Date:
August 29th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 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 2203)
---------------------------------------
Vector Time (GMT): 2007/239/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1863239
92 A = 6724473
63 meter
Y = -6231504
55 meter E =
0004040
Z = -1698769
62 I = 51
96978
XDOT = 4267
997502 Wp = 235
09471
YDOT = 2844
361332 meter/sec RA = 94
85939 deg
ZDOT = -5745
301999 TA = 323
61794
MA = 323
64540
Ha = 185
909 n
mi
Hp = 183
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6112991
87 X = 1941035
21
Y = -20444568
72 feet Y = -6210233
78 meter
Z = -5573391
16 Z = -1689529
17
XDOT = 14002
616477 XDOT = 4263
783336
YDOT = 9331
894134 feet/sec YDOT = 2892
064886 meter/sec
ZDOT = -18849
416008 ZDOT = -5724
578717
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9572015
57 X = -2917550
35
Y = 19081578
94 feet Y = 5816065
26 meter
Z = -5539098
47 Z = -1688317
21
XDOT = -10899
670854 XDOT = -3322
219676
YDOT = -10923
440209 feet/sec YDOT = -3329
464576 meter/sec
ZDOT = -18770
412959 ZDOT = -5721
221870
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 07239
57129639
00020000 00000-0 20000-3 0 9002
2 25544 51
6328 95
4569 0008899 295
5931 64
4313 15
76273086 22047
Satellite: ISS
Catalog Number: 25544
Epoch time: 07239
57129639 = yrday
fracday
Element set: 900
Inclination: 51
6328 deg
RA of node: 95
4569 deg
Eccentricity:
0008899
Arg of perigee: 295
5931 deg
Mean anomaly: 64
4313 deg
Mean motion: 15
76273086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2204
Checksum: 321
Coasting Arc #2 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2007/240/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3698790
16 A = 6716060
41 meter
Y = -3056686
29 meter E =
0008028
Z = 4703275
39 I = 51
94251
XDOT = 2133
760754 Wp = 353
96928
YDOT = -6859
800306 meter/sec RA = 89
69018 deg
ZDOT = -2772
787713 TA = 123
28244
MA = 123
20551
Ha = 186
069 n
mi
Hp = 182
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12135138
31 X = -3687182
24
Y = -10028498
32 feet Y = -3097983
18 meter
Z = 15430693
53 Z = 4685335
25
XDOT = 7000
527408 XDOT = 2223
778965
YDOT = -22505
906517 feet/sec YDOT = -6835
436168 meter/sec
ZDOT = -9097
072549 ZDOT = -2762
203181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10517317
12 X = 3205678
26
Y = 11803676
09 feet Y = 3597760
47 meter
Z = 15362224
27 Z = 4682405
96
XDOT = -9597
832441 XDOT = -2925
419328
YDOT = 20372
016884 feet/sec YDOT = 6209
390746 meter/sec
ZDOT = -9057
757519 ZDOT = -2760
804492
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 07240
58564777
00020000 00000-0 20000-3 0 9012
2 25544 51
6325 90
2278 0008956 299
2098 60
8170 15
76309702 22207
Satellite: ISS
Catalog Number: 25544
Epoch time: 07240
58564777 = yrday
fracday
Element set: 901
Inclination: 51
6325 deg
RA of node: 90
2278 deg
Eccentricity:
0008956
Arg of perigee: 299
2098 deg
Mean anomaly: 60
8170 deg
Mean motion: 15
76309702 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2220
Checksum: 301
Coasting Arc #3 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2007/241/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1895169
50 A = 6721348
43 meter
Y = 5653184
78 meter E =
0008141
Z = 3090855
40 I = 51
95818
XDOT = -4260
378643 Wp = 42
79828
YDOT = -4122
004728 meter/sec RA = 84
60309 deg
ZDOT = 4925
223822 TA = 352
96032
MA = 352
97175
Ha = 186
200 n
mi
Hp = 182
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6217747
72 X = -1973258
07
Y = 18547194
16 feet Y = 5631555
47 meter
