Date:
June 6th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 2666)
---------------------------------------
Vector Time (GMT): 2008/157/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213141
27 A = 6716159
99 meter
Y = -2852162
68 meter E =
0007395
Z = 4384481
04 I = 51
94714
XDOT = 1089
622383 Wp = 32
01751
YDOT = -6832
043615 meter/sec RA = 76
51744 deg
ZDOT = -3388
571209 TA = 91
98381
MA = 91
89912
Ha = 184
980 n
mi
Hp = 181
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13822641
96 X = -4202233
84
Y = -9357489
09 feet Y = -2899216
43 meter
Z = 14384780
31 Z = 4364039
42
XDOT = 3574
876584 XDOT = 1182
399469
YDOT = -22414
841256 feet/sec YDOT = -6819
339327 meter/sec
ZDOT = -11117
359608 ZDOT = -3383
054000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16757776
03 X = -5107770
13
Y = -263290
88 feet Y = -80251
06 meter
Z = 14305857
47 Z = 4360425
36
XDOT = -9190
460431 XDOT = -2801
252339
YDOT = -19551
824975 feet/sec YDOT = -5959
396252 meter/sec
ZDOT = -11096
704775 ZDOT = -3382
275616
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 08157
42937534
00020000 00000-0 20000-3 0 9007
2 25544 51
6372 77
0159 0005843 301
4959 58
5634 15
76718339 26678
Satellite: ISS
Catalog Number: 25544
Epoch time: 08157
42937534 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 77
0159 deg
Eccentricity:
0005843
Arg of perigee: 301
4959 deg
Mean anomaly: 58
5634 deg
Mean motion: 15
76718339 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2667
Checksum: 317
Coasting Arc #2 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2008/158/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1181759
61 A = 6718479
56 meter
Y = 5498270
89 meter E =
0007326
Z = 3667767
76 I = 51
94808
XDOT = -4945
557987 Wp = 72
78964
YDOT = -3981
323099 meter/sec RA = 71
43352 deg
ZDOT = 4369
863347 TA = 331
13579
MA = 331
17629
Ha = 185
039 n
mi
Hp = 181
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3877164
06 X = -1260971
57
Y = 18038946
48 feet Y = 5484612
11 meter
Z = 12033358
79 Z = 3661835
54
XDOT = -16225
583948 XDOT = -4921
898545
YDOT = -13062
083658 feet/sec YDOT = -4036
495779 meter/sec
ZDOT = 14336
822006 ZDOT = 4345
894573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6823805
44 X = 2079895
90
Y = 17158367
06 feet Y = 5229870
28 meter
Z = 12010988
07 Z = 3660949
16
XDOT = -19572
845344 XDOT = -5965
803261
YDOT = -2198
503039 feet/sec YDOT = -670
103726 meter/sec
ZDOT = 14244
220033 ZDOT = 4341
638266
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 08158
44345127
00020000 00000-0 20000-3 0 9012
2 25544 51
6379 71
7873 0005827 304
0102 56
0508 15
76762565 26831
Satellite: ISS
Catalog Number: 25544
Epoch time: 08158
44345127 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 71
7873 deg
Eccentricity:
0005827
Arg of perigee: 304
0102 deg
Mean anomaly: 56
0508 deg
Mean motion: 15
76762565 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2683
Checksum: 295
Coasting Arc #3 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2008/159/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4417529
00 A = 6720246
35 meter
Y = 3991303
57 meter E =
0004934
Z = -3111160
97 I = 51
94279
XDOT = -1691
678819 Wp = 357
09968
YDOT = 5693
894030 meter/sec RA = 66
24770 deg
ZDOT = 4907
161879 TA = 326
87105
MA = 326
90194
Ha = 185
348 n
mi
Hp = 181
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14493205
39 X = 4387682
64
Y = 13094827
98 feet Y = 4040536
59 meter
Z = -10207221
03 Z = -3089772
54
XDOT = -5550
