Date:
October 31st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3210)
---------------------------------------
Vector Time (GMT): 2007/303/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 331542
36 A = 6719027
03 meter
Y = 5221165
34 meter E =
0010152
Z = -4226796
82 I = 51
89313
XDOT = -5905
842835 Wp = 119
73123
YDOT = 3323
733320 meter/sec RA = 125
68648 deg
ZDOT = 3643
982837 TA = 187
26507
MA = 187
27979
Ha = 187
697 n
mi
Hp = 180
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1087737
39 X = 293667
26
Y = 17129807
54 feet Y = 5224661
36 meter
Z = -13867443
62 Z = -4225277
78
XDOT = -19376
124786 XDOT = -5960
272530
YDOT = 10904
636877 feet/sec YDOT = 3257
386254 meter/sec
ZDOT = 11955
324268 ZDOT = 3615
159727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2885850
38 X = -879607
20
Y = -16925216
19 feet Y = -5158805
89 meter
Z = -13861038
78 Z = -4224844
62
XDOT = 17011
253958 XDOT = 5185
030207
YDOT = -12597
720540 feet/sec YDOT = -3839
785221 meter/sec
ZDOT = 11846
067394 ZDOT = 3610
681342
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 07303
42101857
00020000 00000-0 20000-3 0 9000
2 25544 51
6369 126
5523 0002350 153
6818 206
4466 15
75893463 32114
Satellite: ISS
Catalog Number: 25544
Epoch time: 07303
42101857 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 126
5523 deg
Eccentricity:
0002350
Arg of perigee: 153
6818 deg
Mean anomaly: 206
4466 deg
Mean motion: 15
75893463 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3211
Checksum: 276
Coasting Arc #2 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2007/304/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4942457
30 A = 6720905
80 meter
Y = -2679804
36 meter E =
0006510
Z = -3687098
30 I = 51
91476
XDOT = 203
906131 Wp = 99
59198
YDOT = 6349
071160 meter/sec RA = 120
60628 deg
ZDOT = -4348
738392 TA = 124
57397
MA = 124
51253
Ha = 187
644 n
mi
Hp = 180
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16215411
07 X = 4989967
45
Y = -8792009
05 feet Y = -2624269
15 meter
Z = -12096779
20 Z = -3662972
25
XDOT = 668
983368 XDOT = 154
020393
YDOT = 20830
285957 feet/sec YDOT = 6351
072675 meter/sec
ZDOT = -14267
514409 ZDOT = -4347
868615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15133593
29 X = -4612719
23
Y = 10649794
06 feet Y = 3246057
23 meter
Z = -12005302
46 Z = -3659216
19
XDOT = -2422
507973 XDOT = -738
380430
YDOT = -19493
288216 feet/sec YDOT = -5941
554248 meter/sec
ZDOT = -14263
447709 ZDOT = -4347
498862
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 07304
43562405
00020000 00000-0 20000-3 0 9013
2 25544 51
6363 121
3270 0002287 158
5910 201
5350 15
75912743 32274
Satellite: ISS
Catalog Number: 25544
Epoch time: 07304
43562405 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 121
3270 deg
Eccentricity:
0002287
Arg of perigee: 158
5910 deg
Mean anomaly: 201
5350 deg
Mean motion: 15
75912743 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3227
Checksum: 259
Coasting Arc #3 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2007/305/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -84991
33 A = 6721738
12 meter
Y = -5845992
12 meter E =
0013498
Z = 3302633
31 I = 51
93286
XDOT = 5419
231716 Wp = 99
94509
YDOT = -2761
914544 meter/sec RA = 115
42416 deg
ZDOT = -4735
430537 TA = 41
39330
MA = 41
29111
Ha = 187
389 n
mi
Hp = 180
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -278842
96 X = -35658
03
Y = -19179764
18 feet Y = -5846666
83 meter
Z = 10835411
11 Z = 3302340
03
XDOT = 17779
631614 XDOT = 5472