Z = 10140601
72 Z = 3081458
79
XDOT = -13977
620220 XDOT = -4237
894735
YDOT = -13523
637559 feet/sec YDOT = -4169
520715 meter/sec
ZDOT = 16158
870808 ZDOT = 4904
581948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8776993
37 X = 2675227
58
Y = -17502312
81 feet Y = -5334704
94 meter
Z = 10105643
70 Z = 3080200
20
XDOT = 10788
438108 XDOT = 3288
315935
YDOT = 14697
742886 feet/sec YDOT = 4479
872032 meter/sec
ZDOT = 16080
014933 ZDOT = 4901
188551
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 07241
59998278
00020000 00000-0 20000-3 0 9022
2 25544 51
6314 84
9984 0008940 302
6107 57
4194 15
76355175 22362
Satellite: ISS
Catalog Number: 25544
Epoch time: 07241
59998278 = yrday
fracday
Element set: 902
Inclination: 51
6314 deg
RA of node: 84
9984 deg
Eccentricity:
0008940
Arg of perigee: 302
6107 deg
Mean anomaly: 57
4194 deg
Mean motion: 15
76355175 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2236
Checksum: 316
Coasting Arc #4 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2007/242/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3772418
18 A = 6719300
42 meter
Y = 4072092
09 meter E =
0003982
Z = -3782127
70 I = 51
94682
XDOT = -2252
698226 Wp = 343
39246
YDOT = 6024
421128 meter/sec RA = 79
41955 deg
ZDOT = 4242
024584 TA = 330
95889
MA = 330
98104
Ha = 186
403 n
mi
Hp = 182
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12376700
08 X = 3744975
89
Y = 13359882
18 feet Y = 4114123
75 meter
Z = -12408555
43 Z = -3763868
24
XDOT = -7390
742211 XDOT = -2340
503685
YDOT = 19765
161182 feet/sec YDOT = 5998
739477 meter/sec
ZDOT = 13917
403491 ZDOT = 4230
867404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10736586
60 X = -3272511
59
Y = -14768965
44 feet Y = -4501580
67 meter
Z = -12338750
86 Z = -3760851
26
XDOT = 8730
564237 XDOT = 2661
075979
YDOT = -17932
124671 feet/sec YDOT = -5465
711600 meter/sec
ZDOT = 13875
806406 ZDOT = 4229
345792
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 07242
55090850
00020000 00000-0 20000-3 0 9039
2 25544 51
6310 80
0959 0008800 306
7577 53
2778 15
76357485 22513
Satellite: ISS
Catalog Number: 25544
Epoch time: 07242
55090850 = yrday
fracday
Element set: 903
Inclination: 51
6310 deg
RA of node: 80
0959 deg
Eccentricity:
0008800
Arg of perigee: 306
7577 deg
Mean anomaly: 53
2778 deg
Mean motion: 15
76357485 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2251
Checksum: 294
Coasting Arc #5 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2007/243/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2100719
02 A = 6717601
20 meter
Y = -4781737
14 meter E =
0008800
Z = -4231320
11 I = 51
93514
XDOT = 4404
967696 Wp = 7
87415
YDOT = 5160
470215 meter/sec RA = 74
33826 deg
ZDOT = -3637
180074 TA = 225
21291
MA = 225
28451
Ha = 186
468 n
mi
Hp = 182
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6892122
78 X = 2174588
02
Y = -15688113
98 feet Y = -4757832
88 meter
Z = -13882283
83 Z = -4220935
16
XDOT = 14451
993752 XDOT = 4364
603959
YDOT = 16930
676560 feet/sec YDOT = 5209
503206 meter/sec
ZDOT = -11933
005493 ZDOT = -3615
878975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8563980
60 X = -2610301
29
Y = 14877935
98 feet Y = 4534794
89 meter
Z = -13843458
32 Z = -4219486
10
XDOT = -11594
057885 XDOT = -3533
868843
YDOT = -17724
603992 feet/sec YDOT = -5402
459297 meter/sec
ZDOT = -11851
528259 ZDOT = -3612
345813
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 07243
56521203
00020000 00000-0 20000-3 0 9043
2 25544 51
6312 74
8679 0008770 311
7199 48
3214 15
