Date:
October 9th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3229 17 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 2787)
---------------------------------------
Vector Time (GMT): 2007/276/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3708346
64 A = 6720771
16 meter
Y = 3795634
00 meter E =
0012939
Z = 4116607
43 I = 51
30614
XDOT = -2338
171833 Wp = 71
18502
YDOT = 6332
252106 meter/sec RA = 264
08291 deg
ZDOT = -3718
594711 TA = 57
06330
MA = 56
93893
Ha = 188
757 n
mi
Hp = 180
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12166491
59 X = 3645629
81
Y = 12452867
46 feet Y = 3836752
13 meter
Z = 13505929
89 Z = 4134470
39
XDOT = -7671
167430 XDOT = -2390
741865
YDOT = 20775
105334 feet/sec YDOT = 6305
811439 meter/sec
ZDOT = -12200
113882 ZDOT = -3730
081274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16714978
00 X = -5094725
29
Y = -4675211
14 feet Y = -1425004
36 meter
Z = 13574221
12 Z = 4137422
60
XDOT = -4228
147505 XDOT = -1288
739359
YDOT = -20559
423276 feet/sec YDOT = -6266
512215 meter/sec
ZDOT = -12242
947815 ZDOT = -3731
650494
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 07276
59392378
00020000 00000-0 20000-3 0 9007
2 25544 51
6315 264
6643 0002682 55
7481 304
3937 15
75386692 27888
Satellite: ISS
Catalog Number: 25544
Epoch time: 07276
59392378 = yrday
fracday
Element set: 900
Inclination: 51
6315 deg
RA of node: 264
6643 deg
Eccentricity:
0002682
Arg of perigee: 55
7481 deg
Mean anomaly: 304
3937 deg
Mean motion: 15
75386692 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2788
Checksum: 327
Coasting Arc #2 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2007/277/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1891861
13 A = 6722420
83 meter
Y = -5346169
40 meter E =
0014238
Z = 3597208
98 I = 51
31688
XDOT = 4449
823386 Wp = 88
75590
YDOT = 4526
713131 meter/sec RA = 258
96519 deg
ZDOT = 4372
744413 TA = 314
57256
MA = 314
68870
Ha = 188
699 n
mi
Hp = 180
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6206893
48 X = 1934027
54
Y = -17539925
85 feet Y = -5324777
74 meter
Z = 11801866
74 Z = 3606502
15
XDOT = 14599
158091 XDOT = 4377
632209
YDOT = 14851
421032 feet/sec YDOT = 4576
069973 meter/sec
ZDOT = 14346
274320 ZDOT = 4394
186327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3835585
38 X = 1169086
42
Y = 18183629
07 feet Y = 5542370
14 meter
Z = 11836490
30 Z = 3607762
24
XDOT = -18786
274450 XDOT = -5726
056452
YDOT = -5460
304020 feet/sec YDOT = -1664
300665 meter/sec
ZDOT = 14428
256303 ZDOT = 4397
732521
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 07277
60885715
00020000 00000-0 20000-3 0 9013
2 25544 51
6320 259
4410 0002548 61
7517 298
3904 15
75436885 28041
Satellite: ISS
Catalog Number: 25544
Epoch time: 07277
60885715 = yrday
fracday
Element set: 901
Inclination: 51
6320 deg
RA of node: 259
4410 deg
Eccentricity:
0002548
Arg of perigee: 61
7517 deg
Mean anomaly: 298
3904 deg
Mean motion: 15
75436885 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2804
Checksum: 306
Coasting Arc #3 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2007/278/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4078310
66 A = 6722895
53 meter
Y = -4072151
40 meter E =
0007583
Z = -3467191
89 I = 51
32477
XDOT = 2047
802678 Wp = 83
51250
YDOT = -5887
256036 meter/sec RA = 253
74329 deg
ZDOT = 4515
024609 TA = 235
16385
MA = 235
23519
Ha = 188
836 n
mi
Hp = 180
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13380284
31 X = -4015629
12
Y = -13360076
79 feet Y = -4117407
02 meter
