Date:
December 6th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 2010)
---------------------------------------
Vector Time (GMT): 2006/338/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2114615
55 A = 6720491
52 meter
Y = 4785877
21 meter E =
0014562
Z = 4222760
32 I = 51
77131
XDOT = -6780
388493 Wp = 303
96538
YDOT = -199
932744 meter/sec RA = 26
68608 deg
ZDOT = 3638
855829 TA = 109
11673
MA = 108
95900
Ha = 191
470 n
mi
Hp = 179
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6937715
04 X = 2040428
24
Y = 15701696
87 feet Y = 4809108
49 meter
Z = 13854200
52 Z = 4232853
93
XDOT = -22245
369073 XDOT = -6795
326115
YDOT = -655
947324 feet/sec YDOT = -275
838950 meter/sec
ZDOT = 11938
503377 ZDOT = 3605
879758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16192857
55 X = 4935582
98
Y = 5603973
02 feet Y = 1708090
98 meter
Z = 13892476
29 Z = 4234426
77
XDOT = -15201
956825 XDOT = -4633
556440
YDOT = 14773
026742 feet/sec YDOT = 4502
818551 meter/sec
ZDOT = 11815
199578 ZDOT = 3601
272832
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 06338
98305627
00020000 00000-0 20000-3 0 9009
2 25544 51
6356 26
8881 0024320 297
4594 62
4097 15
75365135 20115
Satellite: ISS
Catalog Number: 25544
Epoch time: 06338
98305627 = yrday
fracday
Element set: 900
Inclination: 51
6356 deg
RA of node: 26
8881 deg
Eccentricity:
0024320
Arg of perigee: 297
4594 deg
Mean anomaly: 62
4097 deg
Mean motion: 15
75365135 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2011
Checksum: 296
Coasting Arc #2 (Orbit 2025)
---------------------------------------
Vector Time (GMT): 2006/339/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6107722
80 A = 6724867
16 meter
Y = 52475
57 meter E =
0022624
Z = -2778662
93 I = 51
76047
XDOT = 2301
992353 Wp = 311
50123
YDOT = 5266
479057 meter/sec RA = 21
50035 deg
ZDOT = 5147
347308 TA = 16
68136
MA = 16
60706
Ha = 191
766 n
mi
Hp = 178
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20038460
64 X = 6120180
48
Y = 172163
95 feet Y = 120845
67 meter
Z = -9116348
19 Z = -2748960
96
XDOT = 7552
468350 XDOT = 2217
925566
YDOT = 17278
474597 feet/sec YDOT = 5291
750241 meter/sec
ZDOT = 16887
622403 ZDOT = 5158
327281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13494008
91 X = 4112973
91
Y = -14882667
07 feet Y = -4536236
92 meter
Z = -9005292
55 Z = -2744813
17
XDOT = 16776
563246 XDOT = 5113
496477
YDOT = 4943
266294 feet/sec YDOT = 1506
707566 meter/sec
ZDOT = 16929
264894 ZDOT = 5160
039940
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 06339
93455816
00020000 00000-0 20000-3 0 9012
2 25544 51
6358 21
9909 0024422 301
0940 58
7828 15
75414231 20262
Satellite: ISS
Catalog Number: 25544
Epoch time: 06339
93455816 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 21
9909 deg
Eccentricity:
0024422
Arg of perigee: 301
0940 deg
Mean anomaly: 58
7828 deg
Mean motion: 15
75414231 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2026
Checksum: 286
Coasting Arc #3 (Orbit 2041)
---------------------------------------
Vector Time (GMT): 2006/340/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1848474
68 A = 6718309
78 meter
Y = -4419755
94 meter E =
0020011
Z = -4709524
94 I = 51
71190
XDOT = 7210
385674 Wp = 331
81283
YDOT = -106
078189 meter/sec RA = 16
40496 deg
ZDOT = -2708
523668 TA = 271
45880
MA = 271
68803
Ha = 191
863 n
mi
Hp = 178
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6064549
48 X = -1776036
81
Y = -14500511
62 feet Y = -4440020
75 meter
Z = -15451197
30 Z = -4718329
72
XDOT = 23656
120979 XDOT = 7224
193561