76400249 22671
Satellite: ISS
Catalog Number: 25544
Epoch time: 07243
56521203 = yrday
fracday
Element set: 904
Inclination: 51
6312 deg
RA of node: 74
8679 deg
Eccentricity:
0008770
Arg of perigee: 311
7199 deg
Mean anomaly: 48
3214 deg
Mean motion: 15
76400249 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2267
Checksum: 286
Coasting Arc #6 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2007/244/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3928119
54 A = 6722645
51 meter
Y = -4857751
25 meter E =
0007496
Z = 2481512
87 I = 51
94340
XDOT = 2630
763660 Wp = 68
93887
YDOT = -4870
169294 meter/sec RA = 69
15788 deg
ZDOT = -5353
830805 TA = 83
10249
MA = 83
01723
Ha = 186
595 n
mi
Hp = 181
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12887531
32 X = -3885562
30
Y = -15937504
11 feet Y = -4901439
70 meter
Z = 8141446
43 Z = 2462533
44
XDOT = 8631
114369 XDOT = 2711
035172
YDOT = -15978
245716 feet/sec YDOT = -4840
301902 meter/sec
ZDOT = -17565
061697 ZDOT = -5340
855406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11499292
74 X = 3504984
43
Y = 17001058
49 feet Y = 5181922
63 meter
Z = 8068824
43 Z = 2459377
69
XDOT = -8845
261481 XDOT = -2696
035700
YDOT = 14320
617989 feet/sec YDOT = 4364
924363 meter/sec
ZDOT = -17516
408102 ZDOT = -5339
001190
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 07244
57949748
00020000 00000-0 20000-3 0 9054
2 25544 51
6313 69
6386 0008977 314
4891 45
5539 15
76427152 22836
Satellite: ISS
Catalog Number: 25544
Epoch time: 07244
57949748 = yrday
fracday
Element set: 905
Inclination: 51
6313 deg
RA of node: 69
6386 deg
Eccentricity:
0008977
Arg of perigee: 314
4891 deg
Mean anomaly: 45
5539 deg
Mean motion: 15
76427152 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2283
Checksum: 332
Coasting Arc #7 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2007/245/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2563081
18 A = 6714456
56 meter
Y = 3682983
97 meter E =
0003527
Z = 4994903
35 I = 51
90444
XDOT = -4581
697876 Wp = 342
93876
YDOT = -5869
552248 meter/sec RA = 64
06063 deg
ZDOT = 1980
506646 TA = 88
01771
MA = 87
97732
Ha = 186
843 n
mi
Hp = 181
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8409058
98 X = -2628338
83
Y = 12083280
73 feet Y = 3653957
24 meter
Z = 16387478
20 Z = 4982293
35
XDOT = -15031
817179 XDOT = -4525
344145
YDOT = -19257
061182 feet/sec YDOT = -5920
472302 meter/sec
ZDOT = 6497
725217 ZDOT = 1958
385482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9322996
79 X = 2841649
42
Y = -11460870
59 feet Y = -3493273
36 meter
Z = 16340060
10 Z = 4980450
32
XDOT = 12852
599095 XDOT = 3917
472204
YDOT = 19581
260829 feet/sec YDOT = 5968
368301 meter/sec
ZDOT = 6413
063778 ZDOT = 1954
701839
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 07245
59376876
00020000 00000-0 20000-3 0 9064
2 25544 51
6314 64
4095 0008840 319
0868 40
9632 15
76425759 22992
Satellite: ISS
Catalog Number: 25544
Epoch time: 07245
59376876 = yrday
fracday
Element set: 906
Inclination: 51
6314 deg
RA of node: 64
4095 deg
Eccentricity:
0008840
Arg of perigee: 319
0868 deg
Mean anomaly: 40
9632 deg
Mean motion: 15
76425759 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2299
Checksum: 328
Coasting Arc #8 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2007/246/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4037510
85 A = 6724824
10 meter
Y = 5284775
23 meter E =
0014855
Z = -928749
48 I = 51
92713
XDOT = -3309
808541 Wp = 3
78928
YDOT = 3575
302570 meter/sec RA = 58
90085 deg
