Date:
June 3rd 2008
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) : 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 2573)
---------------------------------------
Vector Time (GMT): 2008/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 646277
56 A = 6723754
32 meter
Y = -6493458
86 meter E =
0008626
Z = 1600681
33 I = 51
96408
XDOT = 5005
050285 Wp = 127
55225
YDOT = -931
446665 meter/sec RA = 106
74707 deg
ZDOT = -5783
455221 TA = 34
84177
MA = 34
78533
Ha = 184
278 n
mi
Hp = 181
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2120333
19 X = 711064
46
Y = -21303998
90 feet Y = -6485869
73 meter
Z = 5251579
17 Z = 1603977
72
XDOT = 16420
768652 XDOT = 5043
189288
YDOT = -3055
927379 feet/sec YDOT = -875
263508 meter/sec
ZDOT = -18974
590620 ZDOT = -5759
047763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18903580
61 X = -5761811
37
Y = -10044102
63 feet Y = -3061442
48 meter
Z = 5263640
19 Z = 1604357
53
XDOT = 2734
711907 XDOT = 833
540189
YDOT = -15068
732185 feet/sec YDOT = -4592
949570 meter/sec
ZDOT = -18880
780716 ZDOT = -5754
861962
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 08151
53483067
00020000 00000-0 20000-3 0 9000
2 25544 51
6351 107
4052 0005850 281
3139 78
7368 15
76569994 25745
Satellite: ISS
Catalog Number: 25544
Epoch time: 08151
53483067 = yrday
fracday
Element set: 900
Inclination: 51
6351 deg
RA of node: 107
4052 deg
Eccentricity:
0005850
Arg of perigee: 281
3139 deg
Mean anomaly: 78
7368 deg
Mean motion: 15
76569994 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2574
Checksum: 307
Coasting Arc #2 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2008/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4205917
99 A = 6712918
81 meter
Y = 105162
31 meter E =
0002929
Z = 5233429
25 I = 51
93575
XDOT = 878
946118 Wp = 266
69679
YDOT = -7604
756257 meter/sec RA = 101
63653 deg
ZDOT = 859
434223 TA = 175
15830
MA = 175
15547
Ha = 184
479 n
mi
Hp = 181
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13798943
55 X = -4232204
89
Y = 345020
69 feet Y = 57981
73 meter
Z = 17170043
46 Z = 5212932
65
XDOT = 2883
681489 XDOT = 959
743316
YDOT = -24949
987721 feet/sec YDOT = -7594
475720 meter/sec
ZDOT = 2819
666087 ZDOT = 863
899591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4747733
44 X = -1447109
15
Y = 13064849
45 feet Y = 3982166
11 meter
Z = 17091196
88 Z = 5209396
81
XDOT = -21232
134789 XDOT = -6471
554684
YDOT = -11424
826762 feet/sec YDOT = -3482
287197 meter/sec
ZDOT = 2836
132233 ZDOT = 864
453105
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 08152
54899768
00020000 00000-0 20000-3 0 9012
2 25544 51
6358 102
1769 0005985 285
0520 74
9982 15
76610118 25906
Satellite: ISS
Catalog Number: 25544
Epoch time: 08152
54899768 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 102
1769 deg
Eccentricity:
0005985
Arg of perigee: 285
0520 deg
Mean anomaly: 74
9982 deg
Mean motion: 15
76610118 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2590
Checksum: 320
Coasting Arc #3 (Orbit 2605)
---------------------------------------
Vector Time (GMT): 2008/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -857956
34 A = 6724762
81 meter
Y = 6661403
93 meter E =
0011103
Z = 126256
34 I = 51
98034
XDOT = -4694
112519 Wp = 18
14644
YDOT = -722
112504 meter/sec RA = 96
49690 deg
ZDOT = 6069
891799 TA = 343
22062
MA = 343
25732
Ha = 184
589 n
mi
Hp = 181
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2814817
38 X = -932994
78
Y = 21854999
78 feet Y = 6651390
19 meter
