT = -9022
417330 ZDOT = -2715
013310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1212403
13 X = -369540
47
Y = 15664988
88 feet Y = 4774688
61 meter
Z = 15432839
42 Z = 4703929
46
XDOT = -21479
461256 XDOT = -6546
939791
YDOT = 7110
534187 feet/sec YDOT = 2167
290820 meter/sec
ZDOT = -8884
469813 ZDOT = -2707
986399
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 09266
58162077
00020000 00000-0 20000-3 0 9008
2 25544 51
6405 161
7028 0008594 121
0139 239
1870 15
74352076 21453
Satellite: ISS
Catalog Number: 25544
Epoch time: 09266
58162077 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 161
7028 deg
Eccentricity:
0008594
Arg of perigee: 121
0139 deg
Mean anomaly: 239
1870 deg
Mean motion: 15
74352076 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2145
Checksum: 283
Coasting Arc #2 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2009/267/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6210886
39 A = 6728651
21 meter
Y = 639689
60 meter E =
0020541
Z = 2492736
30 I = 51
78723
XDOT = 1606
874735 Wp = 93
89994
YDOT = -5323
447032 meter/sec RA = 155
80021 deg
ZDOT = 5330
915349 TA = 294
25771
MA = 294
47217
Ha = 192
591 n
mi
Hp = 180
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20376923
87 X = -6229687
30
Y = 2098719
17 feet Y = 570130
74 meter
Z = 8178268
68 Z = 2462517
79
XDOT = 5271
898737 XDOT = 1640
386096
YDOT = -17465
377402 feet/sec YDOT = -5305
290547 meter/sec
ZDOT = 17489
879754 ZDOT = 5338
803129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18967291
21 X = 5781230
36
Y = -7861175
84 feet Y = -2396086
39 meter
Z = 8059249
69 Z = 2456459
31
XDOT = -523
781801 XDOT = -159
648693
YDOT = 16830
990902 feet/sec YDOT = 5130
086027 meter/sec
ZDOT = 17520
617994 ZDOT = 5340
284365
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 09267
59724921
00020000 00000-0 20000-3 0 9013
2 25544 51
6402 156
4841 0008596 124
6616 235
5358 15
74320689 21619
Satellite: ISS
Catalog Number: 25544
Epoch time: 09267
59724921 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 156
4841 deg
Eccentricity:
0008596
Arg of perigee: 124
6616 deg
Mean anomaly: 235
5358 deg
Mean motion: 15
74320689 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2161
Checksum: 304
Coasting Arc #3 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2009/268/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1139870
96 A = 6721976
60 meter
Y = 4790870
82 meter E =
0018711
Z = -4593740
23 I = 51
79192
XDOT = -6972
013469 Wp = 118
85400
YDOT = 1215
758155 meter/sec RA = 150
62844 deg
ZDOT = 2998
270439 TA = 180
90910
MA = 180
91251
Ha = 192
386 n
mi
Hp = 180
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3739734
13 X = -1171042
85
Y = 15718080
12 feet Y = 4777949
76 meter
Z = -15071326
21 Z = -4599353
55
XDOT = -22874
059938 XDOT = -6999
655282
YDOT = 3988
707856 feet/sec YDOT = 1137
638485 meter/sec
ZDOT = 9836
845273 ZDOT = 2964
332968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1280298
61 X = -390235
02
Y = -16085595
74 feet Y = -4902889
58 meter
Z = -15093143
24 Z = -4600390
06
XDOT = 19472
870924 XDOT = 5935
331058
YDOT = -10653
396029 feet/sec YDOT = -3247
155110 meter/sec
ZDOT = 9703
194465 ZDOT = 2957
533673
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 09268
54938491
00020000 00000-0 20000-3 0 9029
2 25544 51
6399 151
5914 0008495 129
0630 231
1291 15
74361360 21769
Satellite: ISS
Catalog Number: 25544
Epoch time: 09268
54938491 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 151
5914 deg
Eccentricity:
0008495
Arg of perigee: 129
0630 deg