127358 XDOT = -1779
061033
YDOT = 18680
754690 feet/sec YDOT = 5674
487236 meter/sec
ZDOT = 16099
612463 ZDOT = 4898
732551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19430898
04 X = 5922537
72
Y = 2376690
27 feet Y = 724415
19 meter
Z = -10124545
83 Z = -3085961
57
XDOT = 6270
307525 XDOT = 1911
189734
YDOT = 17120
323658 feet/sec YDOT = 5218
274651 meter/sec
ZDOT = 16067
642437 ZDOT = 4897
417415
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 08159
39413740
00020000 00000-0 20000-3 0 9025
2 25544 51
6376 66
8848 0005953 309
2753 50
7883 15
76734318 26982
Satellite: ISS
Catalog Number: 25544
Epoch time: 08159
39413740 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 66
8848 deg
Eccentricity:
0005953
Arg of perigee: 309
2753 deg
Mean anomaly: 50
7883 deg
Mean motion: 15
76734318 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2698
Checksum: 329
Coasting Arc #4 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2008/160/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1854291
83 A = 6714445
72 meter
Y = -4366877
11 meter E =
0010135
Z = -4760180
90 I = 51
91145
XDOT = 5154
760336 Wp = 40
21664
YDOT = 5071
064880 meter/sec RA = 61
15631 deg
ZDOT = -2639
605239 TA = 203
93104
MA = 203
97818
Ha = 185
338 n
mi
Hp = 181
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6083634
60 X = 1926109
04
Y = -14327024
65 feet Y = -4345739
06 meter
Z = -15617391
42 Z = -4750999
06
XDOT = 16911
943361 XDOT = 5110
494404
YDOT = 16637
351969 feet/sec YDOT = 5128
461270 meter/sec
ZDOT = -8660
122175 ZDOT = -2614
670324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3426694
53 X = -1044456
49
Y = -15219178
86 feet Y = -4638805
72 meter
Z = -15582410
58 Z = -4749518
74
XDOT = 22390
909380 XDOT = 6824
749179
YDOT = 3741
688241 feet/sec YDOT = 1140
466576 meter/sec
ZDOT = -8563
699325 ZDOT = -2610
215554
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 08160
40818866
00020000 00000-0 20000-3 0 9038
2 25544 51
6383 61
6553 0005947 313
2557 46
8110 15
76781585 27142
Satellite: ISS
Catalog Number: 25544
Epoch time: 08160
40818866 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 61
6553 deg
Eccentricity:
0005947
Arg of perigee: 313
2557 deg
Mean anomaly: 46
8110 deg
Mean motion: 15
76781585 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2714
Checksum: 302
Coasting Arc #5 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2008/161/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4541568
85 A = 6723411
93 meter
Y = -4746759
66 meter E =
0008529
Z = 1415920
38 I = 51
92688
XDOT = 2636
855741 Wp = 107
32371
YDOT = -4273
247568 meter/sec RA = 55
98561 deg
ZDOT = -5841
811236 TA = 57
15238
MA = 57
07030
Ha = 185
471 n
mi
Hp = 180
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14900160
28 X = -4495030
55
Y = -15573358
47 feet Y = -4797286
07 meter
Z = 4645408
08 Z = 1393969
95
XDOT = 8651
101511 XDOT = 2712
822199
YDOT = -14019
841103 feet/sec YDOT = -4243
335193 meter/sec
ZDOT = -19166
047363 ZDOT = -5828
817518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21291941
74 X = -6489783
84
Y = -3461087
50 feet Y = -1054939
47 meter
Z = 4560501
81 Z = 1390040
95
XDOT = -1688
510008 XDOT = -514
657850
YDOT = -14916
622706 feet/sec YDOT = -4546
586601 meter/sec
ZDOT = -19116
381513 ZDOT = -5826
673085
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 08161
42222713
00020000 00000-0 20000-3 0 9042
2 25544 51
6388 56
4260 0005961 317
0548 43
0150 15
76788873 27300
Satellite: ISS
Catalog Number: 25544
