Date:
August 13th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6200 0 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
234/21:22:30
000 0
0 0
0 0
0
013/22:45:48
047 0
0 0
0 184
5
000/00:00:00
000 0
0 0
0 183
9
Coasting Arc #1 (Orbit 1972)
---------------------------------------
Vector Time (GMT): 2007/224/21:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6125407
08 A = 6724676
31 meter
Y = -2293898
26 meter E =
0012466
Z = 1525485
33 I = 51
70156
XDOT = 2986
386142 Wp = 155
17704
YDOT = 4119
942611 meter/sec RA = 170
08292 deg
ZDOT = -5790
373638 TA = 8
00015
MA = 7
98029
Ha = 186
218 n
mi
Hp = 182
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20096479
91 X = 6143192
19
Y = -7525912
92 feet Y = -2225301
14 meter
Z = 5004873
12 Z = 1555284
90
XDOT = 9797
854797 XDOT = 2968
222272
YDOT = 13516
872084 feet/sec YDOT = 4153
236803 meter/sec
ZDOT = -18997
288839 ZDOT = -5775
910040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11163262
97 X = 3402562
55
Y = 18296141
86 feet Y = 5576664
04 meter
Z = 5117555
83 Z = 1559831
02
XDOT = -10080
619854 XDOT = -3072
572931
YDOT = 11454
082888 feet/sec YDOT = 3491
204464 meter/sec
ZDOT = -18941
922412 ZDOT = -5773
497951
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 07224
92536503
00020000 00000-0 20000-3 0 9007
2 25544 51
6297 170
9071 0008640 236
5341 123
4997 15
76267538 19734
Satellite: ISS
Catalog Number: 25544
Epoch time: 07224
92536503 = yrday
fracday
Element set: 900
Inclination: 51
6297 deg
RA of node: 170
9071 deg
Eccentricity:
0008640
Arg of perigee: 236
5341 deg
Mean anomaly: 123
4997 deg
Mean motion: 15
76267538 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1973
Checksum: 303
Coasting Arc #2 (Orbit 1988)
---------------------------------------
Vector Time (GMT): 2007/225/21:27:29
021
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 185797
29 A = 6714231
10 meter
Y = -4281161
57 meter E =
0004633
Z = 5171990
00 I = 51
69434
XDOT = 7537
005009 Wp = 239
94264
YDOT = -1077
204985 meter/sec RA = 164
92114 deg
ZDOT = -1165
474561 TA = 221
15778
MA = 221
19273
Ha = 186
267 n
mi
Hp = 182
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 609571
15 X = 208532
03
Y = -14045805
68 feet Y = -4278956
91 meter
Z = 16968471
12 Z = 5172947
68
XDOT = 24727
706723 XDOT = 7554
151851
YDOT = -3534
137089 feet/sec YDOT = -992
826041 meter/sec
ZDOT = -3823
735435 ZDOT = -1128
818989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13798481
02 X = 4205777
02
Y = -2674651
86 feet Y = -815233
89 meter
Z = 16971546
94 Z = 5172927
51
XDOT = 8843
037308 XDOT = 2695
357772
YDOT = 22302
709160 feet/sec YDOT = 6797
865752 meter/sec
ZDOT = -3684
893617 ZDOT = -1123
155574
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 07225
93974951
00020000 00000-0 20000-3 0 9013
2 25544 51
6300 165
6791 0008482 238
1033 121
9306 15
76208518 19896
Satellite: ISS
Catalog Number: 25544
Epoch time: 07225
93974951 = yrday
fracday
Element set: 901
Inclination: 51
6300 deg
RA of node: 165
6791 deg
Eccentricity:
0008482
Arg of perigee: 238
1033 deg
Mean anomaly: 121
9306 deg
Mean motion: 15
76208518 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1989
Checksum: 301
Coasting Arc #3 (Orbit 2004)
---------------------------------------
Vector Time (GMT): 2007/226/21:32:08
464
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5863101
17 A = 6721206
62 meter
Y = -561480
96 meter E =
0006267
Z = 3237069
46 I = 51
74710
XDOT = 3136
135447 Wp = 123
02044
YDOT = -5165
415204 meter/sec RA = 159
79243 deg
ZDOT = 4774
342186 TA = 274
81084
MA = 274
88239
Ha = 185
982 n
mi
Hp = 182