YDOT = -348
025555 feet/sec YDOT = -25
369968 meter/sec
ZDOT = -8886
232505 ZDOT = -2673
461870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14890260
07 X = -4538551
27
Y = -4928488
46 feet Y = -1502203
28 meter
Z = -15484613
40 Z = -4719710
16
XDOT = 14841
612938 XDOT = 4523
723624
YDOT = -17106
909601 feet/sec YDOT = -5214
186046 meter/sec
ZDOT = -8755
144899 ZDOT = -2668
568165
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 06340
94947187
00020000 00000-0 20000-3 0 9023
2 25544 51
6356 16
7675 0024484 305
1294 54
7575 15
75463201 20421
Satellite: ISS
Catalog Number: 25544
Epoch time: 06340
94947187 = yrday
fracday
Element set: 902
Inclination: 51
6356 deg
RA of node: 16
7675 deg
Eccentricity:
0024484
Arg of perigee: 305
1294 deg
Mean anomaly: 54
7575 deg
Mean motion: 15
75463201 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2042
Checksum: 296
Coasting Arc #4 (Orbit 2057)
---------------------------------------
Vector Time (GMT): 2006/341/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6455387
57 A = 6726501
39 meter
Y = 248589
42 meter E =
0011317
Z = 1900672
94 I = 51
71159
XDOT = -1845
200735 Wp = 327
86194
YDOT = -4899
060905 meter/sec RA = 11
22484 deg
ZDOT = -5632
156855 TA = 191
06238
MA = 191
08728
Ha = 192
098 n
mi
Hp = 178
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21179093
09 X = -6466920
69
Y = 815582
08 feet Y = 176336
89 meter
Z = 6235803
60 Z = 1869284
65
XDOT = -6053
808185 XDOT = -1762
921581
YDOT = -16073
034465 feet/sec YDOT = -4919
233988 meter/sec
ZDOT = -18478
204904 ZDOT = -5640
921804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12933459
87 X = -3942118
57
Y = 16834324
25 feet Y = 5131102
03 meter
Z = 6118459
60 Z = 1864906
48
XDOT = -14936
924031 XDOT = -4552
774445
YDOT = -4754
882697 feet/sec YDOT = -1449
288246 meter/sec
ZDOT = -18511
528423 ZDOT = -5642
313863
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 06341
96436461
00020000 00000-0 20000-3 0 9035
2 25544 51
6355 11
5433 0024296 309
0154 50
8846 15
75461912 20586
Satellite: ISS
Catalog Number: 25544
Epoch time: 06341
96436461 = yrday
fracday
Element set: 903
Inclination: 51
6355 deg
RA of node: 11
5433 deg
Eccentricity:
0024296
Arg of perigee: 309
0154 deg
Mean anomaly: 50
8846 deg
Mean motion: 15
75461912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2058
Checksum: 283
Coasting Arc #5 (Orbit 2073)
---------------------------------------
Vector Time (GMT): 2006/342/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1326225
05 A = 6716609
25 meter
Y = 4190193
80 meter E =
0019605
Z = 5087818
31 I = 51
65067
XDOT = -7514
768403 Wp = 314
24926
YDOT = 463
887210 meter/sec RA = 6
10988 deg
ZDOT = 1593
994669 TA = 120
53390
MA = 120
34026
Ha = 192
322 n
mi
Hp = 178
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4351132
05 X = 1254555
49
Y = 13747354
98 feet Y = 4204622
92 meter
Z = 16692317
29 Z = 5094087
62
XDOT = -24654
751977 XDOT = -7527
140465
YDOT = 1521
939665 feet/sec YDOT = 379
783492 meter/sec
ZDOT = 5229
641304 ZDOT = 1557
458000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13386824
63 X = 4080304
15
Y = 5283566
34 feet Y = 1610431
02 meter
Z = 16716232
49 Z = 5095107
66
XDOT = -13877
806656 XDOT = -4229
955469
YDOT = 19226
470747 feet/sec YDOT = 5860
228284 meter/sec
ZDOT = 5093
063022 ZDOT = 1552
365609
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 06342
97923292
00020000 00000-0 20000-3 0 9041
2 25544 51
6357 6
3180 0024374 313
0864 46
8260 15
75503786 20748
Satellite: ISS
Catalog Number: 25544
Epoch time: 06342
97923292 = yrday