717225
YDOT = -9061
399424 feet/sec YDOT = -2701
014399 meter/sec
ZDOT = -15536
189425 ZDOT = -4708
973785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2924517
62 X = 891392
97
Y = 18958574
66 feet Y = 5778573
56 meter
Z = 10833599
79 Z = 3302081
22
XDOT = -15098
428952 XDOT = -4602
001145
YDOT = 11175
848368 feet/sec YDOT = 3406
398582 meter/sec
ZDOT = -15435
843829 ZDOT = -4704
845199
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 07305
45020468
00020000 00000-0 20000-3 0 9025
2 25544 51
6371 116
1008 0002074 163
8449 196
2782 15
75999895 32434
Satellite: ISS
Catalog Number: 25544
Epoch time: 07305
45020468 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 116
1008 deg
Eccentricity:
0002074
Arg of perigee: 163
8449 deg
Mean anomaly: 196
2782 deg
Mean motion: 15
75999895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3243
Checksum: 301
Coasting Arc #4 (Orbit 3258)
---------------------------------------
Vector Time (GMT): 2007/306/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4529810
12 A = 6717833
72 meter
Y = 2064832
26 meter E =
0010360
Z = 4506106
45 I = 51
92920
XDOT = -41
184746 Wp = 122
11950
YDOT = -7025
421683 meter/sec RA = 110
34185 deg
ZDOT = 3167
200990 TA = 296
35775
MA = 296
46408
Ha = 187
518 n
mi
Hp = 180
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14861581
76 X = -4574452
82
Y = 6774384
05 feet Y = 2013927
67 meter
Z = 14783813
81 Z = 4483991
98
XDOT = -135
120559 XDOT = 21
991776
YDOT = -23049
283736 feet/sec YDOT = -7025
529050 meter/sec
ZDOT = 10391
079365 ZDOT = 3167
154251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13741759
14 X = 4188488
19
Y = -8966436
11 feet Y = -2732969
73 meter
Z = 14699902
09 Z = 4480530
16
XDOT = 3039
788739 XDOT = 926
527608
YDOT = 21750
206340 feet/sec YDOT = 6629
462893 meter/sec
ZDOT = 10390
067748 ZDOT = 3166
892650
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 07306
46476538
00020000 00000-0 20000-3 0 9031
2 25544 51
6358 110
8740 0002113 165
0694 195
0533 15
75965333 32591
Satellite: ISS
Catalog Number: 25544
Epoch time: 07306
46476538 = yrday
fracday
Element set: 903
Inclination: 51
6358 deg
RA of node: 110
8740 deg
Eccentricity:
0002113
Arg of perigee: 165
0694 deg
Mean anomaly: 195
0533 deg
Mean motion: 15
75965333 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3259
Checksum: 294
Coasting Arc #5 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2007/307/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 25030
98 A = 6724371
02 meter
Y = 6367551
96 meter E =
0005176
Z = -2160395
91 I = 51
96001
XDOT = -5002
717141 Wp = 61
65261
YDOT = 1894
308330 meter/sec RA = 105
16880 deg
ZDOT = 5537
692161 TA = 274
27148
MA = 274
33063
Ha = 187
275 n
mi
Hp = 180
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 82122
64 X = -35678
86
Y = 20890918
49 feet Y = 6367492
42 meter
Z = -7087913
09 Z = -2160421
78
XDOT = -16413
113979 XDOT = -5050
429223
YDOT = 6214
922344 feet/sec YDOT = 1838
098346 meter/sec
ZDOT = 18168
281367 ZDOT = 5513
272753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3649281
26 X = -1112300
93
Y = -20570105
70 feet Y = -6269768
22 meter
Z = -7087258
24 Z = -2160196
31
XDOT = 13728
007291 XDOT = 4184
296622
YDOT = -8649
248652 feet/sec YDOT = -2636
290989 meter/sec
ZDOT = 18075
572575 ZDOT = 5509
434521
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 07307
41589097
00020000 00000-0 20000-3 0 9043
2 25544 51
6350 105
9735 0002231 170
3081 189
8127 15
76028299 32741
Satellite: ISS
Catalog Number: 25544
Epoch time: 07307