Epoch time: 08161
42222713 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 56
4260 deg
Eccentricity:
0005961
Arg of perigee: 317
0548 deg
Mean anomaly: 43
0150 deg
Mean motion: 15
76788873 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2730
Checksum: 284
Coasting Arc #6 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2008/162/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2814072
06 A = 6712082
96 meter
Y = 3080918
45 meter E =
0003842
Z = 5258411
45 I = 51
87193
XDOT = -5181
371168 Wp = 338
12865
YDOT = -5675
947810 meter/sec RA = 50
86534 deg
ZDOT = 556
332362 TA = 106
62617
MA = 106
58398
Ha = 185
592 n
mi
Hp = 180
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9232519
87 X = -2873858
59
Y = 10108000
18 feet Y = 3049114
95 meter
Z = 17252006
09 Z = 5244595
88
XDOT = -16999
249240 XDOT = -5120
219290
YDOT = -18621
876016 feet/sec YDOT = -5733
547021 meter/sec
ZDOT = 1825
237409 ZDOT = 531
309141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1137204
72 X = -346620
00
Y = 13709172
33 feet Y = 4178555
73 meter
Z = 17199074
51 Z = 5242277
91
XDOT = -23866
287883 XDOT = -7274
444547
YDOT = -4133
231886 feet/sec YDOT = -1259
809079 meter/sec
ZDOT = 1728
425576 ZDOT = 526
824116
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 08162
43625070
00020000 00000-0 20000-3 0 9058
2 25544 51
6389 51
1969 0006099 319
6430 40
4281 15
76848202 27466
Satellite: ISS
Catalog Number: 25544
Epoch time: 08162
43625070 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 51
1969 deg
Eccentricity:
0006099
Arg of perigee: 319
6430 deg
Mean anomaly: 40
4281 deg
Mean motion: 15
76848202 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2746
Checksum: 296
Coasting Arc #7 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2008/163/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4409383
25 A = 6724058
20 meter
Y = 5042782
93 meter E =
0014907
Z = 463175
58 I = 51
89265
XDOT = -3868
231843 Wp = 25
63704
YDOT = 2821
929838 meter/sec RA = 45
72502 deg
ZDOT = 6043
091522 TA = 339
39224
MA = 339
45230
Ha = 185
744 n
mi
Hp = 180
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14466480
46 X = 4350416
31
Y = 16544563
41 feet Y = 5091761
42 meter
Z = 1519604
92 Z = 484453
79
XDOT = -12691
049353 XDOT = -3928
855920
YDOT = 9258
299992 feet/sec YDOT = 2778
333357 meter/sec
ZDOT = 19826
415754 ZDOT = 6024
152692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21644431
91 X = 6597222
85
Y = 3776663
29 feet Y = 1151126
97 meter
Z = 1601941
32 Z = 488271
72
XDOT = -3860
926386 XDOT = -1176
810363
YDOT = 13671
132334 feet/sec YDOT = 4166
961136 meter/sec
ZDOT = 19753
736799 ZDOT = 6020
938976
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 08163
45026461
00020000 00000-0 20000-3 0 9061
2 25544 51
6390 45
9670 0006117 324
7125 35
3634 15
76825341 27629
Satellite: ISS
Catalog Number: 25544
Epoch time: 08163
45026461 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 45
9670 deg
Eccentricity:
0006117
Arg of perigee: 324
7125 deg
Mean anomaly: 35
3634 deg
Mean motion: 15
76825341 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2762
Checksum: 282
Coasting Arc #8 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2008/164/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3963387
82 A = 6712872
27 meter
Y = -1874633
11 meter E =
0010368
Z = -5091377
29 I = 51
83458
XDOT = 4809
414859 Wp = 77
00355
YDOT = 5790
096495 meter/sec RA = 40
56542 deg
ZDOT = 1617
018675 TA = 208
46254
MA = 208
51920