ZDOT = 5975
500326 TA = 346
09196
MA = 346
13284
Ha = 186
875 n
mi
Hp = 181
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13246426
67 X = 3982627
34
Y = 17338501
42 feet Y = 5329618
11 meter
Z = -3047078
35 Z = -909268
35
XDOT = -10858
951905 XDOT = -3378
570111
YDOT = 11729
995310 feet/sec YDOT = 3537
905784 meter/sec
ZDOT = 19604
659861 ZDOT = 5959
254304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12333449
32 X = -3759235
35
Y = -18011838
94 feet Y = -5490008
51 meter
Z = -2972511
30 Z = -906021
44
XDOT = 10256
976807 XDOT = 3126
326531
YDOT = -10237
613100 feet/sec YDOT = -3120
424473 meter/sec
ZDOT = 19543
420854 ZDOT = 5956
834676
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 07246
54463056
00020000 00000-0 20000-3 0 9078
2 25544 51
6327 59
5079 0008702 322
6515 37
4044 15
76461569 23144
Satellite: ISS
Catalog Number: 25544
Epoch time: 07246
54463056 = yrday
fracday
Element set: 907
Inclination: 51
6327 deg
RA of node: 59
5079 deg
Eccentricity:
0008702
Arg of perigee: 322
6515 deg
Mean anomaly: 37
4044 deg
Mean motion: 15
76461569 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2314
Checksum: 294
Coasting Arc #9 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2007/247/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3275316
63 A = 6712970
05 meter
Y = -2548725
45 meter E =
0012767
Z = -5285315
96 I = 51
87197
XDOT = 4614
208106 Wp = 54
00463
YDOT = 6160
508467 meter/sec RA = 53
77550 deg
ZDOT = -104
168231 TA = 214
96769
MA = 215
05160
Ha = 186
978 n
mi
Hp = 181
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10745789
46 X = 3329248
51
Y = -8361960
12 feet Y = -2511797
24 meter
Z = -17340275
47 Z = -5269273
60
XDOT = 15138
478037 XDOT = 4545
483475
YDOT = 20211
641953 feet/sec YDOT = 6211
722891 meter/sec
ZDOT = -341
759288 ZDOT = -81
919103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11132155
81 X = -3393081
09
Y = 7972905
97 feet Y = 2430141
74 meter
Z = -17279681
68 Z = -5266846
98
XDOT = -13834
033251 XDOT = -4216
613335
YDOT = -19922
994029 feet/sec YDOT = -6072
528580 meter/sec
ZDOT = -256
584494 ZDOT = -78
206954
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 07247
55886654
00020000 00000-0 20000-3 0 9084
2 25544 51
6332 54
2805 0008679 327
2117 32
8508 15
76506188 23300
Satellite: ISS
Catalog Number: 25544
Epoch time: 07247
55886654 = yrday
fracday
Element set: 908
Inclination: 51
6332 deg
RA of node: 54
2805 deg
Eccentricity:
0008679
Arg of perigee: 327
2117 deg
Mean anomaly: 32
8508 deg
Mean motion: 15
76506188 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2330
Checksum: 306
Coasting Arc #10 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2007/248/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3945923
62 A = 6724665
90 meter
Y = -5391231
71 meter E =
0002295
Z = -765492
50 I = 51
89324
XDOT = 4263
704862 Wp = 96
81435
YDOT = -2271
726173 meter/sec RA = 48
64336 deg
ZDOT = -5994
479856 TA = 91
50364
MA = 91
47735
Ha = 187
097 n
mi
Hp = 180
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12945943
64 X = -3881626
20
Y = -17687768
09 feet Y = -5434997
72 meter
Z = -2511458
35 Z = -784505
73
XDOT = 13988
533013 XDOT = 4317
910675
YDOT = -7453
169860 feet/sec YDOT = -2223
743690 meter/sec
ZDOT = -19666
928663 ZDOT = -5973
635335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12607709
61 X = 3842829
89
Y = 17920080
15 feet Y = 5462040
43 meter
Z = -2584261
12 Z = -787682
79
XDOT = -12925
311929 XDOT = -3939
635076
YDOT = 6275
962331 feet/sec YDOT = 1912
913318 meter/sec
ZDOT = -19588