41589097 = yrday
fracday
Element set: 904
Inclination: 51
6350 deg
RA of node: 105
9735 deg
Eccentricity:
0002231
Arg of perigee: 170
3081 deg
Mean anomaly: 189
8127 deg
Mean motion: 15
76028299 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3274
Checksum: 296
Coasting Arc #6 (Orbit 3289)
---------------------------------------
Vector Time (GMT): 2007/308/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247830
83 A = 6715184
64 meter
Y = -1171736
82 meter E =
0013575
Z = -5078984
42 I = 51
93497
XDOT = 27
887178 Wp = 86
52054
YDOT = 7501
660093 meter/sec RA = 100
07254 deg
ZDOT = -1710
423946 TA = 167
09618
MA = 167
06141
Ha = 187
220 n
mi
Hp = 180
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13936452
85 X = 4285290
85
Y = -3844280
92 feet Y = -1124025
79 meter
Z = -16663334
72 Z = -5058257
12
XDOT = 91
493366 XDOT = -47
690524
YDOT = 24611
745711 feet/sec YDOT = 7501
549345 meter/sec
ZDOT = -5611
627119 ZDOT = -1710
472145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13071186
17 X = -3984097
55
Y = 6384783
29 feet Y = 1946081
95 meter
Z = -16584588
40 Z = -5054982
54
XDOT = -4229
554987 XDOT = -1289
168360
YDOT = -23206
923095 feet/sec YDOT = -7073
470160 meter/sec
ZDOT = -5610
927538 ZDOT = -1710
210714
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 07308
43040285
00020000 00000-0 20000-3 0 9058
2 25544 51
6343 100
7469 0002211 170
8689 189
2516 15
76067379 32903
Satellite: ISS
Catalog Number: 25544
Epoch time: 07308
43040285 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 100
7469 deg
Eccentricity:
0002211
Arg of perigee: 170
8689 deg
Mean anomaly: 189
2516 deg
Mean motion: 15
76067379 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3290
Checksum: 293
Coasting Arc #7 (Orbit 3305)
---------------------------------------
Vector Time (GMT): 2007/309/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -48480
67 A = 6725789
93 meter
Y = -6670838
74 meter E =
0014779
Z = 793562
86 I = 51
97585
XDOT = 4775
695191 Wp = 132
46889
YDOT = -755
886503 meter/sec RA = 94
92098 deg
ZDOT = -6001
871139 TA = 38
90703
MA = 38
80075
Ha = 186
951 n
mi
Hp = 180
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -159057
31 X = 22262
20
Y = -21885953
86 feet Y = -6670985
32 meter
Z = 2603552
68 Z = 793499
29
XDOT = 15668
291310 XDOT = 4812
949294
YDOT = -2479
942595 feet/sec YDOT = -702
273779 meter/sec
ZDOT = -19691
178276 ZDOT = -5978
579828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4607004
76 X = 1404215
05
Y = 21396287
04 feet Y = 6521588
29 meter
Z = 2602531
49 Z = 793251
60
XDOT = -13388
327190 XDOT = -4080
762128
YDOT = 5291
257418 feet/sec YDOT = 1612
775261 meter/sec
ZDOT = -19602
622539 ZDOT = -5974
879350
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 07309
44488818
00020000 00000-0 20000-3 0 9069
2 25544 51
6348 95
5198 0001902 178
5909 181
5261 15
76152753 33065
Satellite: ISS
Catalog Number: 25544
Epoch time: 07309
44488818 = yrday
fracday
Element set: 906
Inclination: 51
6348 deg
RA of node: 95
5198 deg
Eccentricity:
0001902
Arg of perigee: 178
5909 deg
Mean anomaly: 181
5261 deg
Mean motion: 15
76152753 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3306
Checksum: 316
Coasting Arc #8 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2007/310/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4137541
35 A = 6714137
28 meter
Y = 121062
87 meter E =
0003443
Z = 5284237
59 I = 51
93649
XDOT = -101
315916 Wp = 132
45159
YDOT = -7705
700944 meter/sec RA = 89
79920 deg
ZDOT = 94
895580 TA = 316
63879