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19235896
24 X = -5872111
66
Y = -1842129
12 feet Y = -627095
87 meter
Z = 10620306
61 Z = 3208565
14
XDOT = 10289
158292 XDOT = 3170
470339
YDOT = -16946
900276 feet/sec YDOT = -5130
153246 meter/sec
ZDOT = 15663
852317 ZDOT = 4789
660592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3287975
87 X = -1002175
05
Y = -19102040
17 feet Y = -5822301
84 meter
Z = 10512151
65 Z = 3204103
82
XDOT = 17637
693914 XDOT = 5375
969105
YDOT = 5633
946982 feet/sec YDOT = 1717
227040 meter/sec
ZDOT = 15721
263415 ZDOT = 4791
841089
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 07226
95411939
00020000 00000-0 20000-3 0 9029
2 25544 51
6310 160
4511 0008649 242
1117 117
9171 15
76287875 20051
Satellite: ISS
Catalog Number: 25544
Epoch time: 07226
95411939 = yrday
fracday
Element set: 902
Inclination: 51
6310 deg
RA of node: 160
4511 deg
Eccentricity:
0008649
Arg of perigee: 242
1117 deg
Mean anomaly: 117
9171 deg
Mean motion: 15
76287875 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2005
Checksum: 282
Coasting Arc #4 (Orbit 2019)
---------------------------------------
Vector Time (GMT): 2007/227/21:36:29
890
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4637589
09 A = 6723204
01 meter
Y = 4257392
27 meter E =
0003760
Z = -2356004
88 I = 51
78189
XDOT = -4934
896048 Wp = 275
65026
YDOT = -2375
484071 meter/sec RA = 154
58639 deg
ZDOT = 5414
325165 TA = 57
85474
MA = 57
81827
Ha = 185
766 n
mi
Hp = 183
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15215187
30 X = -4673406
32
Y = 13967822
41 feet Y = 4205331
87 meter
Z = -7729674
79 Z = -2378620
96
XDOT = -16190
603833 XDOT = -4934
267711
YDOT = -7793
582909 feet/sec YDOT = -2430
665355 meter/sec
ZDOT = 17763
534007 ZDOT = 5390
353297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17847260
62 X = -5439845
04
Y = -10332125
53 feet Y = -3149231
86 meter
Z = -7814878
79 Z = -2381975
05
XDOT = 1844
032448 XDOT = 562
061090
YDOT = -16569
228086 feet/sec YDOT = -5050
300721 meter/sec
ZDOT = 17672
324012 ZDOT = 5386
524359
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 07227
90508503
00020000 00000-0 20000-3 0 9030
2 25544 51
6321 155
5505 0008557 245
6043 114
4228 15
76285513 20204
Satellite: ISS
Catalog Number: 25544
Epoch time: 07227
90508503 = yrday
fracday
Element set: 903
Inclination: 51
6321 deg
RA of node: 155
5505 deg
Eccentricity:
0008557
Arg of perigee: 245
6043 deg
Mean anomaly: 114
4228 deg
Mean motion: 15
76285513 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2020
Checksum: 266
Coasting Arc #5 (Orbit 2035)
---------------------------------------
Vector Time (GMT): 2007/228/21:41:15
136
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2037892
53 A = 6713489
39 meter
Y = 3623783
57 meter E =
0007728
Z = -5277349
79 I = 51
77504
XDOT = -6661
040743 Wp = 113
41455
YDOT = 3861
755636 meter/sec RA = 149
44789 deg
ZDOT = 76
603042 TA = 157
32813
MA = 157
29398
Ha = 185
519 n
mi
Hp = 183
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6685999
11 X = 2022855
56
Y = 11889053
72 feet Y = 3646488
36 meter
Z = -17314139
74 Z = -5267486
33
XDOT = -21853
808212 XDOT = -6704
100526
YDOT = 12669
801954 feet/sec YDOT = 3787
027363 meter/sec
ZDOT = 251
322315 ZDOT = 44
139419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8947414
26 X = -2727171
87
Y = 10358864
61 feet Y = 3157381
93 meter
Z = -17276264
63 Z = -5265805
46
XDOT = -18475
985492 XDOT = -5631
480378
YDOT = -15727
836606 feet/sec YDOT = -4793
844598 meter/sec
ZDOT = 128
718913 ZDOT = 39
233525
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 07228
91943819
