Date:
November 28th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 3638)
---------------------------------------
Vector Time (GMT): 2007/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5915942
45 A = 6720446
90 meter
Y = 1038589
49 meter E =
0012656
Z = 3002618
05 I = 51
57104
XDOT = -3373
821054 Wp = 86
03570
YDOT = 4845
403064 meter/sec RA = 346
58965 deg
ZDOT = 4954
314371 TA = 308
76947
MA = 308
88248
Ha = 185
697 n
mi
Hp = 179
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19409260
01 X = 5889302
68
Y = 3407445
82 feet Y = 1104595
46 meter
Z = 9851109
10 Z = 3031293
64
XDOT = -11068
966712 XDOT = -3451
819891
YDOT = 15896
991680 feet/sec YDOT = 4807
238161 meter/sec
ZDOT = 16254
312242 ZDOT = 4937
735407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11463985
56 X = -3494222
80
Y = 15960631
17 feet Y = 4864800
38 meter
Z = 9960406
58 Z = 3035931
93
XDOT = -8319
814433 XDOT = -2535
879439
YDOT = -16114
831133 feet/sec YDOT = -4911
800529 meter/sec
ZDOT = 16191
641417 ZDOT = 4935
212304
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 07330
55718527
00020000 00000-0 20000-3 0 9002
2 25544 51
6399 346
7630 0000765 222
2507 137
8599 15
76715116 36395
Satellite: ISS
Catalog Number: 25544
Epoch time: 07330
55718527 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 346
7630 deg
Eccentricity:
0000765
Arg of perigee: 222
2507 deg
Mean anomaly: 137
8599 deg
Mean motion: 15
76715116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3639
Checksum: 309
Coasting Arc #2 (Orbit 3653)
---------------------------------------
Vector Time (GMT): 2007/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3558907
21 A = 6718344
25 meter
Y = -4319583
36 meter E =
0005404
Z = -3722240
10 I = 51
53711
XDOT = 6240
005585 Wp = 108
18128
YDOT = 1470
649912 meter/sec RA = 341
37650 deg
ZDOT = 4262
923230 TA = 206
80819
MA = 206
83613
Ha = 185
657 n
mi
Hp = 179
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11676204
76 X = 3625027
09
Y = -14171861
43 feet Y = -4279415
39 meter
Z = -12212073
83 Z = -3704790
81
XDOT = 20472
459268 XDOT = 6202
388070
YDOT = 4824
966904 feet/sec YDOT = 1540
218208 meter/sec
ZDOT = 13985
968603 ZDOT = 4293
146333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7962401
34 X = 2426939
93
Y = 16594702
95 feet Y = 5058065
46 meter
Z = -12146034
75 Z = -3702111
39
XDOT = -11700
097120 XDOT = -3566
189602
YDOT = 15926
698245 feet/sec YDOT = 4854
457625 meter/sec
ZDOT = 14101
208978 ZDOT = 4298
048496
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 07331
50786576
00020000 00000-0 20000-3 0 9018
2 25544 51
6408 341
8610 0000779 230
6482 129
4613 15
76764199 36546
Satellite: ISS
Catalog Number: 25544
Epoch time: 07331
50786576 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 341
8610 deg
Eccentricity:
0000779
Arg of perigee: 230
6482 deg
Mean anomaly: 129
4613 deg
Mean motion: 15
76764199 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3654
Checksum: 306
Coasting Arc #3 (Orbit 3669)
---------------------------------------
Vector Time (GMT): 2007/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4880939
02 A = 6715916
11 meter
Y = -1615303
60 meter E =
0008321
Z = -4329350
99 I = 51
50145
XDOT = 4702
580001 Wp = 70
41684
YDOT = -5042
353487 meter/sec RA = 336
26119 deg
ZDOT = -3422
971876 TA = 164
97240
MA = 164
94766
Ha = 185
544 n
mi
Hp = 179
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16013579
45 X = -4841482
36
Y = -5299552
51 feet Y = -1669663
85 meter
Z = -14203907
45 Z = -4352967