MA = 316
66587
Ha = 187
227 n
mi
Hp = 180
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13574610
71 X = -4164258
09
Y = 397187
90 feet Y = 74645
23 meter
Z = 17336737
49 Z = 5264072
01
XDOT = -332
401298 XDOT = -15
603072
YDOT = -25281
171076 feet/sec YDOT = -7706
354670 meter/sec
ZDOT = 311
337205 ZDOT = 94
611676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13251306
00 X = 4038998
07
Y = -3389022
59 feet Y = -1032974
08 meter
Z = 17260002
79 Z = 5260848
85
XDOT = 5629
143055 XDOT = 1715
762803
YDOT = 23624
728835 feet/sec YDOT = 7200
817349 meter/sec
ZDOT = 309
365935 ZDOT = 94
294737
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 07310
45935357
00020000 00000-0 20000-3 0 9078
2 25544 51
6341 90
2922 0002133 175
7831 184
3352 15
76094264 33227
Satellite: ISS
Catalog Number: 25544
Epoch time: 07310
45935357 = yrday
fracday
Element set: 907
Inclination: 51
6341 deg
RA of node: 90
2922 deg
Eccentricity:
0002133
Arg of perigee: 175
7831 deg
Mean anomaly: 184
3352 deg
Mean motion: 15
76094264 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3322
Checksum: 277
Coasting Arc #9 (Orbit 3337)
---------------------------------------
Vector Time (GMT): 2007/311/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 117564
93 A = 6725793
08 meter
Y = 6688886
80 meter E =
0012078
Z = 644257
16 I = 51
97578
XDOT = -4777
149722 Wp = 59
74262
YDOT = -503
593722 meter/sec RA = 84
67429 deg
ZDOT = 6023
000605 TA = 307
24687
MA = 307
35698
Ha = 186
899 n
mi
Hp = 180
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 385711
71 X = 39630
27
Y = 21945166
66 feet Y = 6689765
72 meter
Z = 2113704
58 Z = 644638
99
XDOT = -15673
063391 XDOT = -4800
422913
YDOT = -1652
210375 feet/sec YDOT = -557
144638 meter/sec
ZDOT = 19760
500673 ZDOT = 5999
736002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5548660
43 X = -1691231
70
Y = -21235397
49 feet Y = -6472549
15 meter
Z = 2115920
92 Z = 644932
70
XDOT = 14179
060389 XDOT = 4321
777607
YDOT = -1719
541806 feet/sec YDOT = -524
116343 meter/sec
ZDOT = 19671
898796 ZDOT = 5995
994753
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 07311
47378937
00020000 00000-0 20000-3 0 9087
2 25544 51
6347 85
0646 0002183 181
4612 178
6546 15
76185127 33381
Satellite: ISS
Catalog Number: 25544
Epoch time: 07311
47378937 = yrday
fracday
Element set: 908
Inclination: 51
6347 deg
RA of node: 85
0646 deg
Eccentricity:
0002183
Arg of perigee: 181
4612 deg
Mean anomaly: 178
6546 deg
Mean motion: 15
76185127 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3338
Checksum: 310
Coasting Arc #10 (Orbit 3352)
---------------------------------------
Vector Time (GMT): 2007/312/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4254652
52 A = 6714629
28 meter
Y = 1007885
30 meter E =
0014279
Z = -5108487
88 I = 51
93521
XDOT = 126
301474 Wp = 110
49384
YDOT = 7526
881155 meter/sec RA = 79
52478 deg
ZDOT = 1588
884006 TA = 174
72047
MA = 174
70540
Ha = 186
824 n
mi
Hp = 180
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13958833
72 X = 4267882
88
Y = 3306710
30 feet Y = 1055537
29 meter
Z = -16760130
84 Z = -5087785
96
XDOT = 414
374916 XDOT = 34
406606
YDOT = 24694
491977 feet/sec YDOT = 7527
779693 meter/sec
ZDOT = 5212
874034 ZDOT = 1589
274500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14432445
75 X = -4399009
47
Y = 355788
99 feet Y = 108444
48 meter
Z = -16681225
41 Z = -5084437
51
XDOT = -6593
508155 XDOT = -2009
701286
YDOT = -22741
437762 feet/sec YDOT = -6931
590230 meter/sec
ZDOT = 5215
205883 ZDOT = 1589