Z = -11375301
47 Z = -3486851
98
XDOT = 6718
512722 XDOT = 2091
549445
YDOT = -19315
144474 feet/sec YDOT = -5864
111607 meter/sec
ZDOT = 14813
072863 ZDOT = 4525
079295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18386540
62 X = 5604217
58
Y = 4212240
43 feet Y = 1283890
88 meter
Z = -11450471
52 Z = -3490103
72
XDOT = 4982
079236 XDOT = 1518
537751
YDOT = 18540
069620 feet/sec YDOT = 5651
013220 meter/sec
ZDOT = 14850
515050 ZDOT = 4526
436987
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 07278
56034805
00020000 00000-0 20000-3 0 9026
2 25544 51
6317 254
5433 0002731 61
8788 298
2652 15
75397972 28191
Satellite: ISS
Catalog Number: 25544
Epoch time: 07278
56034805 = yrday
fracday
Element set: 902
Inclination: 51
6317 deg
RA of node: 254
5433 deg
Eccentricity:
0002731
Arg of perigee: 61
8788 deg
Mean anomaly: 298
2652 deg
Mean motion: 15
75397972 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2819
Checksum: 319
Coasting Arc #4 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2007/279/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1743762
55 A = 6720131
17 meter
Y = 4904428
32 meter E =
0011289
Z = -4262026
92 I = 51
32582
XDOT = -4892
073298 Wp = 68
57751
YDOT = -4787
806486 meter/sec RA = 248
62445 deg
ZDOT = -3511
316205 TA = 165
66235
MA = 165
63029
Ha = 188
806 n
mi
Hp = 180
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5721005
73 X = -1777770
79
Y = 16090644
08 feet Y = 4884738
20 meter
Z = -13983027
94 Z = -4270581
00
XDOT = -16050
109244 XDOT = -4821
114350
YDOT = -15708
026530 feet/sec YDOT = -4842
115851 meter/sec
ZDOT = -11520
066291 ZDOT = -3534
909349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4082672
67 X = -1244398
63
Y = -16555314
77 feet Y = -5046059
94 meter
Z = -14014889
97 Z = -4271738
46
XDOT = 20767
782044 XDOT = 6330
019967
YDOT = 4697
750016 feet/sec YDOT = 1431
874205 meter/sec
ZDOT = -11610
272960 ZDOT = -3538
811198
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 07279
57525755
00020000 00000-0 20000-3 0 9038
2 25544 51
6323 249
3188 0002731 65
3953 294
7495 15
75446465 28356
Satellite: ISS
Catalog Number: 25544
Epoch time: 07279
57525755 = yrday
fracday
Element set: 903
Inclination: 51
6323 deg
RA of node: 249
3188 deg
Eccentricity:
0002731
Arg of perigee: 65
3953 deg
Mean anomaly: 294
7495 deg
Mean motion: 15
75446465 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2835
Checksum: 326
Coasting Arc #5 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2007/280/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4486379
23 A = 6724926
70 meter
Y = 4247822
19 meter E =
0016033
Z = 2639323
12 I = 51
35438
XDOT = -1977
815953 Wp = 96
62307
YDOT = 5334
274156 meter/sec RA = 243
40861 deg
ZDOT = -5198
085748 TA = 53
17893
MA = 53
03196
Ha = 188
748 n
mi
Hp = 180
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14719091
96 X = 4425724
58
Y = 13936424
51 feet Y = 4297652
47 meter
Z = 8659196
60 Z = 2660970
44
XDOT = -6488
897484 XDOT = -2012
066103
YDOT = 17500
899461 feet/sec YDOT = 5311
965229 meter/sec
ZDOT = -17054
087099 ZDOT = -5207
777603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19964620
67 X = -6085216
38
Y = -3293851
05 feet Y = -1003965
80 meter
Z = 8741953
38 Z = 2664547
39
XDOT = -4777
869243 XDOT = -1456
294545
YDOT = -16615
221164 feet/sec YDOT = -5064
319411 meter/sec
ZDOT = -17090
209904 ZDOT = -5209
095979
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 07280
59015406
00020000 00000-0 20000-3 0 9040
2 25544 51
6327 244
0949 0002727 68
1365 292
0089 15
75463884 28512
Satellite: ISS
