Date:
October 11th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 2690 98 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 ET - UTC (sec) : 65 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 2897)
---------------------------------------
Vector Time (GMT): 2007/283/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3743116
13 A = 6727356
84 meter
Y = 5475413
47 meter E =
0011106
Z = -1104696
14 I = 51
41370
XDOT = -4568
863741 Wp = 129
25573
YDOT = 1945
048215 meter/sec RA = 228
00570 deg
ZDOT = -5886
690251 TA = 62
87728
MA = 62
76406
Ha = 188
784 n
mi
Hp = 180
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12280564
74 X = 3686977
56
Y = 17963954
97 feet Y = 5516957
14 meter
Z = -3624331
17 Z = -1086648
51
XDOT = -14989
710437 XDOT = -4561
676941
YDOT = 6381
391781 feet/sec YDOT = 1893
996318 meter/sec
ZDOT = -19313
288226 ZDOT = -5908
868927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20102251
76 X = -6127166
33
Y = -8361379
02 feet Y = -2548548
33 meter
Z = -3555072
44 Z = -1083586
08
XDOT = 8391
411841 XDOT = 2557
702329
YDOT = -11993
027497 feet/sec YDOT = -3655
474781 meter/sec
ZDOT = -19397
270669 ZDOT = -5912
288100
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 07283
57133927
00020000 00000-0 20000-3 0 9006
2 25544 51
6348 228
7539 0002799 77
8215 282
3262 15
75514814 28985
Satellite: ISS
Catalog Number: 25544
Epoch time: 07283
57133927 = yrday
fracday
Element set: 900
Inclination: 51
6348 deg
RA of node: 228
7539 deg
Eccentricity:
0002799
Arg of perigee: 77
8215 deg
Mean anomaly: 282
3262 deg
Mean motion: 15
75514814 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2898
Checksum: 323
Coasting Arc #2 (Orbit 2913)
---------------------------------------
Vector Time (GMT): 2007/284/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216883
94 A = 6716788
61 meter
Y = -1528465
86 meter E =
0008066
Z = 4994463
82 I = 51
39880
XDOT = 4385
219957 Wp = 63
70516
YDOT = 6065
960326 meter/sec RA = 222
81655 deg
ZDOT = -1840
300850 TA = 44
11544
MA = 44
05113
Ha = 188
608 n
mi
Hp = 180
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13834921
06 X = 4209399
27
Y = -5014651
78 feet Y = -1481351
79 meter
Z = 16386036
14 Z = 5014931
85
XDOT = 14387
204582 XDOT = 4326
003621
YDOT = 19901
444640 feet/sec YDOT = 6114
667120 meter/sec
ZDOT = -6037
732447 ZDOT = -1819
141183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8588873
48 X = -2617888
64
Y = 11842119
24 feet Y = 3609477
95 meter
Z = 16463578
52 Z = 5018098
73
XDOT = -22220
713117 XDOT = -6772
873358
YDOT = -7808
723374 feet/sec YDOT = -2380
098884 meter/sec
ZDOT = -5956
574819 ZDOT = -1815
564005
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 07284
58618565
00020000 00000-0 20000-3 0 9015
2 25544 51
6348 223
5303 0002779 80
3590 279
7887 15
75545380 29144
Satellite: ISS
Catalog Number: 25544
Epoch time: 07284
58618565 = yrday
fracday
Element set: 901
Inclination: 51
6348 deg
RA of node: 223
5303 deg
Eccentricity:
0002779
Arg of perigee: 80
3590 deg
Mean anomaly: 279
7887 deg
Mean motion: 15
75545380 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2914
Checksum: 321
Coasting Arc #3 (Orbit 2929)
---------------------------------------
Vector Time (GMT): 2007/285/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3858413
88 A = 6725925
91 meter
Y = -5086773
80 meter E =
0016830
Z = 2091569
93 I = 51
45177
XDOT = 5126
816936 Wp = 72
05471
YDOT = -1603
675379 meter/sec RA = 217
68758 deg
ZDOT = 5526
259374 TA = 311
40240
MA = 311
54694
Ha = 188
754 n
mi
Hp = 180
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12658838