00020000 00000-0 20000-3 0 9046
2 25544 51
6322 150
3238 0008489 249
7462 110
2790 15
76322116 20361
Satellite: ISS
Catalog Number: 25544
Epoch time: 07228
91943819 = yrday
fracday
Element set: 904
Inclination: 51
6322 deg
RA of node: 150
3238 deg
Eccentricity:
0008489
Arg of perigee: 249
7462 deg
Mean anomaly: 110
2790 deg
Mean motion: 15
76322116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2036
Checksum: 289
Coasting Arc #6 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2007/229/21:46:03
412
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5953315
98 A = 6722950
63 meter
Y = -1861522
10 meter E =
0007319
Z = -2495041
78 I = 51
83107
XDOT = -508
511853 Wp = 215
50983
YDOT = 5532
611137 meter/sec RA = 144
31044 deg
ZDOT = -5339
223625 TA = 352
67999
MA = 352
69067
Ha = 185
410 n
mi
Hp = 183
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19531876
57 X = 5985809
73
Y = -6107355
97 feet Y = -1794767
07 meter
Z = -8185832
60 Z = -2466041
81
XDOT = -1668
345974 XDOT = -544
403698
YDOT = 18151
611341 feet/sec YDOT = 5526
724022 meter/sec
ZDOT = -17517
137876 ZDOT = -5341
781108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12903623
45 X = 3933024
43
Y = 15939730
60 feet Y = 4858429
89 meter
Z = -8076097
15 Z = -2461594
41
XDOT = -16286
664946 XDOT = -4964
175476
YDOT = 4301
354042 feet/sec YDOT = 1311
052712 meter/sec
ZDOT = -17526
119787 ZDOT = -5341
961311
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 07229
93378166
00020000 00000-0 20000-3 0 9057
2 25544 51
6321 145
0950 0008582 253
8777 106
1443 15
76316566 20520
Satellite: ISS
Catalog Number: 25544
Epoch time: 07229
93378166 = yrday
fracday
Element set: 905
Inclination: 51
6321 deg
RA of node: 145
0950 deg
Eccentricity:
0008582
Arg of perigee: 253
8777 deg
Mean anomaly: 106
1443 deg
Mean motion: 15
76316566 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2052
Checksum: 299
Coasting Arc #7 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2007/230/21:50:25
450
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2510366
72 A = 6721355
84 meter
Y = -5401763
69 meter E =
0005487
Z = 3106380
83 I = 51
84904
XDOT = 5945
585796 Wp = 122
20122
YDOT = -56
736047 meter/sec RA = 139
10924 deg
ZDOT = -4900
088514 TA = 21
78298
MA = 21
75966
Ha = 185
118 n
mi
Hp = 183
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8236111
27 X = 2555493
27
Y = -17722321
82 feet Y = -5373439
09 meter
Z = 10191538
17 Z = 3118685
67
XDOT = 19506
515078 XDOT = 5969
582017
YDOT = -186
141885 feet/sec YDOT = 9
885105 meter/sec
ZDOT = -16076
405887 ZDOT = -4871
146653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19515446
56 X = 5948308
11
Y = 349883
89 feet Y = 106644
61 meter
Z = 10237509
29 Z = 3120392
83
XDOT = 8086
939723 XDOT = 2464
899228
YDOT = 16439
416079 feet/sec YDOT = 5010
734021 meter/sec
ZDOT = -15966
650808 ZDOT = -4866
635166
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 07230
94811584
00020000 00000-0 20000-3 0 9067
2 25544 51
6326 139
8676 0008574 257
5318 102
4887 15
76313816 20687
Satellite: ISS
Catalog Number: 25544
Epoch time: 07230
94811584 = yrday
fracday
Element set: 906
Inclination: 51
6326 deg
RA of node: 139
8676 deg
Eccentricity:
0008574
Arg of perigee: 257
5318 deg
Mean anomaly: 102
4887 deg
Mean motion: 15
76313816 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2068
Checksum: 316
Coasting Arc #8 (Orbit 2083)
---------------------------------------
Vector Time (GMT): 2007/231/21:55:09
183
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3661389
11 A = 6713627
63 meter
Y = -2112836
28 meter E =
0006383
Z = 5220853
82 I = 51