Ha = 185
866 n
mi
Hp = 180
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13003240
87 X = 4008788
83
Y = -6150371
10 feet Y = -1830057
74 meter
Z = -16703993
72 Z = -5072012
99
XDOT = 15778
920141 XDOT = 4736
456407
YDOT = 18996
379576 feet/sec YDOT = 5843
469989 meter/sec
ZDOT = 5305
179380 ZDOT = 1640
206479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6094338
04 X = 1857554
23
Y = -13124415
55 feet Y = -4000321
86 meter
Z = -16629597
24 Z = -5068701
24
XDOT = 23312
883670 XDOT = 7105
766943
YDOT = 4010
584118 feet/sec YDOT = 1222
426039 meter/sec
ZDOT = 5394
922528 ZDOT = 1644
372386
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 08164
40088906
00020000 00000-0 20000-3 0 9070
2 25544 51
6399 41
0643 0006135 328
2317 31
8477 15
76852048 27773
Satellite: ISS
Catalog Number: 25544
Epoch time: 08164
40088906 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 41
0643 deg
Eccentricity:
0006135
Arg of perigee: 328
2317 deg
Mean anomaly: 31
8477 deg
Mean motion: 15
76852048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2777
Checksum: 305
Coasting Arc #9 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2008/165/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3859298
99 A = 6721623
92 meter
Y = -4990113
43 meter E =
0001799
Z = -2323938
68 I = 51
84199
XDOT = 5235
421267 Wp = 38
39115
YDOT = -1516
992573 meter/sec RA = 35
45654 deg
ZDOT = -5437
784129 TA = 167
68868
MA = 167
68428
Ha = 185
914 n
mi
Hp = 180
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12661742
08 X = -3791922
54
Y = -16371763
23 feet Y = -5032893
27 meter
Z = -7624470
73 Z = -2342524
37
XDOT = 17176
578961 XDOT = 5278
411418
YDOT = -4977
009755 feet/sec YDOT = -1458
205954 meter/sec
ZDOT = -17840
499110 ZDOT = -5412
246008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20258482
79 X = -6174785
56
Y = -4104366
17 feet Y = -1251010
81 meter
Z = -7696424
55 Z = -2345870
20
XDOT = 9495
106337 XDOT = 2894
108412
YDOT = -13601
496588 feet/sec YDOT = -4145
736160 meter/sec
ZDOT = -17742
303707 ZDOT = -5407
854170
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 08165
41487659
00020000 00000-0 20000-3 0 9081
2 25544 51
6406 35
8349 0006158 331
6615 28
4214 15
76868891 27932
Satellite: ISS
Catalog Number: 25544
Epoch time: 08165
41487659 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 35
8349 deg
Eccentricity:
0006158
Arg of perigee: 331
6615 deg
Mean anomaly: 28
4214 deg
Mean motion: 15
76868891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2793
Checksum: 325
Coasting Arc #10 (Orbit 2808)
---------------------------------------
Vector Time (GMT): 2008/166/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5148259
22 A = 6716261
45 meter
Y = 848271
00 meter E =
0011163
Z = 4228287
31 I = 51
79879
XDOT = -3900
616800 Wp = 39
89138
YDOT = -5572
558790 meter/sec RA = 30
26643 deg
ZDOT = -3617
700620 TA = 86
86612
MA = 86
73839
Ha = 186
097 n
mi
Hp = 179
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16890614
25 X = -5177902
56
Y = 2783041
35 feet Y = 790533
80 meter
Z = 13872333
70 Z = 4203204
93
XDOT = -12797
299213 XDOT = -3820
439344
YDOT = -18282
673194 feet/sec YDOT = -5615
728843 meter/sec
ZDOT = -11869
096522 ZDOT = -3636
456164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10769450
86 X = -3282528
62
Y = 13406156
75 feet Y = 4086196
58 meter
Z = 13775837
56 Z = 4198875
29
XDOT = -20707
808625 XDOT = -6311
740069
YDOT = -4317
677357 feet/sec YDOT = -1316
028058 meter/sec
ZDOT = -11941