Catalog Number: 25544
Epoch time: 07280
59015406 = yrday
fracday
Element set: 904
Inclination: 51
6327 deg
RA of node: 244
0949 deg
Eccentricity:
0002727
Arg of perigee: 68
1365 deg
Mean anomaly: 292
0089 deg
Mean motion: 15
75463884 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2851
Checksum: 304
Coasting Arc #6 (Orbit 2866)
---------------------------------------
Vector Time (GMT): 2007/281/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1756181
13 A = 6717940
57 meter
Y = -4398021
42 meter E =
0009265
Z = 4758470
16 I = 51
34592
XDOT = 5395
780776 Wp = 108
43367
YDOT = 4892
106788 meter/sec RA = 238
28409 deg
ZDOT = 2523
246477 TA = 316
74702
MA = 316
81973
Ha = 188
611 n
mi
Hp = 180
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5761749
10 X = 1782113
91
Y = -14429204
12 feet Y = -4378237
42 meter
Z = 15611778
76 Z = 4767065
13
XDOT = 17702
692834 XDOT = 5328
417875
YDOT = 16050
219120 feet/sec YDOT = 4952
069023 meter/sec
ZDOT = 8278
367707 ZDOT = 2549
295417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3667438
03 X = 1117835
11
Y = 15064763
34 feet Y = 4591739
87 meter
Z = 15643852
58 Z = 4768246
27
XDOT = -22577
984840 XDOT = -6881
769779
YDOT = -3226
942358 feet/sec YDOT = -983
572031 meter/sec
ZDOT = 8377
930838 ZDOT = 2553
593319
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 07281
60503550
00020000 00000-0 20000-3 0 9056
2 25544 51
6332 238
8712 0002541 73
3497 286
7946 15
75516980 28670
Satellite: ISS
Catalog Number: 25544
Epoch time: 07281
60503550 = yrday
fracday
Element set: 905
Inclination: 51
6332 deg
RA of node: 238
8712 deg
Eccentricity:
0002541
Arg of perigee: 73
3497 deg
Mean anomaly: 286
7946 deg
Mean motion: 15
75516980 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2867
Checksum: 308
Coasting Arc #7 (Orbit 2881)
---------------------------------------
Vector Time (GMT): 2007/282/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4919045
66 A = 6726590
42 meter
Y = -4244346
71 meter E =
0009799
Z = -1732101
00 I = 51
39118
XDOT = 2107
169392 Wp = 47
30101
YDOT = -4750
407875 meter/sec RA = 233
08069 deg
ZDOT = 5683
066891 TA = 293
45109
MA = 293
55407
Ha = 188
716 n
mi
Hp = 180
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16138601
24 X = -4862804
78
Y = -13925022
00 feet Y = -4299039
94 meter
Z = -5682746
05 Z = -1755861
11
XDOT = 6913
285408 XDOT = 2132
524824
YDOT = -15585
327674 feet/sec YDOT = -4726
702069 meter/sec
ZDOT = 18645
232583 ZDOT = 5693
365661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21219361
20 X = 6467661
29
Y = 1749075
72 feet Y = 533118
28 meter
Z = -5773537
46 Z = -1759774
22
XDOT = 3819
076172 XDOT = 1164
054417
YDOT = 15054
813151 feet/sec YDOT = 4588
707048 meter/sec
ZDOT = 18683
729528 ZDOT = 5694
800760
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 07282
55647739
00020000 00000-0 20000-3 0 9060
2 25544 51
6331 233
9731 0002654 73
8189 286
3267 15
75487925 28829
Satellite: ISS
Catalog Number: 25544
Epoch time: 07282
55647739 = yrday
fracday
Element set: 906
Inclination: 51
6331 deg
RA of node: 233
9731 deg
Eccentricity:
0002654
Arg of perigee: 73
8189 deg
Mean anomaly: 286
3267 deg
Mean motion: 15
75487925 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2882
Checksum: 331
Coasting Arc #8 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2007/283/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1988181
84 A = 6716423
45 meter
Y = 3894449
18 meter E =
0016695
Z = -5112859
00 I = 51
37664
XDOT = -5838
050218 Wp = 79
25967
YDOT = -4808
837054 meter/sec RA = 227