18 X = -3811406
78
Y = -16688890
42 feet Y = -5129657
83 meter
Z = 6862106
06 Z = 2072939
69
XDOT = 16820
265539 XDOT = 5117
522139
YDOT = -5261
402163 feet/sec YDOT = -1546
396100 meter/sec
ZDOT = 18130
772223 ZDOT = 5551
143624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19971732
25 X = 6087383
99
Y = 6392988
64 feet Y = 1948582
94 meter
Z = 6790681
42 Z = 2069799
70
XDOT = -10214
038172 XDOT = -3113
238835
YDOT = 12439
960700 feet/sec YDOT = 3791
700021 meter/sec
ZDOT = 18225
083339 ZDOT = 5555
005402
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 07285
60102197
00020000 00000-0 20000-3 0 9029
2 25544 51
6350 218
3057 0002797 83
7584 276
3899 15
75545880 29304
Satellite: ISS
Catalog Number: 25544
Epoch time: 07285
60102197 = yrday
fracday
Element set: 902
Inclination: 51
6350 deg
RA of node: 218
3057 deg
Eccentricity:
0002797
Arg of perigee: 83
7584 deg
Mean anomaly: 276
3899 deg
Mean motion: 15
75545880 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2930
Checksum: 315
Coasting Arc #4 (Orbit 2944)
---------------------------------------
Vector Time (GMT): 2007/286/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4747485
00 A = 6718473
58 meter
Y = 1306802
21 meter E =
0013180
Z = -4583349
82 I = 51
45136
XDOT = -4387
238324 Wp = 105
48088
YDOT = -5585
224657 meter/sec RA = 212
48525 deg
ZDOT = 2955
479720 TA = 193
92343
MA = 193
95981
Ha = 188
683 n
mi
Hp = 180
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15575738
18 X = -4739479
29
Y = 4287408
81 feet Y = 1253757
76 meter
Z = -15037236
94 Z = -4606394
35
XDOT = -14393
826523 XDOT = -4338
815026
YDOT = -18324
227878 feet/sec YDOT = -5634
014395 meter/sec
ZDOT = 9696
455773 ZDOT = 2934
283716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10018608
09 X = 3053671
74
Y = -12568922
27 feet Y = -3831007
51 meter
Z = -15124604
92 Z = -4609979
58
XDOT = 21539
806547 XDOT = 6565
333035
YDOT = 5613
002140 feet/sec YDOT = 1710
843052 meter/sec
ZDOT = 9615
218311 ZDOT = 2930
718541
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 07286
55242014
00020000 00000-0 20000-3 0 9038
2 25544 51
6356 213
4080 0002780 86
9533 273
1949 15
75570037 29452
Satellite: ISS
Catalog Number: 25544
Epoch time: 07286
55242014 = yrday
fracday
Element set: 903
Inclination: 51
6356 deg
RA of node: 213
4080 deg
Eccentricity:
0002780
Arg of perigee: 86
9533 deg
Mean anomaly: 273
1949 deg
Mean motion: 15
75570037 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2945
Checksum: 292
Coasting Arc #5 (Orbit 2960)
---------------------------------------
Vector Time (GMT): 2007/287/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3745416
03 A = 6723652
87 meter
Y = 4676534
21 meter E =
0007165
Z = -3055396
47 I = 51
49428
XDOT = -5759
514593 Wp = 101
74159
YDOT = 1414
147193 meter/sec RA = 207
37268 deg
ZDOT = -4906
870204 TA = 113
74648
MA = 113
67131
Ha = 188
666 n
mi
Hp = 180
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12288110
35 X = 3707686
94
Y = 15342960
01 feet Y = 4718206
58 meter
Z = -10024266
62 Z = -3037292
43
XDOT = -18896
045252 XDOT = -5751
062374
YDOT = 4639
590529 feet/sec YDOT = 1349
788238 meter/sec
ZDOT = -16098
655524 ZDOT = -4934
830201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19088614
80 X = -5818209
79
Y = -4838901
95 feet Y = -1474897
31 meter
Z = -9954888
85 Z = -3034250
12
XDOT = 11884
735416 XDOT = 3622
467355
YDOT = -13621
441377 feet/sec YDOT = -4151
815332 meter/sec
ZDOT = -16204
690740 ZDOT = -4939
189738
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 07287
56723442
00020000 00000-0 20000-3 0 9040