068371 ZDOT = -5970
443239
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 07248
57308357
00020000 00000-0 20000-3 0 9097
2 25544 51
6327 49
0505 0008917 331
0799 28
9871 15
76546437 23464
Satellite: ISS
Catalog Number: 25544
Epoch time: 07248
57308357 = yrday
fracday
Element set: 909
Inclination: 51
6327 deg
RA of node: 49
0505 deg
Eccentricity:
0008917
Arg of perigee: 331
0799 deg
Mean anomaly: 28
9871 deg
Mean motion: 15
76546437 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2346
Checksum: 323
Coasting Arc #11 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2007/249/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203524
62 A = 6714124
69 meter
Y = 1461041
35 meter E =
0011175
Z = 5029740
93 I = 51
83772
XDOT = -4332
042130 Wp = 4
41966
YDOT = -6098
631811 meter/sec RA = 43
48151 deg
ZDOT = -1837
712744 TA = 103
30588
MA = 103
18124
Ha = 187
352 n
mi
Hp = 180
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13791091
26 X = -4243983
09
Y = 4793442
74 feet Y = 1413808
80 meter
Z = 16501774
70 Z = 5009222
20
XDOT = -14212
736646 XDOT = -4254
597175
YDOT = -20008
634552 feet/sec YDOT = -6146
642082 meter/sec
ZDOT = -6029
241285 ZDOT = -1858
569640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13888339
30 X = 4233165
82
Y = -4779581
51 feet Y = -1456816
45 meter
Z = 16424052
23 Z = 5006051
12
XDOT = 13810
265995 XDOT = 4209
369075
YDOT = 19009
885111 feet/sec YDOT = 5794
212982 meter/sec
ZDOT = -6109
128260 ZDOT = -1862
062294
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 07249
58728546
00020000 00000-0 20000-3 0 9107
2 25544 51
6334 43
8217 0008752 335
3566 24
7179 15
76506321 23621
Satellite: ISS
Catalog Number: 25544
Epoch time: 07249
58728546 = yrday
fracday
Element set: 910
Inclination: 51
6334 deg
RA of node: 43
8217 deg
Eccentricity:
0008752
Arg of perigee: 335
3566 deg
Mean anomaly: 24
7179 deg
Mean motion: 15
76506321 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2362
Checksum: 300
Coasting Arc #12 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2007/250/13:01:45
256
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3517274
86 A = 6722226
85 meter
Y = 5189123
13 meter E =
0015618
Z = 2398475
82 I = 51
84545
XDOT = -5383
704603 Wp = 40
05077
YDOT = 1149
214024 meter/sec RA = 38
37699 deg
ZDOT = 5401
082901 TA = 346
97764
MA = 347
01792
Ha = 187
225 n
mi
Hp = 180
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11539615
68 X = 3447336
70
Y = 17024682
18 feet Y = 5228064
22 meter
Z = 7869015
15 Z = 2415392
66
XDOT = -17663
072845 XDOT = -5422
392280
YDOT = 3770
387218 feet/sec YDOT = 1088
794048 meter/sec
ZDOT = 17720
088258 ZDOT = 5374
835264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11769681
65 X = -3587398
97
Y = -16836052
67 feet Y = -5131628
85 meter
Z = 7933842
52 Z = 2418235
20
XDOT = 16471
212335 XDOT = 5020
425520
YDOT = -3199
458329 feet/sec YDOT = -975
194899 meter/sec
ZDOT = 17620
578040 ZDOT = 5370
752187
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 07250
60146398
00020000 00000-0 20000-3 0 9112
2 25544 51
6346 38
5928 0008802 338
2059 21
8729 15
76606038 23781
Satellite: ISS
Catalog Number: 25544
Epoch time: 07250
60146398 = yrday
fracday
Element set: 911
Inclination: 51
6346 deg
RA of node: 38
5928 deg
Eccentricity:
0008802
Arg of perigee: 338
2059 deg
Mean anomaly: 21
8729 deg
Mean motion: 15
76606038 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2378
Checksum: 305
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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