94300 deg
ZDOT = -1393
484397 TA = 177
33498
MA = 177
32608
Ha = 188
715 n
mi
Hp = 180
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6522906
31 X = -2006744
55
Y = 12777064
24 feet Y = 3872112
02 meter
Z = -16774471
78 Z = -5122563
17
XDOT = -19153
708065 XDOT = -5777
073749
YDOT = -15777
024457 feet/sec YDOT = -4873
780609 meter/sec
ZDOT = -4571
799203 ZDOT = -1421
697719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2584733
22 X = -787826
69
Y = -14067693
82 feet Y = -4287833
08 meter
Z = -16810821
67 Z = -5123938
45
XDOT = 23747
255865 XDOT = 7238
163588
YDOT = 1225
785532 feet/sec YDOT = 373
619430 meter/sec
ZDOT = -4679
580998 ZDOT = -1426
336288
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
57133413
00020000 00000-0 20000-3 0 9073
2 25544 51
6342 228
7484 0002700 78
3845 281
7622 15
75530050 28988
Satellite: ISS
Catalog Number: 25544
Epoch time: 07283
57133413 = yrday
fracday
Element set: 907
Inclination: 51
6342 deg
RA of node: 228
7484 deg
Eccentricity:
0002700
Arg of perigee: 78
3845 deg
Mean anomaly: 281
7622 deg
Mean motion: 15
75530050 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2898
Checksum: 293
Coasting Arc #9 (Orbit 2913)
---------------------------------------
Vector Time (GMT): 2007/284/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5264221
64 A = 6727603
13 meter
Y = 4121865
15 meter E =
0015461
Z = 687036
27 I = 51
43538
XDOT = -2486
132849 Wp = 120
78353
YDOT = 4185
749041 meter/sec RA = 222
76015 deg
ZDOT = -5971
683585 TA = 51
70458
MA = 51
56563
Ha = 188
710 n
mi
Hp = 180
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17271068
38 X = 5214401
50
Y = 13523179
64 feet Y = 4180454
15 meter
Z = 2254056
02 Z = 712489
19
XDOT = -8156
603835 XDOT = -2503
743684
YDOT = 13732
772445 feet/sec YDOT = 4157
848833 meter/sec
ZDOT = -19592
137746 ZDOT = -5983
804564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21925291
89 X = -6682828
97
Y = 8776
10 feet Y = 2674
96 meter
Z = 2351267
21 Z = 716666
24
XDOT = -2142
430245 XDOT = -653
012739
YDOT = -14172
732745 feet/sec YDOT = -4319
848941 meter/sec
ZDOT = -19637
630676 ZDOT = -5985
549830
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
58617741
00020000 00000-0 20000-3 0 9087
2 25544 51
6347 223
5243 0002684 83
1048 277
0421 15
75531729 29147
Satellite: ISS
Catalog Number: 25544
Epoch time: 07284
58617741 = yrday
fracday
Element set: 908
Inclination: 51
6347 deg
RA of node: 223
5243 deg
Eccentricity:
0002684
Arg of perigee: 83
1048 deg
Mean anomaly: 277
0421 deg
Mean motion: 15
75531729 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2914
Checksum: 296
Coasting Arc #10 (Orbit 2929)
---------------------------------------
Vector Time (GMT): 2007/285/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2386766
46 A = 6715542
54 meter
Y = -3442868
19 meter E =
0004910
Z = 5244465
62 I = 51
41737
XDOT = 6195
134402 Wp = 93
39302
YDOT = 4582
341898 meter/sec RA = 217
60647 deg
ZDOT = 188
344190 TA = 354
81318
MA = 354
81826
Ha = 188
470 n
mi
Hp = 180
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7830598
62 X = 2399610
38
Y = -11295499
30 feet Y = -3416105
93 meter
Z = 17206252
04 Z = 5256092
22
XDOT = 20325
244101 XDOT = 6142
518560
YDOT = 15033
930113 feet/sec YDOT = 4651
325217 meter/sec
ZDOT = 617
927131 ZDOT = 218
312925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1119837
18 X = 341326
37
Y = 13643543
73 feet Y = 4158552
13 meter
Z = 17249967
18 Z = 5257790
00
XDOT = -24257
211896 XDOT = -7393
598186
YDOT = 1063
238123 feet/sec YDOT = 324
074980 meter/sec