2 25544 51
6360 208
1838 0002724 90
8594 269
2882 15
75587302 29611
Satellite: ISS
Catalog Number: 25544
Epoch time: 07287
56723442 = yrday
fracday
Element set: 904
Inclination: 51
6360 deg
RA of node: 208
1838 deg
Eccentricity:
0002724
Arg of perigee: 90
8594 deg
Mean anomaly: 269
2882 deg
Mean motion: 15
75587302 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2961
Checksum: 313
Coasting Arc #6 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2007/288/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5299967
71 A = 6720751
64 meter
Y = -1221794
96 meter E =
0013676
Z = 3937721
40 I = 51
51038
XDOT = 4155
837911 Wp = 82
04888
YDOT = 5119
879116 meter/sec RA = 202
16485 deg
ZDOT = -3991
304780 TA = 49
42860
MA = 49
30964
Ha = 188
546 n
mi
Hp = 180
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17388345
52 X = 5294106
85
Y = -4008513
64 feet Y = -1162560
51 meter
Z = 12919033
46 Z = 3963455
08
XDOT = 13634
638815 XDOT = 4117
667333
YDOT = 16797
503663 feet/sec YDOT = 5166
138644 meter/sec
ZDOT = -13094
831956 ZDOT = -3971
207876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11190680
55 X = -3410919
43
Y = 13807960
23 feet Y = 4208666
28 meter
Z = 13016645
88 Z = 3967473
66
XDOT = -20132
017855 XDOT = -6136
239042
YDOT = -4002
357433 feet/sec YDOT = -1219
918545 meter/sec
ZDOT = -13017
821474 ZDOT = -3967
831985
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 07288
58203809
00020000 00000-0 20000-3 0 9054
2 25544 51
6352 202
9596 0002775 93
6990 266
4491 15
75603895 29770
Satellite: ISS
Catalog Number: 25544
Epoch time: 07288
58203809 = yrday
fracday
Element set: 905
Inclination: 51
6352 deg
RA of node: 202
9596 deg
Eccentricity:
0002775
Arg of perigee: 93
6990 deg
Mean anomaly: 266
4491 deg
Mean motion: 15
75603895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2977
Checksum: 336
Coasting Arc #7 (Orbit 2992)
---------------------------------------
Vector Time (GMT): 2007/289/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3450475
38 A = 6721139
60 meter
Y = -4271109
38 meter E =
0014101
Z = 3866028
06 I = 51
53915
XDOT = 6375
329584 Wp = 98
82201
YDOT = -1438
533281 meter/sec RA = 197
06037 deg
ZDOT = 4086
033615 TA = 308
50472
MA = 308
63109
Ha = 188
669 n
mi
Hp = 180
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11320457
28 X = -3421239
66
Y = -14012826
05 feet Y = -4309531
15 meter
Z = 12683819
11 Z = 3849336
19
XDOT = 20916
435642 XDOT = 6371
091960
YDOT = -4719
597377 feet/sec YDOT = -1367
264505 meter/sec
ZDOT = 13405
622096 ZDOT = 4116
995386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17666877
42 X = 5384864
24
Y = 3743283
88 feet Y = 1140952
93 meter
Z = 12619848
74 Z = 3846529
90
XDOT = -12974
194663 XDOT = -3954
534533
YDOT = 15478
391872 feet/sec YDOT = 4717
813843 meter/sec
ZDOT = 13523
082727 ZDOT = 4121
835615
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 07289
59683016
00020000 00000-0 20000-3 0 9069
2 25544 51
6355 197
7348 0002740 96
8266 263
3210 15
75613961 29930
Satellite: ISS
Catalog Number: 25544
Epoch time: 07289
59683016 = yrday
fracday
Element set: 906
Inclination: 51
6355 deg
RA of node: 197
7348 deg
Eccentricity:
0002740
Arg of perigee: 96
8266 deg
Mean anomaly: 263
3210 deg
Mean motion: 15
75613961 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2993
Checksum: 321
Coasting Arc #8 (Orbit 3007)
---------------------------------------
Vector Time (GMT): 2007/290/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5799153
19 A = 6723127
42 meter
Y = 1326276
57 meter E =
0007060
Z = -3137936
84 I = 51
57464
XDOT = -3692
640355 Wp = 87