10
XDOT = 15428
412078 XDOT = 4775
243127
YDOT = -16543
154484 feet/sec YDOT = -4989
359845 meter/sec
ZDOT = -11230
222690 ZDOT = -3399
950769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11263825
44 X = 3433214
00
Y = -12453055
39 feet Y = -3795691
28 meter
Z = -14294006
38 Z = -4356813
14
XDOT = 8001
510072 XDOT = 2438
860270
YDOT = 20018
053212 feet/sec YDOT = 6101
502619 meter/sec
ZDOT = -11143
031945 ZDOT = -3396
396137
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 07332
52189797
00020000 00000-0 20000-3 0 9024
2 25544 51
6397 336
6312 0000792 233
0526 127
0567 15
76811574 36705
Satellite: ISS
Catalog Number: 25544
Epoch time: 07332
52189797 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 336
6312 deg
Eccentricity:
0000792
Arg of perigee: 233
0526 deg
Mean anomaly: 127
0567 deg
Mean motion: 15
76811574 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3670
Checksum: 301
Coasting Arc #4 (Orbit 3685)
---------------------------------------
Vector Time (GMT): 2007/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4537887
53 A = 6722040
09 meter
Y = 4461056
54 meter E =
0013620
Z = 2145760
08 I = 51
49590
XDOT = -4879
280907 Wp = 111
57289
YDOT = -2304
894505 meter/sec RA = 331
04999 deg
ZDOT = -5503
945517 TA = 44
32874
MA = 44
21976
Ha = 185
480 n
mi
Hp = 179
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14888082
45 X = -4597858
23
Y = 14636012
28 feet Y = 4409975
77 meter
Z = 7039895
29 Z = 2123569
74
XDOT = -16008
139460 XDOT = -4826
407307
YDOT = -7561
989846 feet/sec YDOT = -2359
161171 meter/sec
ZDOT = -18057
564033 ZDOT = -5527
520980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7725984
69 X = -2354880
13
Y = -19425596
48 feet Y = -5920921
81 meter
Z = 6955813
55 Z = 2120131
97
XDOT = 11707
378204 XDOT = 3568
408877
YDOT = -11181
740154 feet/sec YDOT = -3408
194399 meter/sec
ZDOT = -18147
580093 ZDOT = -5531
382412
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 07333
53590105
00020000 00000-0 20000-3 0 9036
2 25544 51
6392 331
4016 0000682 244
9679 115
1415 15
76879195 36862
Satellite: ISS
Catalog Number: 25544
Epoch time: 07333
53590105 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 331
4016 deg
Eccentricity:
0000682
Arg of perigee: 244
9679 deg
Mean anomaly: 115
1415 deg
Mean motion: 15
76879195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3686
Checksum: 300
Coasting Arc #5 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2007/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3584972
29 A = 6712495
64 meter
Y = 2483702
32 meter E =
0004087
Z = 5100693
84 I = 51
43853
XDOT = -5573
205049 Wp = 134
06109
YDOT = 5132
976132 meter/sec RA = 325
91137 deg
ZDOT = 1414
149593 TA = 302
34879
MA = 302
38835
Ha = 185
306 n
mi
Hp = 179
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11761720
12 X = 3532154
35
Y = 8148629
65 feet Y = 2523495
75 meter
Z = 16734559
84 Z = 5117981
64
XDOT = -18284
793468 XDOT = -5637
058269
YDOT = 16840
472873 feet/sec YDOT = 5070
296252 meter/sec
ZDOT = 4639
598403 ZDOT = 1386
920165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11893296
54 X = -3625076
79
Y = 7814819
47 feet Y = 2381956
97 meter
Z = 16800649
17 Z = 5120837
87
XDOT = -8282
276770 XDOT = -2524
437959
YDOT = -22381
851541 feet/sec YDOT = -6821
988350 meter/sec
ZDOT = 4536
392916 ZDOT = 1382
692561
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 07334
54987592
00020000 00000-0 20000-3 0 9049
2 25544 51
6385 326
1718 0000743 247
9601 112
1485 15
76893791 37021
Satellite: ISS