ZDOT = 732
354042 ZDOT = 223
221512
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
60100458
00020000 00000-0 20000-3 0 9094
2 25544 51
6346 218
3003 0002508 85
7255 274
4195 15
75604366 29300
Satellite: ISS
Catalog Number: 25544
Epoch time: 07285
60100458 = yrday
fracday
Element set: 909
Inclination: 51
6346 deg
RA of node: 218
3003 deg
Eccentricity:
0002508
Arg of perigee: 85
7255 deg
Mean anomaly: 274
4195 deg
Mean motion: 15
75604366 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2930
Checksum: 286
Coasting Arc #11 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2007/286/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5501260
31 A = 6727653
89 meter
Y = -3844096
21 meter E =
0015022
Z = 367465
08 I = 51
48188
XDOT = 3029
650110 Wp = 55
17344
YDOT = -3745
178163 meter/sec RA = 212
44675 deg
ZDOT = 6012
889566 TA = 308
83342
MA = 308
96742
Ha = 188
621 n
mi
Hp = 180
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18048754
30 X = -5459651
31
Y = -12611864
22 feet Y = -3905381
76 meter
Z = 1205594
10 Z = 340840
40
XDOT = 9939
796948 XDOT = 3042
093721
YDOT = -12287
329930 feet/sec YDOT = -3711
229132 meter/sec
ZDOT = 19727
327973 ZDOT = 6027
638370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21935287
28 X = 6685875
56
Y = -1973461
76 feet Y = -601511
15 meter
Z = 1103960
37 Z = 336487
12
XDOT = 245
935346 XDOT = 74
961094
YDOT = 14130
413765 feet/sec YDOT = 4306
950116 meter/sec
ZDOT = 19782
868473 ZDOT = 6029
818311
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
61582140
00020000 00000-0 20000-3 0 9100
2 25544 51
6348 213
0757 0002625 87
5862 272
5603 15
75576843 29462
Satellite: ISS
Catalog Number: 25544
Epoch time: 07286
61582140 = yrday
fracday
Element set: 910
Inclination: 51
6348 deg
RA of node: 213
0757 deg
Eccentricity:
0002625
Arg of perigee: 87
5862 deg
Mean anomaly: 272
5603 deg
Mean motion: 15
75576843 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2946
Checksum: 304
Coasting Arc #12 (Orbit 2960)
---------------------------------------
Vector Time (GMT): 2007/287/13:16:22
438
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2941753
69 A = 6715852
38 meter
Y = 3124853
67 meter E =
0017101
Z = -5180564
65 I = 51
46814
XDOT = -6343
074437 Wp = 97
30366
YDOT = -4218
463443 meter/sec RA = 207
27476 deg
ZDOT = 1058
194483 TA = 182
82186
MA = 182
83152
Ha = 188
559 n
mi
Hp = 180
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9651422
86 X = -2951310
67
Y = 10252144
59 feet Y = 3091903
81 meter
Z = -16996603
20 Z = -5194879
35
XDOT = -20810
611670 XDOT = -6300
572172
YDOT = -13840
103159 feet/sec YDOT = -4289
157635 meter/sec
ZDOT = 3471
766676 ZDOT = 1027
482254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 470648
07 X = 143453
53
Y = -14007038
56 feet Y = -4269345
35 meter
Z = -17050581
02 Z = -5197017
10
XDOT = 23775
522189 XDOT = 7246
779163
YDOT = -3281
219244 feet/sec YDOT = -1000
115626 meter/sec
ZDOT = 3354
550453 ZDOT = 1022
466978
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
56719682
00020000 00000-0 20000-3 0 9119
2 25544 51
6353 208
1779 0002597 91
7819 268
3642 15
75615285 29611
Satellite: ISS
Catalog Number: 25544
Epoch time: 07287
56719682 = yrday
fracday
Element set: 911
Inclination: 51
6353 deg
RA of node: 208
1779 deg
Eccentricity:
0002597
Arg of perigee: 91
7819 deg
Mean anomaly: 268
3642 deg
Mean motion: 15
75615285 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2961
Checksum: 332
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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