744081 ZDOT = -3639
843596
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 08166
42885166
00020000 00000-0 20000-3 0 9099
2 25544 51
6401 30
6056 0006220 336
0818 24
0057 15
76895017 28094
Satellite: ISS
Catalog Number: 25544
Epoch time: 08166
42885166 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 30
6056 deg
Eccentricity:
0006220
Arg of perigee: 336
0818 deg
Mean anomaly: 24
0057 deg
Mean motion: 15
76895017 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2809
Checksum: 285
Coasting Arc #11 (Orbit 2824)
---------------------------------------
Vector Time (GMT): 2008/167/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2820349
02 A = 6717309
29 meter
Y = 4697551
76 meter E =
0009732
Z = 3875244
35 I = 51
77729
XDOT = -6505
819645 Wp = 65
58285
YDOT = 515
570667 meter/sec RA = 25
17006 deg
ZDOT = 4105
802166 TA = 341
72579
MA = 341
76074
Ha = 186
126 n
mi
Hp = 179
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9253113
57 X = 2748785
20
Y = 15411915
22 feet Y = 4728689
68 meter
Z = 12714056
26 Z = 3888772
77
XDOT = -21344
552641 XDOT = -6531
046760
YDOT = 1691
504814 feet/sec YDOT = 442
677074 meter/sec
ZDOT = 13470
479548 ZDOT = 4074
135371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17216012
39 X = 5247440
58
Y = 5041797
10 feet Y = 1536739
76 meter
Z = 12766505
68 Z = 3891230
93
XDOT = -14173
762693 XDOT = -4320
162869
YDOT = 14564
414016 feet/sec YDOT = 4439
233392 meter/sec
ZDOT = 13348
605480 ZDOT = 4068
654950
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 08167
44281403
00020000 00000-0 20000-3 0 9108
2 25544 51
6407 25
3755 0006269 339
9357 20
1561 15
76904798 28252
Satellite: ISS
Catalog Number: 25544
Epoch time: 08167
44281403 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 25
3755 deg
Eccentricity:
0006269
Arg of perigee: 339
9357 deg
Mean anomaly: 20
1561 deg
Mean motion: 15
76904798 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2825
Checksum: 302
Coasting Arc #12 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2008/168/09:18:27
802
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6104580
96 A = 6720485
26 meter
Y = -127286
82 meter E =
0008773
Z = -2797819
46 I = 51
76138
XDOT = 2455
667314 Wp = 14
01969
YDOT = 5196
392650 meter/sec RA = 19
97204 deg
ZDOT = 5133
303637 TA = 313
95053
MA = 314
02287
Ha = 186
297 n
mi
Hp = 179
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20028152
76 X = 6119142
02
Y = -417607
67 feet Y = -58939
93 meter
Z = -9179197
69 Z = -2768127
79
XDOT = 8056
651293 XDOT = 2372
441042
YDOT = 17048
532315 feet/sec YDOT = 5223
386970 meter/sec
ZDOT = 16841
547366 ZDOT = 5145
032247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14183746
64 X = 4323205
98
Y = -14219985
72 feet Y = -4334251
65 meter
Z = -9064894
20 Z = -2762979
75
XDOT = 16518
398710 XDOT = 5034
807927
YDOT = 5735
915596 feet/sec YDOT = 1748
307074 meter/sec
ZDOT = 16887
101907 ZDOT = 5147
188661
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 08168
39339155
00020000 00000-0 20000-3 0 9112
2 25544 51
6411 20
4727 0006351 342
6221 17
4726 15
76939859 28400
Satellite: ISS
Catalog Number: 25544
Epoch time: 08168
39339155 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 20
4727 deg
Eccentricity:
0006351
Arg of perigee: 342
6221 deg
Mean anomaly: 17
4726 deg
Mean motion: 15
76939859 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2840
Checksum: 294
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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