Catalog Number: 25544
Epoch time: 07334
54987592 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 326
1718 deg
Eccentricity:
0000743
Arg of perigee: 247
9601 deg
Mean anomaly: 112
1485 deg
Mean motion: 15
76893791 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3702
Checksum: 312
Coasting Arc #6 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2007/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5062346
56 A = 6723646
63 meter
Y = -4409170
36 meter E =
0011064
Z = -261902
02 I = 51
45362
XDOT = 3328
621406 Wp = 42
19745
YDOT = 3473
367893 meter/sec RA = 320
72624 deg
ZDOT = 6019
319920 TA = 314
94554
MA = 315
03522
Ha = 185
299 n
mi
Hp = 179
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16608748
55 X = 5112546
61
Y = -14465782
03 feet Y = -4352279
63 meter
Z = -859258
60 Z = -237187
33
XDOT = 10920
673904 XDOT = 3260
293305
YDOT = 11395
563954 feet/sec YDOT = 3510
207960 meter/sec
ZDOT = 19748
424936 ZDOT = 6035
324758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7632506
06 X = 2326387
85
Y = 20664134
82 feet Y = 6298428
29 meter
Z = -765563
39 Z = -233343
72
XDOT = -12981
731311 XDOT = -3956
831704
YDOT = 5507
742045 feet/sec YDOT = 1678
759775 meter/sec
ZDOT = 19809
728128 ZDOT = 6038
005133
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 07335
50044989
00020000 00000-0 20000-3 0 9051
2 25544 51
6384 321
2697 0000751 234
1428 125
9667 15
76992691 37175
Satellite: ISS
Catalog Number: 25544
Epoch time: 07335
50044989 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 321
2697 deg
Eccentricity:
0000751
Arg of perigee: 234
1428 deg
Mean anomaly: 125
9667 deg
Mean motion: 15
76992691 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3717
Checksum: 318
Coasting Arc #7 (Orbit 3732)
---------------------------------------
Vector Time (GMT): 2007/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2224238
03 A = 6711909
47 meter
Y = -3633441
39 meter E =
0013999
Z = -5198730
93 I = 51
39170
XDOT = 5916
093776 Wp = 97
51548
YDOT = -4846
419250 meter/sec RA = 315
54682 deg
ZDOT = 856
214049 TA = 180
66927
MA = 180
67114
Ha = 185
287 n
mi
Hp = 179
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7297368
88 X = -2158188
26
Y = -11920739
48 feet Y = -3657944
45 meter
Z = -17056203
85 Z = -5209376
19
XDOT = 19409
756483 XDOT = 5965
688094
YDOT = -15900
325625 feet/sec YDOT = -4779
984894 meter/sec
ZDOT = 2809
101211 ZDOT = 885
074911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13654732
29 X = 4161962
40
Y = -2739849
05 feet Y = -835105
99 meter
Z = -17097111
60 Z = -5211199
62
XDOT = 8195
566570 XDOT = 2498
008690
YDOT = 22635
830168 feet/sec YDOT = 6899
401035 meter/sec
ZDOT = 2918
541282 ZDOT = 889
571383
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 07336
51436754
00020000 00000-0 20000-3 0 9069
2 25544 51
6380 316
0389 0000707 258
0225 102
0860 15
76971018 37331
Satellite: ISS
Catalog Number: 25544
Epoch time: 07336
51436754 = yrday
fracday
Element set: 906
Inclination: 51
6380 deg
RA of node: 316
0389 deg
Eccentricity:
0000707
Arg of perigee: 258
0225 deg
Mean anomaly: 102
0860 deg
Mean motion: 15
76971018 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3733
Checksum: 282
Coasting Arc #8 (Orbit 3748)
---------------------------------------
Vector Time (GMT): 2007/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5167459
48 A = 6722160
38 meter
Y = 3924793
70 meter E =
0007099
Z = -1744254
43 I = 51
40741
XDOT = -1797
307353 Wp = 146
11093
YDOT = -4883
419830 meter/sec RA = 310