fracday
Element set: 904
Inclination: 51
6357 deg
RA of node: 6
3180 deg
Eccentricity:
0024374
Arg of perigee: 313
0864 deg
Mean anomaly: 46
8260 deg
Mean motion: 15
75503786 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2074
Checksum: 291
Coasting Arc #6 (Orbit 2088)
---------------------------------------
Vector Time (GMT): 2006/343/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6625457
64 A = 6727480
83 meter
Y = -586538
58 meter E =
0027825
Z = -879118
67 I = 51
65871
XDOT = 1216
336879 Wp = 337
71516
YDOT = 4740
855283 meter/sec RA =
94141 deg
ZDOT = 5968
001605 TA = 12
66780
MA = 12
59802
Ha = 192
562 n
mi
Hp = 178
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21737065
75 X = 6635794
57
Y = -1924339
17 feet Y = -512391
13 meter
Z = -2884247
61 Z = -846907
24
XDOT = 3990
606558 XDOT = 1134
242174
YDOT = 15553
987149 feet/sec YDOT = 4753
997294 meter/sec
ZDOT = 19580
057760 ZDOT = 5973
711727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11800570
90 X = 3596814
01
Y = -18374700
82 feet Y = -5600608
81 meter
Z = -2763854
04 Z = -842422
71
XDOT = 13333
422148 XDOT = 4064
027071
YDOT = 5596
057201 feet/sec YDOT = 1705
678235 meter/sec
ZDOT = 19601
947168 ZDOT = 5974
673497
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 06343
93065108
00020000 00000-0 20000-3 0 9052
2 25544 51
6352 1
4196 0024518 316
6409 43
2826 15
75546889 20896
Satellite: ISS
Catalog Number: 25544
Epoch time: 06343
93065108 = yrday
fracday
Element set: 905
Inclination: 51
6352 deg
RA of node: 1
4196 deg
Eccentricity:
0024518
Arg of perigee: 316
6409 deg
Mean anomaly: 43
2826 deg
Mean motion: 15
75546889 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2089
Checksum: 300
Coasting Arc #7 (Orbit 2104)
---------------------------------------
Vector Time (GMT): 2006/344/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -775393
12 A = 6715572
56 meter
Y = -4116537
68 meter E =
0019657
Z = -5249506
40 I = 51
58975
XDOT = 7641
186995 Wp = 357
86530
YDOT = -888
533474 meter/sec RA = 355
80424 deg
ZDOT = -412
532272 TA = 268
10350
MA = 268
32864
Ha = 192
683 n
mi
Hp = 178
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2543940
67 X = -703802
67
Y = -13505701
05 feet Y = -4124807
74 meter
Z = -17222790
02 Z = -5253099
78
XDOT = 25069
511140 XDOT = 7652
558797
YDOT = -2915
136070 feet/sec YDOT = -803
021852 meter/sec
ZDOT = -1353
452337 ZDOT = -375
383903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12283312
71 X = -3743953
71
Y = -6125082
87 feet Y = -1866925
26 meter
Z = -17236695
73 Z = -5253744
86
XDOT = 12232
658654 XDOT = 3728
514358
YDOT = -20934
772194 feet/sec YDOT = -6380
918565 meter/sec
ZDOT = -1214
628950 ZDOT = -370
218904
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 06344
94547566
00020000 00000-0 20000-3 0 9068
2 25544 51
6342 356
1948 0024469 320
5532 39
3850 15
75604963 21056
Satellite: ISS
Catalog Number: 25544
Epoch time: 06344
94547566 = yrday
fracday
Element set: 906
Inclination: 51
6342 deg
RA of node: 356
1948 deg
Eccentricity:
0024469
Arg of perigee: 320
5532 deg
Mean anomaly: 39
3850 deg
Mean motion: 15
75604963 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2105
Checksum: 306
Coasting Arc #8 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2006/345/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6666038
92 A = 6727586
82 meter
Y = 940698
07 meter E =
0012769
Z = -194954
22 I = 51
60215
XDOT = -489
853975 Wp = 330
62341
YDOT = -4755
956640 meter/sec RA = 350
65247 deg
ZDOT = -6021
692061 TA = 211
49331
MA = 211
56981
Ha = 192
927 n