84532
XDOT = 4765
519733 Wp = 242
09562
YDOT = -5978
526129 meter/sec RA = 133
98645 deg
ZDOT = 920
527243 TA = 199
14849
MA = 199
17250
Ha = 184
804 n
mi
Hp = 183
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12012431
47 X = -3662852
87
Y = -6931877
56 feet Y = -2153788
36 meter
Z = 17128785
49 Z = 5203063
19
XDOT = 15634
907261 XDOT = 4827
546567
YDOT = -19614
587037 feet/sec YDOT = -5924
888622 meter/sec
ZDOT = 3020
102503 ZDOT = 943
828567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 942614
82 X = 287309
00
Y = -13920384
83 feet Y = -4242933
29 meter
Z = 17061040
19 Z = 5200205
05
XDOT = 23452
845289 XDOT = 7148
427244
YDOT = 5405
346992 feet/sec YDOT = 1647
549763 meter/sec
ZDOT = 3107
715688 ZDOT = 947
231742
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 07231
96243812
00020000 00000-0 20000-3 0 9074
2 25544 51
6334 134
6394 0008666 262
5303 97
4877 15
76379874 20844
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
96243812 = yrday
fracday
Element set: 907
Inclination: 51
6334 deg
RA of node: 134
6394 deg
Eccentricity:
0008666
Arg of perigee: 262
5303 deg
Mean anomaly: 97
4877 deg
Mean motion: 15
76379874 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2084
Checksum: 320
Coasting Arc #9 (Orbit 2099)
---------------------------------------
Vector Time (GMT): 2007/232/21:59:56
852
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5031420
00 A = 6724227
28 meter
Y = 4113822
34 meter E =
0007028
Z = 1707674
50 I = 51
90037
XDOT = -1942
752009 Wp = 37
05196
YDOT = -4760
569764 meter/sec RA = 128
84027 deg
ZDOT = 5737
611289 TA = 341
78840
MA = 341
81356
Ha = 184
388 n
mi
Hp = 184
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16507283
47 X = -5085342
99
Y = 13496792
44 feet Y = 4057256
58 meter
Z = 5602606
64 Z = 1683101
13
XDOT = -6373
858298 XDOT = -1917
246458
YDOT = -15618
667205 feet/sec YDOT = -4782
152393 meter/sec
ZDOT = 18824
184019 ZDOT = 5728
235126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19696321
35 X = -6003438
75
Y = -8230354
24 feet Y = -2508611
97 meter
Z = 5509919
15 Z = 1679423
36
XDOT = 10124
652258 XDOT = 3085
994008
YDOT = -11636
877439 feet/sec YDOT = -3546
920244 meter/sec
ZDOT = 18788
017145 ZDOT = 5726
587626
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 07232
97675329
00020000 00000-0 20000-3 0 9089
2 25544 51
6336 129
4116 0008519 266
6039 93
4150 15
76366938 21004
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
97675329 = yrday
fracday
Element set: 908
Inclination: 51
6336 deg
RA of node: 129
4116 deg
Eccentricity:
0008519
Arg of perigee: 266
6039 deg
Mean anomaly: 93
4150 deg
Mean motion: 15
76366938 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2100
Checksum: 305
Coasting Arc #10 (Orbit 2114)
---------------------------------------
Vector Time (GMT): 2007/233/22:05:05
949
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -449323
16 A = 6719967
64 meter
Y = 5690182
90 meter E =
0003450
Z = -3544110
88 I = 51
90347
XDOT = -5797
075241 Wp = 261
33719
YDOT = 2346
138940 meter/sec RA = 123
64530 deg
ZDOT = 4497
551327 TA = 56
57330
MA = 56
54031
Ha = 184
421 n
mi
Hp = 184
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1474157
36 X = -495701
64
Y = 18668579
06 feet Y = 5684899
23 meter
Z = -11627660
37 Z = -3546405
97
XDOT = -19019
275725 XDOT = -5844
727484
YDOT = 7697
306234 feet/sec YDOT = 2281
046049 meter/sec
ZDOT = 14755
745825 ZDOT = 4469
273630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16817536
98 X = -5125985
27
Y = 8226391
68 feet Y = 2507404
19 meter
Z = -11635652
08 Z = -3546546
75
XDOT = -15701
197299 XDOT = -4785