594753
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 07312
42480200
00020000 00000-0 20000-3 0 9091
2 25544 51
6355 80
1644 0002150 181
9715 178
1441 15
76217358 33535
Satellite: ISS
Catalog Number: 25544
Epoch time: 07312
42480200 = yrday
fracday
Element set: 909
Inclination: 51
6355 deg
RA of node: 80
1644 deg
Eccentricity:
0002150
Arg of perigee: 181
9715 deg
Mean anomaly: 178
1441 deg
Mean motion: 15
76217358 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3353
Checksum: 268
Coasting Arc #11 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2007/313/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -59554
20 A = 6723743
56 meter
Y = -6378733
80 meter E =
0007821
Z = -2115591
85 I = 51
96042
XDOT = 5017
840477 Wp = 149
17498
YDOT = 1792
927742 meter/sec RA = 74
42578 deg
ZDOT = -5562
670710 TA = 54
38370
MA = 54
31087
Ha = 186
661 n
mi
Hp = 180
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -195387
79 X = 22055
70
Y = -20927604
35 feet Y = -6378943
39 meter
Z = -6940918
15 Z = -2115683
17
XDOT = 16462
731224 XDOT = 5024
442104
YDOT = 5882
308866 feet/sec YDOT = 1849
077188 meter/sec
ZDOT = -18250
231988 ZDOT = -5538
277121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5792048
93 X = 1765416
52
Y = 20110702
61 feet Y = 6129742
16 meter
Z = -6941970
50 Z = -2115912
61
XDOT = -16071
261174 XDOT = -4898
520406
YDOT = -1621
376441 feet/sec YDOT = -494
195539 meter/sec
ZDOT = -18157
188623 ZDOT = -5534
311092
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 07313
43918997
00020000 00000-0 20000-3 0 9104
2 25544 51
6358 74
9369 0001924 186
4268 173
6871 15
76279709 33696
Satellite: ISS
Catalog Number: 25544
Epoch time: 07313
43918997 = yrday
fracday
Element set: 910
Inclination: 51
6358 deg
RA of node: 74
9369 deg
Eccentricity:
0001924
Arg of perigee: 186
4268 deg
Mean anomaly: 173
6871 deg
Mean motion: 15
76279709 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3369
Checksum: 342
Coasting Arc #12 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2007/314/09:52:44
280
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4543092
69 A = 6717041
09 meter
Y = -2073151
49 meter E =
0008149
Z = 4486224
75 I = 51
92869
XDOT = 28
433654 Wp = 80
05229
YDOT = -7010
291924 meter/sec RA = 69
25188 deg
ZDOT = -3204
498961 TA = 41
85527
MA = 41
79299
Ha = 186
777 n
mi
Hp = 180
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14905159
76 X = -4541366
74
Y = -6801678
12 feet Y = -2123945
53 meter
Z = 14718585
14 Z = 4464157
74
XDOT = 93
286268 XDOT = 122
389080
YDOT = -22999
645421 feet/sec YDOT = -7009
448451 meter/sec
ZDOT = -10513
448035 ZDOT = -3204
132996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16307313
56 X = 4970469
17
Y = 2229392
42 feet Y = 679518
81 meter
Z = 14634366
91 Z = 4460555
03
XDOT = 6596
611184 XDOT = 2010
647089
YDOT = 20892
717371 feet/sec YDOT = 6368
100255 meter/sec
ZDOT = -10512
816548 ZDOT = -3204
306484
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 07314
45355465
00020000 00000-0 20000-3 0 9113
2 25544 51
6360 69
7096 0002050 188
9574 171
1554 15
76268570 33859
Satellite: ISS
Catalog Number: 25544
Epoch time: 07314
45355465 = yrday
fracday
Element set: 911
Inclination: 51
6360 deg
RA of node: 69
7096 deg
Eccentricity:
0002050
Arg of perigee: 188
9574 deg
Mean anomaly: 171
1554 deg
Mean motion: 15
76268570 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3385
Checksum: 304
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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