Mean anomaly: 231
1291 deg
Mean motion: 15
74361360 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2176
Checksum: 300
Coasting Arc #4 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2009/269/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5958471
80 A = 6727937
46 meter
Y = -1456646
52 meter E =
0013208
Z = -2760795
46 I = 51
83692
XDOT = -1009
574271 Wp = 130
02419
YDOT = 5617
053758 meter/sec RA = 145
54796 deg
ZDOT = -5167
064385 TA = 81
44266
MA = 81
29301
Ha = 192
389 n
mi
Hp = 180
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19548792
00 X = 5987728
94
Y = -4779024
02 feet Y = -1389851
85 meter
Z = -9057727
90 Z = -2731777
97
XDOT = -3312
251546 XDOT = -1047
209311
YDOT = 18428
654063 feet/sec YDOT = 5605
553584 meter/sec
ZDOT = -16952
310975 ZDOT = -5172
060438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17050116
32 X = -5196875
46
Y = 10786321
32 feet Y = 3287670
74 meter
Z = -8943465
76 Z = -2725968
36
XDOT = -2051
033668 XDOT = -625
155062
YDOT = -17246
639879 feet/sec YDOT = -5256
775835 meter/sec
ZDOT = -16971
648800 ZDOT = -5172
958554
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 09269
56498277
00020000 00000-0 20000-3 0 9036
2 25544 51
6396 146
3730 0008452 133
8493 226
3370 15
74352459 21928
Satellite: ISS
Catalog Number: 25544
Epoch time: 09269
56498277 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 146
3730 deg
Eccentricity:
0008452
Arg of perigee: 133
8493 deg
Mean anomaly: 226
3370 deg
Mean motion: 15
74352459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2192
Checksum: 316
Coasting Arc #5 (Orbit 2207)
---------------------------------------
Vector Time (GMT): 2009/270/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 590872
62 A = 6722344
67 meter
Y = -5008826
50 meter E =
0014392
Z = 4430773
83 I = 51
84337
XDOT = 6636
789136 Wp = 101
09083
YDOT = -2135
749901 meter/sec RA = 140
37670 deg
ZDOT = -3293
199171 TA = 21
83876
MA = 21
77747
Ha = 192
101 n
mi
Hp = 180
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1938558
47 X = 625314
31
Y = -16433157
80 feet Y = -5002026
31 meter
Z = 14536659
55 Z = 4433728
10
XDOT = 21774
242571 XDOT = 6676
176010
YDOT = -7007
053482 feet/sec YDOT = -2061
313288 meter/sec
ZDOT = -10804
459221 ZDOT = -3260
861827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3766578
84 X = 1148053
23
Y = 16102483
18 feet Y = 4908036
87 meter
Z = 14547992
11 Z = 4434227
99
XDOT = -17046
426253 XDOT = -5195
750722
YDOT = 13652
280143 feet/sec YDOT = 4161
214988 meter/sec
ZDOT = -10677
142879 ZDOT = -3254
393149
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 09270
58056371
00020000 00000-0 20000-3 0 9046
2 25544 51
6399 141
1540 0008279 137
1268 223
0542 15
74439937 22087
Satellite: ISS
Catalog Number: 25544
Epoch time: 09270
58056371 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 141
1540 deg
Eccentricity:
0008279
Arg of perigee: 137
1268 deg
Mean anomaly: 223
0542 deg
Mean motion: 15
74439937 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2208
Checksum: 295
Coasting Arc #6 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2009/271/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5592249
31 A = 6727164
84 meter
Y = 2237199
14 meter E =
0019011
Z = 2986387
28 I = 51
88047
XDOT = 342
571873 Wp = 104
80058
YDOT = -5853
107729 meter/sec RA = 135
30091 deg
ZDOT = 4995
206337 TA = 289
57652
MA = 289
78167
Ha = 192
085 n
mi
Hp = 180
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18347274
63 X = -5631357
78
Y = 7339892
19 feet Y = 2174444
78 meter
Z = 9797858