724937
YDOT = -11359
424800 feet/sec YDOT = -3462
352679 meter/sec
ZDOT = 14648
771988 ZDOT = 4464
945702
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 07233
92766429
00020000 00000-0 20000-3 0 9098
2 25544 51
6338 124
5113 0008688 270
7753 89
2415 15
76364715 21159
Satellite: ISS
Catalog Number: 25544
Epoch time: 07233
92766429 = yrday
fracday
Element set: 909
Inclination: 51
6338 deg
RA of node: 124
5113 deg
Eccentricity:
0008688
Arg of perigee: 270
7753 deg
Mean anomaly: 89
2415 deg
Mean motion: 15
76364715 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2115
Checksum: 309
Coasting Arc #11 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2007/234/21:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4559454
93 A = 6714832
50 meter
Y = 286790
46 meter E =
0004261
Z = 4924834
99 I = 51
90131
XDOT = 1932
033281 Wp = 227
79869
YDOT = -7122
707760 meter/sec RA = 118
70475 deg
ZDOT = 2201
876885 TA = 200
88947
MA = 200
90689
Ha = 184
470 n
mi
Hp = 183
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14958841
64 X = -4586246
80
Y = 940913
59 feet Y = 235653
91 meter
Z = 16157595
12 Z = 4902620
24
XDOT = 6338
691868 XDOT = 2000
840612
YDOT = -23368
463781 feet/sec YDOT = -7100
718115 meter/sec
ZDOT = 7224
005527 ZDOT = 2211
429257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6196819
94 X = -1888790
72
Y = -13746521
86 feet Y = -4189939
86 meter
Z = 16073353
75 Z = 4899158
22
XDOT = 23084
196841 XDOT = 7036
063197
YDOT = -1911
885543 feet/sec YDOT = -582
742713 meter/sec
ZDOT = 7259
356082 ZDOT = 2212
651734
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 07234
94195923
00020000 00000-0 20000-3 0 9108
2 25544 51
6341 119
2821 0008607 274
3411 85
6770 15
76421602 21313
Satellite: ISS
Catalog Number: 25544
Epoch time: 07234
94195923 = yrday
fracday
Element set: 910
Inclination: 51
6341 deg
RA of node: 119
2821 deg
Eccentricity:
0008607
Arg of perigee: 274
3411 deg
Mean anomaly: 85
6770 deg
Mean motion: 15
76421602 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2131
Checksum: 273
Coasting Arc #12 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2007/235/21:26:31
324
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2903008
45 A = 6725340
06 meter
Y = 6051037
86 meter E =
0009985
Z = 312296
18 I = 51
94958
XDOT = -4164
993174 Wp = 6
46346
YDOT = -2311
277899 meter/sec RA = 113
54230 deg
ZDOT = 6057
855287 TA = 356
92052
MA = 356
92666
Ha = 184
851 n
mi
Hp = 183
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9524305
94 X = -2971973
36
Y = 19852486
42 feet Y = 6018189
16 meter
Z = 1024593
77 Z = 298026
44
XDOT = -13664
675768 XDOT = -4168
266233
YDOT = -7582
932738 feet/sec YDOT = -2357
871943 meter/sec
ZDOT = 19874
853304 ZDOT = 6037
613838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21991965
02 X = -6703150
94
Y = -1137387
29 feet Y = -346675
65 meter
Z = 971204
26 Z = 296023
06
XDOT = 1601
326344 XDOT = 488
084270
YDOT = -14031
079219 feet/sec YDOT = -4276
672946 meter/sec
ZDOT = 19797
767486 ZDOT = 6034
359530
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 07235
95624687
00020000 00000-0 20000-3 0 9115
2 25544 51
6344 114
0546 0008558 279
4068 80
6128 15
76395614 21474
Satellite: ISS
Catalog Number: 25544
Epoch time: 07235
95624687 = yrday
fracday
Element set: 911
Inclination: 51
6344 deg
RA of node: 114
0546 deg
Eccentricity:
0008558
Arg of perigee: 279
4068 deg
Mean anomaly: 80
6128 deg
Mean motion: 15
76395614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2147
Checksum: 311
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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