Z = 414226
85 Z = 121907
02
XDOT = -15400
631624 XDOT = -4715
175937
YDOT = -2369
135513 feet/sec YDOT = -774
723430 meter/sec
ZDOT = 19914
343172 ZDOT = 6047
036030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19500909
80 X = 5943877
31
Y = 10261180
58 feet Y = 3127607
84 meter
Z = 398103
64 Z = 121341
99
XDOT = -6881
776691 XDOT = -2097
565535
YDOT = 12291
912500 feet/sec YDOT = 3746
574930 meter/sec
ZDOT = 19826
339044 ZDOT = 6043
068141
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 08153
56315498
00020000 00000-0 20000-3 0 9029
2 25544 51
6358 96
9476 0005936 289
1490 70
9031 15
76610454 26060
Satellite: ISS
Catalog Number: 25544
Epoch time: 08153
56315498 = yrday
fracday
Element set: 902
Inclination: 51
6358 deg
RA of node: 96
9476 deg
Eccentricity:
0005936
Arg of perigee: 289
1490 deg
Mean anomaly: 70
9031 deg
Mean motion: 15
76610454 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2606
Checksum: 311
Coasting Arc #4 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2008/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4034331
89 A = 6713082
05 meter
Y = 1376487
69 meter E =
0008704
Z = -5193425
82 I = 51
94412
XDOT = -1083
803119 Wp = 88
95501
YDOT = 7534
119311 meter/sec RA = 91
35314 deg
ZDOT = 1156
769500 TA = 192
03481
MA = 192
05562
Ha = 184
806 n
mi
Hp = 181
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13235997
00 X = 4043869
17
Y = 4516035
72 feet Y = 1421656
17 meter
Z = -17038798
63 Z = -5173803
22
XDOT = -3555
784511 XDOT = -1173
589767
YDOT = 24718
239208 feet/sec YDOT = 7521
497369 meter/sec
ZDOT = 3795
175526 ZDOT = 1151
287565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8692506
69 X = 2649476
04
Y = -11072398
17 feet Y = -3374866
96 meter
Z = -16963171
29 Z = -5170374
61
XDOT = 21314
644217 XDOT = 6496
703557
YDOT = 10959
412907 feet/sec YDOT = 3340
429054 meter/sec
ZDOT = 3774
756297 ZDOT = 1150
545719
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 08154
51391710
00020000 00000-0 20000-3 0 9037
2 25544 51
6368 92
0457 0005999 293
2778 66
7754 15
76618722 26219
Satellite: ISS
Catalog Number: 25544
Epoch time: 08154
51391710 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 92
0457 deg
Eccentricity:
0005999
Arg of perigee: 293
2778 deg
Mean anomaly: 66
7754 deg
Mean motion: 15
76618722 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2621
Checksum: 318
Coasting Arc #5 (Orbit 2636)
---------------------------------------
Vector Time (GMT): 2008/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1049705
22 A = 6723144
85 meter
Y = -6369033
52 meter E =
0002993
Z = -1872758
28 I = 51
97882
XDOT = 4606
300579 Wp = 196
63633
YDOT = 2427
829273 meter/sec RA = 86
24761 deg
ZDOT = -5675
462568 TA = 4
07733
MA = 4
07489
Ha = 184
881 n
mi
Hp = 181
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3443914
78 X = 1129944
40
Y = -20895779
26 feet Y = -6356846
08 meter
Z = -6144220
09 Z = -1867465
19
XDOT = 15112
534709 XDOT = 4606
380647
YDOT = 7965
319137 feet/sec YDOT = 2479
341220 meter/sec
ZDOT = -18620
284017 ZDOT = -5653
084098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18723094
99 X = -5706799
35
Y = -9908729
29 feet Y = -3020180
69 meter
Z = -6124408
42 Z = -1866719
69
XDOT = 11646
746126 XDOT = 3549
928219
YDOT = -10552
864790 feet/sec YDOT = -3216
513188 meter/sec
ZDOT = -18533
954663 ZDOT = -5649
149381
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 08155
52805269
00020000 00000-0 20000-3 0 9049
2 25544 51
6379 86
8174 0005995 297
3928 62
6626 15