52 Z = 2959124
99
XDOT = 1123
923467 XDOT = 383
731019
YDOT = -19203
109347 feet/sec YDOT = -5849
046540 meter/sec
ZDOT = 16388
472235 ZDOT = 4996
970782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14647794
27 X = 4464647
69
Y = -13342791
45 feet Y = -4066882
83 meter
Z = 9690540
48 Z = 2953676
74
XDOT = 4816
743753 XDOT = 1468
143496
YDOT = 17269
959372 feet/sec YDOT = 5263
883617 meter/sec
ZDOT = 16395
065115 ZDOT = 4997
215847
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 09271
59613165
00020000 00000-0 20000-3 0 9059
2 25544 51
6388 135
9347 0008274 141
4482 218
7274 15
74431293 22240
Satellite: ISS
Catalog Number: 25544
Epoch time: 09271
59613165 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 135
9347 deg
Eccentricity:
0008274
Arg of perigee: 141
4482 deg
Mean anomaly: 218
7274 deg
Mean motion: 15
74431293 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2224
Checksum: 301
Coasting Arc #7 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2009/272/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -8324
27 A = 6722986
41 meter
Y = 5206984
77 meter E =
0016106
Z = -4269830
30 I = 51
88632
XDOT = -6140
968979 Wp = 127
81496
YDOT = 2926
798895 meter/sec RA = 130
12941 deg
ZDOT = 3580
636347 TA = 178
48580
MA = 178
48092
Ha = 191
953 n
mi
Hp = 180
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -27310
59 X = -45806
94
Y = 17083283
37 feet Y = 5206681
85 meter
Z = -14008629
58 Z = -4269962
10
XDOT = -20147
536019 XDOT = -6190
634663
YDOT = 9602
358580 feet/sec YDOT = 2857
849485 meter/sec
ZDOT = 11747
494578 ZDOT = 3550
682640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6331759
46 X = -1929920
28
Y = -15866397
27 feet Y = -4836077
89 meter
Z = -14008828
60 Z = -4269890
96
XDOT = 14111
939920 XDOT = 4301
319288
YDOT = -15901
168496 feet/sec YDOT = -4846
676158 meter/sec
ZDOT = 11629
601476 ZDOT = 3544
702530
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 09272
54821205
00020000 00000-0 20000-3 0 9062
2 25544 51
6379 131
0409 0008335 144
9968 215
1745 15
74451056 22390
Satellite: ISS
Catalog Number: 25544
Epoch time: 09272
54821205 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 131
0409 deg
Eccentricity:
0008335
Arg of perigee: 144
9968 deg
Mean anomaly: 215
1745 deg
Mean motion: 15
74451056 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2239
Checksum: 294
Coasting Arc #8 (Orbit 2254)
---------------------------------------
Vector Time (GMT): 2009/273/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5136812
00 A = 6726242
13 meter
Y = -2842573
70 meter E =
0011705
Z = -3281898
07 I = 51
91488
XDOT = 315
420875 Wp = 130
63380
YDOT = 6043
126909 meter/sec RA = 125
05903 deg
ZDOT = -4758
932212 TA = 87
67763
MA = 87
54361
Ha = 191
909 n
mi
Hp = 181
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16853057
76 X = 5184159
31
Y = -9326029
20 feet Y = -2784866
37 meter
Z = -10767382
11 Z = -3256828
10
XDOT = 1034
845389 XDOT = 270
940271
YDOT = 19826
531855 feet/sec YDOT = 6046
405053 meter/sec
ZDOT = -15613
294660 ZDOT = -4757
508411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12043585
97 X = -3670885
00
Y = 15101892
69 feet Y = 4603056
89 meter
Z = -10668728
52 Z = -3251828
45
XDOT = -7544
388595 XDOT = -2299
529644
YDOT = -16999
184686 feet/sec YDOT = -5181
351492 meter/sec
ZDOT = -15607
311931 ZDOT = -4757
108677
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 09273
56374926
00020000 00000-0 20000-3 0 9079
2 25544 51
6372 125
8222 0008273 148
8344 211
3312 15
74467698 22554
Satellite: ISS
Catalog Number: 25544