15580
YDOT = -4703
369643 meter/sec RA = 191
85521 deg
ZDOT = 4846
060728 TA = 236
29324
MA = 236
36056
Ha = 188
484 n
mi
Hp = 180
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19026093
15 X = -5798308
97
Y = 4351301
08 feet Y = 1261431
95 meter
Z = -10295068
37 Z = -3166107
62
XDOT = -12114
961793 XDOT = -3663
313888
YDOT = -15431
002766 feet/sec YDOT = -4744
498976 meter/sec
ZDOT = 15899
149369 ZDOT = 4828
192642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11756637
86 X = 3583423
22
Y = -15507912
68 feet Y = -4726811
78 meter
Z = -10401951
01 Z = -3170514
67
XDOT = 18131
021706 XDOT = 5526
335416
YDOT = 3147
916777 feet/sec YDOT = 959
485034 meter/sec
ZDOT = 15830
647042 ZDOT = 4825
181219
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 07290
54818697
00020000 00000-0 20000-3 0 9072
2 25544 51
6357 192
8367 0002596 99
7609 260
3849 15
75641760 30082
Satellite: ISS
Catalog Number: 25544
Epoch time: 07290
54818697 = yrday
fracday
Element set: 907
Inclination: 51
6357 deg
RA of node: 192
8367 deg
Eccentricity:
0002596
Arg of perigee: 99
7609 deg
Mean anomaly: 260
3849 deg
Mean motion: 15
75641760 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3008
Checksum: 336
Coasting Arc #9 (Orbit 3023)
---------------------------------------
Vector Time (GMT): 2007/291/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2939323
20 A = 6718495
61 meter
Y = 3983788
98 meter E =
0012267
Z = -4553473
67 I = 51
58742
XDOT = -6882
487492 Wp = 76
43625
YDOT = 1610
746107 meter/sec RA = 186
75047 deg
ZDOT = -3037
508865 TA = 163
32713
MA = 163
28676
Ha = 188
432 n
mi
Hp = 180
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9643448
81 X = 2916677
74
Y = 13070173
82 feet Y = 4016531
63 meter
Z = -14939218
06 Z = -4539249
12
XDOT = -22580
339540 XDOT = -6885
231656
YDOT = 5284
600087 feet/sec YDOT = 1533
766954 meter/sec
ZDOT = -9965
580265 ZDOT = -3070
951184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15910039
40 X = -4849380
01
Y = -3510515
65 feet Y = -1070005
17 meter
Z = -14884646
82 Z = -4536840
35
XDOT = 13308
972389 XDOT = 4056
574784
YDOT = -17581
360279 feet/sec YDOT = -5358
798613 meter/sec
ZDOT = -10092
473559 ZDOT = -3076
185941
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 07291
56295709
00020000 00000-0 20000-3 0 9089
2 25544 51
6356 187
6118 0002473 103
0706 257
0734 15
75664180 30243
Satellite: ISS
Catalog Number: 25544
Epoch time: 07291
56295709 = yrday
fracday
Element set: 908
Inclination: 51
6356 deg
RA of node: 187
6118 deg
Eccentricity:
0002473
Arg of perigee: 103
0706 deg
Mean anomaly: 257
0734 deg
Mean motion: 15
75664180 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3024
Checksum: 294
Coasting Arc #10 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2007/292/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6182834
64 A = 6725416
28 meter
Y = -1525163
68 meter E =
0016695
Z = 2138719
29 I = 51
63977
XDOT = 3017
953289 Wp = 109
28431
YDOT = 4452
563364 meter/sec RA = 181
55807 deg
ZDOT = -5519
994412 TA = 46
76064
MA = 46
62139
Ha = 188
443 n
mi
Hp = 180
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20284890
55 X = 6189040
07
Y = -5003817
86 feet Y = -1455989
05 meter
Z = 7016795
58 Z = 2168770
98
XDOT = 9901
421551 XDOT = 2994
755263
YDOT = 14608
147520 feet/sec YDOT = 4486
182164 meter/sec
ZDOT = -18110
217888 ZDOT = -5505
389303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11731489
72 X = -3575758
07
Y = 17241631
93 feet Y = 5255249
41 meter
Z = 7130825
72 Z = 2173475
68
XDOT = -15942
952863 XDOT = -4859
412033
YDOT = -3341