76643372 26375
Satellite: ISS
Catalog Number: 25544
Epoch time: 08155
52805269 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 86
8174 deg
Eccentricity:
0005995
Arg of perigee: 297
3928 deg
Mean anomaly: 62
6626 deg
Mean motion: 15
76643372 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2637
Checksum: 336
Coasting Arc #6 (Orbit 2652)
---------------------------------------
Vector Time (GMT): 2008/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4052456
97 A = 6715670
33 meter
Y = -2813800
92 meter E =
0007182
Z = 4557296
65 I = 51
95058
XDOT = 1347
276188 Wp = 22
81979
YDOT = -6933
464457 meter/sec RA = 81
07552 deg
ZDOT = -3074
801399 TA = 97
67644
MA = 97
59487
Ha = 185
086 n
mi
Hp = 181
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13295462
49 X = -4042830
11
Y = -9231630
33 feet Y = -2859065
03 meter
Z = 14951760
65 Z = 4537632
39
XDOT = 4420
197466 XDOT = 1439
644090
YDOT = -22747
586800 feet/sec YDOT = -6917
881287 meter/sec
ZDOT = -10087
931100 ZDOT = -3068
033496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12819326
78 X = -3907330
80
Y = 9996087
57 feet Y = 3046807
49 meter
Z = 14875838
20 Z = 4534155
48
XDOT = -19628
925502 XDOT = -5982
896493
YDOT = -10158
512320 feet/sec YDOT = -3096
314555 meter/sec
ZDOT = -10062
479733 ZDOT = -3067
043822
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 08156
54217750
00020000 00000-0 20000-3 0 9055
2 25544 51
6380 81
5894 0005991 301
2896 58
7681 15
76653450 26536
Satellite: ISS
Catalog Number: 25544
Epoch time: 08156
54217750 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 81
5894 deg
Eccentricity:
0005991
Arg of perigee: 301
2896 deg
Mean anomaly: 58
7681 deg
Mean motion: 15
76653450 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2653
Checksum: 313
Coasting Arc #7 (Orbit 2668)
---------------------------------------
Vector Time (GMT): 2008/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1350894
24 A = 6719533
98 meter
Y = 5621524
72 meter E =
0008304
Z = 3414406
36 I = 51
95831
XDOT = -4723
314117 Wp = 65
99969
YDOT = -3952
922633 meter/sec RA = 75
99002 deg
ZDOT = 4633
916807 TA = 334
21683
MA = 334
25819
Ha = 185
271 n
mi
Hp = 181
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4432067
73 X = -1430241
19
Y = 18443322
56 feet Y = 5605973
83 meter
Z = 11202120
60 Z = 3407652
24
XDOT = -15496
437392 XDOT = -4701
271600
YDOT = -12968
906277 feet/sec YDOT = -4005
619226 meter/sec
ZDOT = 15203
139131 ZDOT = 4611
023587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16412750
28 X = 5002606
29
Y = 9538977
49 feet Y = 2907480
34 meter
Z = 11176601
17 Z = 3406628
04
XDOT = -16158
139185 XDOT = -4925
000823
YDOT = 10071
061290 feet/sec YDOT = 3069
659481 meter/sec
ZDOT = 15114
685616 ZDOT = 4606
956176
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
55629108
00020000 00000-0 20000-3 0 9062
2 25544 51
6383 76
3602 0006025 305
5088 54
5514 15
76668040 26694
Satellite: ISS
Catalog Number: 25544
Epoch time: 08157
55629108 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 76
3602 deg
Eccentricity:
0006025
Arg of perigee: 305
5088 deg
Mean anomaly: 54
5514 deg
Mean motion: 15
76668040 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2669
Checksum: 298
Coasting Arc #8 (Orbit 2683)
---------------------------------------
Vector Time (GMT): 2008/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4204066
12 A = 6719532
66 meter
Y = 3988992
21 meter E =
0003823
Z = -3397095
43 I = 51
95068
XDOT = -1812
139448 Wp = 2
11514
YDOT = 5867
898389 meter/sec RA = 70