mi
Hp = 178
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21870206
44 X = -6675115
45
Y = 3086279
77 feet Y = 866103
99 meter
Z = -639613
57 Z = -227359
84
XDOT = -1607
132464 XDOT = -407
383467
YDOT = -15603
532285 feet/sec YDOT = -4760
972810 meter/sec
ZDOT = -19756
207549 ZDOT = -6023
871876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10285496
66 X = -3135019
38
Y = 19541495
87 feet Y = 5956247
94 meter
Z = -760694
15 Z = -231859
58
XDOT = -12107
359366 XDOT = -3690
323135
YDOT = -7161
041267 feet/sec YDOT = -2182
685378 meter/sec
ZDOT = -19764
901796 ZDOT = -6024
342067
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 06345
96027831
00020000 00000-0 20000-3 0 9070
2 25544 51
6344 350
9708 0024362 324
2911 35
6622 15
75601793 21210
Satellite: ISS
Catalog Number: 25544
Epoch time: 06345
96027831 = yrday
fracday
Element set: 907
Inclination: 51
6344 deg
RA of node: 350
9708 deg
Eccentricity:
0024362
Arg of perigee: 324
2911 deg
Mean anomaly: 35
6622 deg
Mean motion: 15
75601793 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2121
Checksum: 282
Coasting Arc #9 (Orbit 2136)
---------------------------------------
Vector Time (GMT): 2006/346/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 68039
87 A = 6715712
80 meter
Y = 4255219
61 meter E =
0024596
Z = 5206646
51 I = 51
53404
XDOT = -7543
770641 Wp = 335
75109
YDOT = 1227
296553 meter/sec RA = 345
48791 deg
ZDOT = -883
876736 TA = 122
80454
MA = 122
56740
Ha = 193
105 n
mi
Hp = 177
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 223227
93 X = -4840
71
Y = 13960694
25 feet Y = 4255572
54 meter
Z = 17082173
58 Z = 5206800
37
XDOT = -24749
903679 XDOT = -7552
640040
YDOT = 4026
563493 feet/sec YDOT = 1142
888400 meter/sec
ZDOT = -2899
858059 ZDOT = -920
545996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11536047
09 X = 3516187
15
Y = 7863469
35 feet Y = 2396785
46 meter
Z = 17083235
53 Z = 5206970
19
XDOT = -10239
009838 XDOT = -3120
850199
YDOT = 21765
174946 feet/sec YDOT = 6634
025324 meter/sec
ZDOT = -3036
849376 ZDOT = -925
631690
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 06346
97505660
00020000 00000-0 20000-3 0 9084
2 25544 51
6339 345
7447 0024362 328
1970 31
7721 15
75647191 21370
Satellite: ISS
Catalog Number: 25544
Epoch time: 06346
97505660 = yrday
fracday
Element set: 908
Inclination: 51
6339 deg
RA of node: 345
7447 deg
Eccentricity:
0024362
Arg of perigee: 328
1970 deg
Mean anomaly: 31
7721 deg
Mean motion: 15
75647191 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2137
Checksum: 306
Coasting Arc #10 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2006/347/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6466684
81 A = 6726547
38 meter
Y = -1186282
44 meter E =
0028412
Z = 1331057
09 I = 51
54279
XDOT = -275
593474 Wp =
93966
YDOT = 5030
485172 meter/sec RA = 340
35201 deg
ZDOT = 5848
431798 TA = 13
73901
MA = 13
66184
Ha = 193
155 n
mi
Hp = 177
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21216157
51 X = 6473003
28
Y = -3892002
77 feet Y = -1113933
17 meter
Z = 4366985
20 Z = 1362487
77
XDOT = -904
178064 XDOT = -360
235450
YDOT = 16504
216443 feet/sec YDOT = 5026
929582 meter/sec
ZDOT = 19187
768366 ZDOT = 5846
887781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8562301
38 X = 2609789
46
Y = -19771717
98 feet Y = -6026419
64 meter
Z = 4484389
39 Z = 1366841
89
XDOT = 11706
873807 XDOT = 3568
255136
YDOT = 9401
551950 feet/sec YDOT = 2865
593034 meter/sec
ZDOT = 19182
569725 ZDOT = 5846
847252
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 06347