Epoch time: 09273
56374926 = yrday
fracday
Element set: 907
Inclination: 51
6372 deg
RA of node: 125
8222 deg
Eccentricity:
0008273
Arg of perigee: 148
8344 deg
Mean anomaly: 211
3312 deg
Mean motion: 15
74467698 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2255
Checksum: 305
Coasting Arc #9 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2009/274/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -589563
17 A = 6723618
99 meter
Y = -5328856
88 meter E =
0014969
Z = 4041794
48 I = 51
92289
XDOT = 5594
337574 Wp = 109
55026
YDOT = -3588
503194 meter/sec RA = 119
88815 deg
ZDOT = -3908
466706 TA = 20
56718
MA = 20
50698
Ha = 191
710 n
mi
Hp = 181
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1934262
37 X = -549565
61
Y = -17483126
25 feet Y = -5335225
70 meter
Z = 13260480
58 Z = 4039028
02
XDOT = 18354
125898 XDOT = 5653
035821
YDOT = -11773
304441 feet/sec YDOT = -3525
616185 meter/sec
ZDOT = -12823
053496 ZDOT = -3881
146296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8827751
95 X = 2690698
79
Y = 15223979
68 feet Y = 4640269
01 meter
Z = 13249251
22 Z = 4038371
77
XDOT = -11081
375514 XDOT = -3377
603257
YDOT = 17511
059275 feet/sec YDOT = 5337
370867 meter/sec
ZDOT = -12715
568046 ZDOT = -3875
705141
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 09274
57926975
00020000 00000-0 20000-3 0 9089
2 25544 51
6373 120
6023 0008198 153
6020 206
5563 15
74507670 22715
Satellite: ISS
Catalog Number: 25544
Epoch time: 09274
57926975 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 120
6023 deg
Eccentricity:
0008198
Arg of perigee: 153
6020 deg
Mean anomaly: 206
5563 deg
Mean motion: 15
74507670 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2271
Checksum: 296
Coasting Arc #10 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2009/275/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4612573
57 A = 6725298
89 meter
Y = 3378253
59 meter E =
0017458
Z = 3535966
62 I = 51
94118
XDOT = -1038
101559 Wp = 118
02885
YDOT = -6159
482202 meter/sec RA = 114
81976 deg
ZDOT = 4505
772725 TA = 283
88639
MA = 284
08054
Ha = 191
617 n
mi
Hp = 181
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15133115
38 X = -4667184
26
Y = 11083509
15 feet Y = 3326368
10 meter
Z = 11600940
36 Z = 3513425
47
XDOT = -3405
845011 XDOT = -991
036504
YDOT = -20208
274941 feet/sec YDOT = -6170
827242 meter/sec
ZDOT = 14782
718914 ZDOT = 4500
844531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9227082
58 X = 2812414
77
Y = -16394071
29 feet Y = -4996912
93 meter
Z = 11512278
10 Z = 3508942
36
XDOT = 10371
042192 XDOT = 3161
093660
YDOT = 16261
576046 feet/sec YDOT = 4956
528379 meter/sec
ZDOT = 14762
921697 ZDOT = 4499
738533
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 09275
59477508
00020000 00000-0 20000-3 0 9096
2 25544 51
6360 115
3821 0008289 157
7302 202
4223 15
74537717 22877
Satellite: ISS
Catalog Number: 25544
Epoch time: 09275
59477508 = yrday
fracday
Element set: 909
Inclination: 51
6360 deg
RA of node: 115
3821 deg
Eccentricity:
0008289
Arg of perigee: 157
7302 deg
Mean anomaly: 202
4223 deg
Mean motion: 15
74537717 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2287
Checksum: 305
Coasting Arc #11 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2009/276/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1225953
37 A = 6724381
06 meter
Y = 5419159
44 meter E =
0012926
Z = -3803141
77 I = 51
94919
XDOT = -4964
424312 Wp = 136
95023
YDOT = 4084
307813 meter/sec RA = 109
64872 deg
ZDOT = 4218
646360 TA = 177
21803
MA = 177
21083
Ha = 191
526 n