80490 deg
ZDOT = 4651
591510 TA = 317
93080
MA = 317
96015
Ha = 185
398 n
mi
Hp = 181
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13792867
84 X = 4175650
51
Y = 13087244
80 feet Y = 4035846
30 meter
Z = -11145326
22 Z = -3376740
38
XDOT = -5945
339397 XDOT = -1900
217001
YDOT = 19251
635133 feet/sec YDOT = 5847
140587 meter/sec
ZDOT = 15261
127000 ZDOT = 4642
575444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16310640
23 X = 4971483
14
Y = -9860532
94 feet Y = -3005490
44 meter
Z = -11066633
70 Z = -3373109
95
XDOT = 16224
314012 XDOT = 4945
170911
YDOT = 9762
241586 feet/sec YDOT = 2975
531235 meter/sec
ZDOT = 15226
916004 ZDOT = 4641
163998
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
50701210
00020000 00000-0 20000-3 0 9074
2 25544 51
6388 71
4582 0006057 308
8531 51
2092 15
76700749 26841
Satellite: ISS
Catalog Number: 25544
Epoch time: 08158
50701210 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 71
4582 deg
Eccentricity:
0006057
Arg of perigee: 308
8531 deg
Mean anomaly: 51
2092 deg
Mean motion: 15
76700749 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2684
Checksum: 287
Coasting Arc #9 (Orbit 2699)
---------------------------------------
Vector Time (GMT): 2008/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1889568
44 A = 6715322
33 meter
Y = -4539597
89 meter E =
0009384
Z = -4581842
42 I = 51
92646
XDOT = 4904
281736 Wp = 34
08758
YDOT = 5102
428333 meter/sec RA = 65
71808 deg
ZDOT = -3028
206892 TA = 205
90791
MA = 205
95492
Ha = 185
451 n
mi
Hp = 181
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6199371
54 X = 1962448
10
Y = -14893693
87 feet Y = -4518059
34 meter
Z = -15032291
42 Z = -4572486
76
XDOT = 16090
163176 XDOT = 4861
571449
YDOT = 16740
250437 feet/sec YDOT = 5157
032555 meter/sec
ZDOT = -9935
061981 ZDOT = -3004
484896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12846733
08 X = -3915684
24
Y = -9812533
63 feet Y = -2990860
25 meter
Z = -14996657
71 Z = -4570981
27
XDOT = 19533
058964 XDOT = 5953
676372
YDOT = -10506
026643 feet/sec YDOT = -3202
236921 meter/sec
ZDOT = -9843
309036 ZDOT = -3000
240594
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
52110394
00020000 00000-0 20000-3 0 9085
2 25544 51
6393 66
2294 0006113 313
3709 46
6946 15
76728212 27000
Satellite: ISS
Catalog Number: 25544
Epoch time: 08159
52110394 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 66
2294 deg
Eccentricity:
0006113
Arg of perigee: 313
3709 deg
Mean anomaly: 46
6946 deg
Mean motion: 15
76728212 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2700
Checksum: 287
Coasting Arc #10 (Orbit 2715)
---------------------------------------
Vector Time (GMT): 2008/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4336006
07 A = 6723109
78 meter
Y = -4807413
43 meter E =
0008796
Z = 1802451
23 I = 51
93878
XDOT = 2593
532181 Wp = 99
58421
YDOT = -4484
866097 meter/sec RA = 60
54307 deg
ZDOT = -5700
803107 TA = 60
49911
MA = 60
41141
Ha = 185
595 n
mi
Hp = 181
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14225741
69 X = -4290682
47
Y = -15772353
77 feet Y = -4855647
99 meter
Z = 5913553
90 Z = 1781496
41
XDOT = 8508
963849 XDOT = 2671
183168
YDOT = -14714
127615 feet/sec YDOT = -4455
428690 meter/sec
ZDOT = -18703
422266 ZDOT = -5688
015895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18666814
44 X = -5689645
04
Y = 10180434
83 feet Y = 3102996
54 meter
Z = 5832475
88 Z = 1777738
65
XDOT = -11552
286769 XDOT = -3521
137007
YDOT = -10452
957229 feet/sec YDOT = -3186