39485 deg
ZDOT = -5680
562708 TA = 53
28682
MA = 53
22163
Ha = 185
155 n
mi
Hp = 179
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16953607
22 X = -5202489
66
Y = 12876619
76 feet Y = 3866812
49 meter
Z = -5722619
52 Z = -1769443
16
XDOT = -5896
677668 XDOT = -1714
971071
YDOT = -16021
718602 feet/sec YDOT = -4903
057606 meter/sec
ZDOT = -18637
016760 ZDOT = -5689
094478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6735258
11 X = -2052906
67
Y = -20168435
29 feet Y = -6147339
08 meter
Z = -5818163
35 Z = -1773376
19
XDOT = 15562
630599 XDOT = 4743
489807
YDOT = 173
035090 feet/sec YDOT = 52
741095 meter/sec
ZDOT = -18670
000969 ZDOT = -5690
616295
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 07337
52825527
00020000 00000-0 20000-3 0 9072
2 25544 51
6381 310
8082 0000667 269
0422 91
0666 15
77041997 37493
Satellite: ISS
Catalog Number: 25544
Epoch time: 07337
52825527 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 310
8082 deg
Eccentricity:
0000667
Arg of perigee: 269
0422 deg
Mean anomaly: 91
0666 deg
Mean motion: 15
77041997 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3749
Checksum: 307
Coasting Arc #9 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2007/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 973851
70 A = 6714495
63 meter
Y = 4874704
28 meter E =
0008050
Z = 4509300
40 I = 51
36362
XDOT = -5825
495160 Wp = 63
63815
YDOT = 4008
665412 meter/sec RA = 305
17827 deg
ZDOT = -3067
652617 TA = 57
03021
MA = 56
95285
Ha = 185
038 n
mi
Hp = 179
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3195051
52 X = 897363
87
Y = 15993124
29 feet Y = 4885166
44 meter
Z = 14794292
64 Z = 4513846
03
XDOT = -19112
516930 XDOT = -5854
985321
YDOT = 13151
789411 feet/sec YDOT = 3943
356764 meter/sec
ZDOT = -10064
477090 ZDOT = -3096
024735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16178084
92 X = -4931080
28
Y = -1931553
71 feet Y = -588737
57 meter
Z = 14812094
45 Z = 4514726
39
XDOT = -6830
897041 XDOT = -2082
057418
YDOT = -20986
070898 feet/sec YDOT = -6396
554410 meter/sec
ZDOT = -10172
136628 ZDOT = -3100
467244
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 07338
54211303
00020000 00000-0 20000-3 0 9087
2 25544 51
6377 305
5778 0000793 273
2890 86
8184 15
77088768 37659
Satellite: ISS
Catalog Number: 25544
Epoch time: 07338
54211303 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 305
5778 deg
Eccentricity:
0000793
Arg of perigee: 273
2890 deg
Mean anomaly: 86
8184 deg
Mean motion: 15
77088768 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3765
Checksum: 328
Coasting Arc #10 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2007/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4925772
08 A = 6717724
83 meter
Y = -2914576
73 meter E =
0011382
Z = 3507928
42 I = 51
36037
XDOT = 509
305505 Wp = 93
29090
YDOT = 6258
319793 meter/sec RA = 300
04868 deg
ZDOT = 4471
499291 TA = 308
70040
MA = 308
80213
Ha = 184
855 n
mi
Hp = 179
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16160669
54 X = 4940955
98
Y = -9562259
61 feet Y = -2859409
37 meter
Z = 11508951
51 Z = 3531894
95
XDOT = 1670
949819 XDOT = 417
563978
YDOT = 20532
545252 feet/sec YDOT = 6263
501778 meter/sec
ZDOT = 14670
273264 ZDOT = 4473
751271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4491726
20 X = 1369078
14
Y = 18174865
80 feet Y = 5539699
10 meter
Z = 11599942
34 Z = 3535662
43
XDOT = -18787
385760 XDOT = -5726
395180
YDOT = -4753
140785 feet/sec YDOT = -1448
757311 meter/sec
ZDOT = 14679