mi
Hp = 181
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4022156
74 X = 1183739
57
Y = 17779394
50 feet Y = 5432632
35 meter
Z = -12477499
25 Z = -3797289
09
XDOT = -16287
481339 XDOT = -5030
220555
YDOT = 13399
960017 feet/sec YDOT = 4028
425250 meter/sec
ZDOT = 13840
703282 ZDOT = 4194
368528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11353928
03 X = -3460677
26
Y = -14281320
53 feet Y = -4352946
50 meter
Z = -12454107
89 Z = -3796012
08
XDOT = 7958
032274 XDOT = 2425
608237
YDOT = -18315
849221 feet/sec YDOT = -5582
670842 meter/sec
ZDOT = 13745
230208 ZDOT = 4189
546167
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 09276
54679764
00020000 00000-0 20000-3 0 9102
2 25544 51
6355 110
4875 0008384 160
1913 199
9578 15
74541432 23028
Satellite: ISS
Catalog Number: 25544
Epoch time: 09276
54679764 = yrday
fracday
Element set: 910
Inclination: 51
6355 deg
RA of node: 110
4875 deg
Eccentricity:
0008384
Arg of perigee: 160
1913 deg
Mean anomaly: 199
9578 deg
Mean motion: 15
74541432 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2302
Checksum: 312
Coasting Arc #12 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2009/277/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4075376
03 A = 6724174
80 meter
Y = -3722220
11 meter E =
0010572
Z = -3842822
60 I = 51
95773
XDOT = 1758
151057 Wp = 126
59353
YDOT = 6222
591213 meter/sec RA = 104
58280 deg
ZDOT = -4176
787089 TA = 99
91883
MA = 99
79948
Ha = 191
430 n
mi
Hp = 181
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13370656
28 X = 4135363
80
Y = -12212008
22 feet Y = -3676311
80 meter
Z = -12607685
69 Z = -3822877
92
XDOT = 5768
212128 XDOT = 1708
728818
YDOT = 20415
325501 feet/sec YDOT = 6241
975163 meter/sec
ZDOT = -13703
369713 ZDOT = -4168
366443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6582158
30 X = -2006241
85
Y = 16927905
47 feet Y = 5159625
59 meter
Z = -12529267
38 Z = -3818920
70
XDOT = -13108
643776 XDOT = -3995
514623
YDOT = -15180
585620 feet/sec YDOT = -4627
042497 meter/sec
ZDOT = -13669
816570 ZDOT = -4166
560091
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 09277
56227115
00020000 00000-0 20000-3 0 9115
2 25544 51
6355 105
2678 0008280 163
2194 196
9245 15
74581509 23185
Satellite: ISS
Catalog Number: 25544
Epoch time: 09277
56227115 = yrday
fracday
Element set: 911
Inclination: 51
6355 deg
RA of node: 105
2678 deg
Eccentricity:
0008280
Arg of perigee: 163
2194 deg
Mean anomaly: 196
9245 deg
Mean motion: 15
74581509 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2318
Checksum: 302
Coasting Arc #13 (Orbit 2333)
---------------------------------------
Vector Time (GMT): 2009/278/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1869427
43 A = 6725245
29 meter
Y = -5422762
53 meter E =
0016028
Z = 3491618
14 I = 51
96734
XDOT = 4351
469564 Wp = 118
97684
YDOT = -4441
100743 meter/sec RA = 99
41312 deg
ZDOT = -4559
584710 TA = 19
71262
MA = 19
65074
Ha = 191
329 n
mi
Hp = 181
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6133292
09 X = -1825612
30
Y = -17791215
64 feet Y = -5443422
32 meter
Z = 11455440
09 Z = 3482643
07
XDOT = 14276
474949 XDOT = 4422
957517
YDOT = -14570
540494 feet/sec YDOT = -4392
040683 meter/sec
ZDOT = -14959
267420 ZDOT = -4538
270745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13711422
34 X = 4179241
53
Y = 12921214
83 feet Y = 3938386
28 meter
Z = 11419756
50 Z = 3480741
78
XDOT = -5074
924253 XDOT = -1546
836912
YDOT = 18555
503934 feet/sec YDOT = 5655
717599 meter/sec
ZDOT = -14875
481574 ZDOT = -4534
046784