061363 meter/sec
ZDOT = -18654
570943 ZDOT = -5685
913223
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
53518575
00020000 00000-0 20000-3 0 9092
2 25544 51
6389 61
0001 0006069 316
4631 43
6054 15
76706836 27164
Satellite: ISS
Catalog Number: 25544
Epoch time: 08160
53518575 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 61
0001 deg
Eccentricity:
0006069
Arg of perigee: 316
4631 deg
Mean anomaly: 43
6054 deg
Mean motion: 15
76706836 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2716
Checksum: 288
Coasting Arc #11 (Orbit 2731)
---------------------------------------
Vector Time (GMT): 2008/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2706078
86 A = 6712580
19 meter
Y = 3266062
53 meter E =
0002931
Z = 5203171
05 I = 51
88871
XDOT = -4981
143176 Wp = 340
75286
YDOT = -5785
658611 meter/sec RA = 55
43090 deg
ZDOT = 1043
963052 TA = 99
34850
MA = 99
31535
Ha = 185
765 n
mi
Hp = 180
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8878211
50 X = -2767675
30
Y = 10715428
24 feet Y = 3235456
50 meter
Z = 17070771
18 Z = 5189875
81
XDOT = -16342
333255 XDOT = -4921
148178
YDOT = -18981
819590 feet/sec YDOT = -5841
025297 meter/sec
ZDOT = 3425
075631 ZDOT = 1019
909728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8514433
14 X = 2595199
22
Y = 11085263
78 feet Y = 3378788
40 meter
Z = 17019859
74 Z = 5187653
25
XDOT = -21269
568844 XDOT = -6482
964584
YDOT = 11235
585705 feet/sec YDOT = 3424
606523 meter/sec
ZDOT = 3331
986222 ZDOT = 1015
589401
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
54925453
00020000 00000-0 20000-3 0 9103
2 25544 51
6393 55
7705 0006206 320
1117 39
9591 15
76760726 27324
Satellite: ISS
Catalog Number: 25544
Epoch time: 08161
54925453 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 55
7705 deg
Eccentricity:
0006206
Arg of perigee: 320
1117 deg
Mean anomaly: 39
9591 deg
Mean motion: 15
76760726 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2732
Checksum: 289
Coasting Arc #12 (Orbit 2747)
---------------------------------------
Vector Time (GMT): 2008/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284367
02 A = 6724327
65 meter
Y = 5170692
77 meter E =
0014666
Z = 10685
34 I = 51
91102
XDOT = -3670
863723 Wp = 20
06876
YDOT = 3024
084937 meter/sec RA = 50
28385 deg
ZDOT = 6068
010915 TA = 340
04708
MA = 340
10437
Ha = 185
867 n
mi
Hp = 180
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14056322
23 X = 4226177
18
Y = 16964215
12 feet Y = 5218277
66 meter
Z = 35056
90 Z = 31358
06
XDOT = -12043
516151 XDOT = -3733
883945
YDOT = 9921
538508 feet/sec YDOT = 2982
682127 meter/sec
ZDOT = 19908
172293 ZDOT = 6050
025178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19432727
58 X = 5923095
37
Y = -10378914
90 feet Y = -3163493
26 meter
Z = 115076
98 Z = 35075
46
XDOT = 6532
865888 XDOT = 1991
217523
YDOT = 12478
467040 feet/sec YDOT = 3803
436754 meter/sec
ZDOT = 19839
180921 ZDOT = 6046
982345
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
56331397
00020000 00000-0 20000-3 0 9115
2 25544 51
6397 50
5409 0006326 324
0901 35
9838 15
76766795 27488
Satellite: ISS
Catalog Number: 25544
Epoch time: 08162
56331397 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 50
5409 deg
Eccentricity:
0006326
Arg of perigee: 324
0901 deg
Mean anomaly: 35
9838 deg
Mean motion: 15
76766795 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2748
Checksum: 315
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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