477446 ZDOT = 4474
304726
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 07339
55593984
00020000 00000-0 20000-3 0 9098
2 25544 51
6384 300
3474 0000842 265
0264 95
0804 15
77167270 37817
Satellite: ISS
Catalog Number: 25544
Epoch time: 07339
55593984 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 300
3474 deg
Eccentricity:
0000842
Arg of perigee: 265
0264 deg
Mean anomaly: 95
0804 deg
Mean motion: 15
77167270 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3781
Checksum: 307
Coasting Arc #11 (Orbit 3795)
---------------------------------------
Vector Time (GMT): 2007/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 12596
78 A = 6718977
80 meter
Y = -5955886
12 meter E =
0003872
Z = -3111663
31 I = 51
35090
XDOT = 5432
083644 Wp = 71
17503
YDOT = -2516
413118 meter/sec RA = 294
81697 deg
ZDOT = 4844
677558 TA = 252
46051
MA = 252
50282
Ha = 184
980 n
mi
Hp = 179
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 41328
02 X = 94311
70
Y = -19540308
79 feet Y = -5955288
02 meter
Z = -10208869
13 Z = -3111404
28
XDOT = 17821
796731 XDOT = 5436
283741
YDOT = -8255
948550 feet/sec YDOT = -2455
645527 meter/sec
ZDOT = 15894
611410 ZDOT = 4871
077136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18770658
99 X = 5721296
86
Y = 5430996
34 feet Y = 1655367
69 meter
Z = -10208478
06 Z = -3111544
11
XDOT = 3496
226608 XDOT = 1065
649870
YDOT = 17943
585632 feet/sec YDOT = 5469
204901 meter/sec
ZDOT = 15994
912139 ZDOT = 4875
249220
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 07340
50637772
00020000 00000-0 20000-3 0 9101
2 25544 51
6383 295
4430 0000759 283
4253 76
6827 15
77157239 37961
Satellite: ISS
Catalog Number: 25544
Epoch time: 07340
50637772 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 295
4430 deg
Eccentricity:
0000759
Arg of perigee: 283
4253 deg
Mean anomaly: 76
6827 deg
Mean motion: 15
77157239 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3796
Checksum: 314
Coasting Arc #12 (Orbit 3811)
---------------------------------------
Vector Time (GMT): 2007/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4536974
91 A = 6712977
52 meter
Y = 1334886
03 meter E =
0011187
Z = -4774787
50 I = 51
32119
XDOT = 481
780194 Wp = 69
89753
YDOT = -7267
131105 meter/sec RA = 289
67976 deg
ZDOT = -2490
380666 TA = 175
62245
MA = 175
61266
Ha = 184
871 n
mi
Hp = 178
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14885088
28 X = -4528369
05
Y = 4379547
33 feet Y = 1284199
74 meter
Z = -15665313
31 Z = -4796807
53
XDOT = 1580
643680 XDOT = 575
104631
YDOT = -23842
293650 feet/sec YDOT = -7261
221439 meter/sec
ZDOT = -8170
540243 ZDOT = -2487
814378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -438057
43 X = -133519
90
Y = -15424775
46 feet Y = -4701471
56 meter
Z = -15749055
11 Z = -4800312
00
XDOT = 21502
746110 XDOT = 6554
037014
YDOT = 7719
316683 feet/sec YDOT = 2352
847725 meter/sec
ZDOT = -8161
490441 ZDOT = -2487
622286
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 07341
52014765
00020000 00000-0 20000-3 0 9116
2 25544 51
6391 290
2116 0000778 284
5037 75
6042 15
77223680 38128
Satellite: ISS
Catalog Number: 25544
Epoch time: 07341
52014765 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 290
2116 deg
Eccentricity:
0000778
Arg of perigee: 284
5037 deg
Mean anomaly: 75
6042 deg
Mean motion: 15
77223680 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3812
Checksum: 276
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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