717861 feet/sec YDOT = -1018
555604 meter/sec
ZDOT = -18054
132455 ZDOT = -5502
899572
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 07292
57771787
00020000 00000-0 20000-3 0 9097
2 25544 51
6355 182
3871 0002634 107
5371 252
6081 15
75656136 30402
Satellite: ISS
Catalog Number: 25544
Epoch time: 07292
57771787 = yrday
fracday
Element set: 909
Inclination: 51
6355 deg
RA of node: 182
3871 deg
Eccentricity:
0002634
Arg of perigee: 107
5371 deg
Mean anomaly: 252
6081 deg
Mean motion: 15
75656136 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3040
Checksum: 301
Coasting Arc #11 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2007/293/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2299921
96 A = 6716499
11 meter
Y = -3830258
94 meter E =
0008095
Z = 5010221
10 I = 51
63879
XDOT = 7233
196821 Wp = 120
53486
YDOT = -1916
037408 meter/sec RA = 176
44408 deg
ZDOT = 1849
333907 TA = 311
61284
MA = 311
68216
Ha = 188
460 n
mi
Hp = 180
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7545675
73 X = -2281259
55
Y = -12566466
35 feet Y = -3855873
58 meter
Z = 16437733
26 Z = 4999093
31
XDOT = 23730
960700 XDOT = 7245
100808
YDOT = -6286
211967 feet/sec YDOT = -1835
085130 meter/sec
ZDOT = 6067
368460 ZDOT = 1884
502150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14147457
88 X = 4312145
16
Y = 4013450
82 feet Y = 1223299
81 meter
Z = 16394938
91 Z = 4997177
38
XDOT = -12797
526166 XDOT = -3900
685975
YDOT = 19697
190214 feet/sec YDOT = 6003
703577 meter/sec
ZDOT = 6200
808674 ZDOT = 1890
006484
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 07293
59246585
00020000 00000-0 20000-3 0 9105
2 25544 51
6356 177
1619 0002502 109
8265 250
3169 15
75679841 30563
Satellite: ISS
Catalog Number: 25544
Epoch time: 07293
59246585 = yrday
fracday
Element set: 910
Inclination: 51
6356 deg
RA of node: 177
1619 deg
Eccentricity:
0002502
Arg of perigee: 109
8265 deg
Mean anomaly: 250
3169 deg
Mean motion: 15
75679841 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3056
Checksum: 310
Coasting Arc #12 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2007/294/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6383609
63 A = 6726798
90 meter
Y = 1826020
63 meter E =
0010408
Z = -1058811
60 I = 51
70234
XDOT = -2230
344543 Wp = 50
67862
YDOT = -4389
154441 meter/sec RA = 171
27137 deg
ZDOT = 5922
335721 TA = 297
74582
MA = 297
85134
Ha = 188
248 n
mi
Hp = 180
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20943601
14 X = -6398410
44
Y = 5990881
32 feet Y = 1754552
70 meter
Z = -3473791
32 Z = -1089859
59
XDOT = -7317
403356 XDOT = -2209
868608
YDOT = -14400
112994 feet/sec YDOT = -4413
980742 meter/sec
ZDOT = 19430
235304 ZDOT = 5911
550441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10936958
33 X = 3333584
90
Y = -18816900
42 feet Y = -5735391
25 meter
Z = -3591589
45 Z = -1094716
46
XDOT = 13960
250428 XDOT = 4255
084330
YDOT = 4440
674227 feet/sec YDOT = 1353
517504 meter/sec
ZDOT = 19388
665340 ZDOT = 5909
665196
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 07294
54378209
00020000 00000-0 20000-3 0 9111
2 25544 51
6352 172
2631 0002313 113
1814 246
9593 15
75705721 30713
Satellite: ISS
Catalog Number: 25544
Epoch time: 07294
54378209 = yrday
fracday
Element set: 911
Inclination: 51
6352 deg
RA of node: 172
2631 deg
Eccentricity:
0002313
Arg of perigee: 113
1814 deg
Mean anomaly: 246
9593 deg
Mean motion: 15
75705721 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3071
Checksum: 276
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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