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 09278
57772785
00020000 00000-0 20000-3 0 9126
2 25544 51
6352 100
0471 0008324 168
2758 191
8601 15
74580371 23340
Satellite: ISS
Catalog Number: 25544
Epoch time: 09278
57772785 = yrday
fracday
Element set: 912
Inclination: 51
6352 deg
RA of node: 100
0471 deg
Eccentricity:
0008324
Arg of perigee: 168
2758 deg
Mean anomaly: 191
8601 deg
Mean motion: 15
74580371 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2334
Checksum: 298
Coasting Arc #14 (Orbit 2349)
---------------------------------------
Vector Time (GMT): 2009/279/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3524596
29 A = 6723096
25 meter
Y = 3987045
70 meter E =
0015739
Z = 4106318
67 I = 51
96457
XDOT = -2527
562690 Wp = 133
33410
YDOT = -6190
402112 meter/sec RA = 94
34637 deg
ZDOT = 3821
432461 TA = 277
52762
MA = 277
70640
Ha = 191
131 n
mi
Hp = 181
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11563636
11 X = -3588866
46
Y = 13080858
60 feet Y = 3947272
45 meter
Z = 13472174
10 Z = 4089039
39
XDOT = -8292
528510 XDOT = -2476
717023
YDOT = -20309
718214 feet/sec YDOT = -6218
382316 meter/sec
ZDOT = 12537
508075 ZDOT = 3809
277053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3997769
64 X = 1218520
19
Y = -17049037
55 feet Y = -5196546
64 meter
Z = 13404259
52 Z = 4085618
30
XDOT = 15792
652168 XDOT = 4813
600381
YDOT = 13573
427803 feet/sec YDOT = 4137
180794 meter/sec
ZDOT = 12489
255092 ZDOT = 3806
724952
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 09279
59316702
00020000 00000-0 20000-3 0 9133
2 25544 51
6355 94
8266 0008368 172
1573 187
9722 15
74641034 23504
Satellite: ISS
Catalog Number: 25544
Epoch time: 09279
59316702 = yrday
fracday
Element set: 913
Inclination: 51
6355 deg
RA of node: 94
8266 deg
Eccentricity:
0008368
Arg of perigee: 172
1573 deg
Mean anomaly: 187
9722 deg
Mean motion: 15
74641034 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2350
Checksum: 309
Coasting Arc #15 (Orbit 2364)
---------------------------------------
Vector Time (GMT): 2009/280/12:55:40
959
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2546003
50 A = 6726042
22 meter
Y = 5373192
96 meter E =
0009046
Z = -3157241
05 I = 51
97703
XDOT = -3740
531078 Wp = 144
62198
YDOT = 4633
034411 meter/sec RA = 89
17894 deg
ZDOT = 4868
122114 TA = 178
84169
MA = 178
83959
Ha = 191
000 n
mi
Hp = 181
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8353029
86 X = 2501068
02
Y = 17628585
81 feet Y = 5401412
54 meter
Z = -10358402
41 Z = -3144981
53
XDOT = -12272
083589 XDOT = -3815
709558
YDOT = 15200
244129 feet/sec YDOT = 4590
785371 meter/sec
ZDOT = 15971
529244 ZDOT = 4849
767392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15994959
85 X = -4875263
76
Y = -11211873
25 feet Y = -3417378
97 meter
Z = -10309791
64 Z = -3142424
49
XDOT = 2473
580742 XDOT = 753
947410
YDOT = -18149
909036 feet/sec YDOT = -5532
092274 meter/sec
ZDOT = 15899
395478 ZDOT = 4846
135742
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 09280
54512722
00020000 00000-0 20000-3 0 9141
2 25544 51
6369 89
9328 0008375 174
5743 185
5513 15
74647268 23659
Satellite: ISS
Catalog Number: 25544
Epoch time: 09280
54512722 = yrday
fracday
Element set: 914
Inclination: 51
6369 deg
RA of node: 89
9328 deg
Eccentricity:
0008375
Arg of perigee: 174
5743 deg
Mean anomaly: 185
5513 deg
Mean motion: 15
74647268 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2365
Checksum: 322
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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