98981147
00020000 00000-0 20000-3 0 9095
2 25544 51
6328 340
5186 0024318 332
0166 27
9689 15
75699683 21534
Satellite: ISS
Catalog Number: 25544
Epoch time: 06347
98981147 = yrday
fracday
Element set: 909
Inclination: 51
6328 deg
RA of node: 340
5186 deg
Eccentricity:
0024318
Arg of perigee: 332
0166 deg
Mean anomaly: 27
9689 deg
Mean motion: 15
75699683 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2153
Checksum: 331
Coasting Arc #11 (Orbit 2167)
---------------------------------------
Vector Time (GMT): 2006/348/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 517994
25 A = 6716719
40 meter
Y = -4547505
99 meter E =
0018714
Z = -4911597
02 I = 51
48247
XDOT = 7253
637857 Wp = 6
32073
YDOT = -1473
283279 meter/sec RA = 335
16303 deg
ZDOT = 2148
147417 TA = 284
44435
MA = 284
65194
Ha = 193
354 n
mi
Hp = 177
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1699456
21 X = 592666
54
Y = -14919639
07 feet Y = -4541295
51 meter
Z = -16114163
46 Z = -4908899
62
XDOT = 23798
024464 XDOT = 7259
137774
YDOT = -4833
606558 feet/sec YDOT = -1392
138521 meter/sec
ZDOT = 7047
727746 ZDOT = 2183
399235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11565787
22 X = -3525251
94
Y = -9592945
86 feet Y = -2923929
90 meter
Z = -16104595
65 Z = -4908680
76
XDOT = 8122
174436 XDOT = 2475
638768
YDOT = -21740
101736 feet/sec YDOT = -6626
383009 meter/sec
ZDOT = 7179
388493 ZDOT = 2188
277613
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 06348
94112379
00020000 00000-0 20000-3 0 9107
2 25544 51
6317 335
6192 0024186 335
8191 24
1836 15
75733230 21682
Satellite: ISS
Catalog Number: 25544
Epoch time: 06348
94112379 = yrday
fracday
Element set: 910
Inclination: 51
6317 deg
RA of node: 335
6192 deg
Eccentricity:
0024186
Arg of perigee: 335
8191 deg
Mean anomaly: 24
1836 deg
Mean motion: 15
75733230 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2168
Checksum: 291
Coasting Arc #12 (Orbit 2183)
---------------------------------------
Vector Time (GMT): 2006/349/22:17:48
224
Vector Time (MET): N/A
Weight (LBS) : 469411
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6144033
92 A = 6724498
60 meter
Y = 1314141
97 meter E =
0019621
Z = -2424350
67 I = 51
48383
XDOT = 950
829897 Wp = 346
80834
YDOT = -5450
820034 meter/sec RA = 330
04220 deg
ZDOT = -5337
056459 TA = 220
58457
MA = 220
73101
Ha = 193
543 n
mi
Hp = 176
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20157591
60 X = -6146494
98
Y = 4311489
39 feet Y = 1245422
47 meter
Z = -7953906
40 Z = -2454204
65
XDOT = 3119
520660 XDOT = 1037
637889
YDOT = -17883
267829 feet/sec YDOT = -5439
701371 meter/sec
ZDOT = -17510
027754 ZDOT = -5332
227002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6951701
82 X = -2118878
72
Y = 19359886
97 feet Y = 5900893
55 meter
Z = -8065400
52 Z = -2458334
08
XDOT = -12081
253813 XDOT = -3682
366162
YDOT = -11662
383343 feet/sec YDOT = -3554
694443 meter/sec
ZDOT = -17492
587952 ZDOT = -5331
740808
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 06349
95583320
00020000 00000-0 20000-3 0 9118
2 25544 51
6315 330
3942 0024238 339
8757 20
1449 15
75776452 21842
Satellite: ISS
Catalog Number: 25544
Epoch time: 06349
95583320 = yrday
fracday
Element set: 911
Inclination: 51
6315 deg
RA of node: 330
3942 deg
Eccentricity:
0024238
Arg of perigee: 339
8757 deg
Mean anomaly: 20
1449 deg
Mean motion: 15
75776452 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2184
Checksum: 302
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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