Date:
November 12th 2006
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) : 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 1592)
---------------------------------------
Vector Time (GMT): 2006/312/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4864526
78 A = 6718010
82 meter
Y = -3736108
78 meter E =
0017923
Z = 2710924
75 I = 51
73548
XDOT = 5004
263401 Wp = 141
98360
YDOT = 2744
425978 meter/sec RA = 162
87663 deg
ZDOT = -5193
272592 TA = 7
02809
MA = 7
00299
Ha = 186
615 n
mi
Hp = 177
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15959733
53 X = 4892773
45
Y = -12257574
74 feet Y = -3681553
29 meter
Z = 8894110
09 Z = 2734625
39
XDOT = 16418
187012 XDOT = 4998
431462
YDOT = 9004
022239 feet/sec YDOT = 2800
354353 meter/sec
ZDOT = -17038
295906 ZDOT = -5168
975215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4552762
41 X = -1387681
98
Y = 19561729
81 feet Y = 5962415
25 meter
Z = 8982065
92 Z = 2737733
69
XDOT = -17055
110427 XDOT = -5198
397658
YDOT = 3818
439731 feet/sec YDOT = 1163
860430 meter/sec
ZDOT = -16947
238930 ZDOT = -5165
518426
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 06312
51637072
00020000 00000-0 20000-3 0 9002
2 25544 51
6331 163
6751 0011740 191
2173 168
8732 15
77834690 15930
Satellite: ISS
Catalog Number: 25544
Epoch time: 06312
51637072 = yrday
fracday
Element set: 900
Inclination: 51
6331 deg
RA of node: 163
6751 deg
Eccentricity:
0011740
Arg of perigee: 191
2173 deg
Mean anomaly: 168
8732 deg
Mean motion: 15
77834690 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1593
Checksum: 284
Coasting Arc #2 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2006/313/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3333920
93 A = 6710334
20 meter
Y = -2928325
14 meter E =
0014582
Z = 5036383
19 I = 51
73526
XDOT = 6288
441811 Wp = 174
67335
YDOT = -4083
500264 meter/sec RA = 157
75585 deg
ZDOT = 1773
794448 TA = 258
19464
MA = 258
35824
Ha = 186
620 n
mi
Hp = 177
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10938060
81 X = -3325394
46
Y = -9607365
96 feet Y = -2965559
73 meter
Z = 16523566
90 Z = 5020207
14
XDOT = 20631
370772 XDOT = 6325
019790
YDOT = -13397
310576 feet/sec YDOT = -4012
975082 meter/sec
ZDOT = 5819
535591 ZDOT = 1804
432657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14625565
10 X = 4457872
24
Y = 200761
04 feet Y = 61191
96 meter
Z = 16462790
12 Z = 5017858
43
XDOT = -7041
487258 XDOT = -2146
245316
YDOT = 22471
004793 feet/sec YDOT = 6849
162261 meter/sec
ZDOT = 5933
355794 ZDOT = 1808
486846
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 06313
52973615
00020000 00000-0 20000-3 0 9011
2 25544 51
6322 158
4397 0011762 195
1178 164
9637 15
77819296 16094
Satellite: ISS
Catalog Number: 25544
Epoch time: 06313
52973615 = yrday
fracday
Element set: 901
Inclination: 51
6322 deg
RA of node: 158
4397 deg
Eccentricity:
0011762
Arg of perigee: 195
1178 deg
Mean anomaly: 164
9637 deg
Mean motion: 15
77819296 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1609
Checksum: 317
Coasting Arc #3 (Orbit 1623)
---------------------------------------
Vector Time (GMT): 2006/314/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5863586
65 A = 6721109
07 meter
Y = 3278042
80 meter E =
0004695
Z = -266387
24 I = 51
79744
XDOT = -2531
816910 Wp = 123
02244
YDOT = -4043
749117 meter/sec RA = 152
58097 deg
ZDOT = 6042
445305 TA = 234
08734
MA = 234
13092
Ha = 186
280 n
mi
Hp = 177
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19237489
00 X = -5898512
30
Y = 10754733
61 feet Y = 3212277
67 meter
Z = -873973
87 Z = -294957
45
XDOT = -8306
485925 XDOT = -2515
764451
YDOT = -13266
893429 feet/sec YDOT = -4071
972080 meter/sec
ZDOT = 19824
295620 ZDOT = 6030
184214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7365604
37 X = 2245036
21
Y = -20767671
87 feet Y = -6329986
39 meter
Z = -980196
70 Z = -298763
95
XDOT = 13561
230399 XDOT = 4133
463026
YDOT = 3886
436541 feet/sec YDOT = 1184
585858 meter/sec
ZDOT = 19777
977864 ZDOT = 6028
327653
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 06314
47974256
00020000 00000-0 20000-3 0 9029
2 25544 51
6314 153
5312 0011786 199
6058 160
4655 15
77879338 16241
Satellite: ISS
Catalog Number: 25544
Epoch time: 06314
47974256 = yrday
fracday
Element set: 902
Inclination: 51
6314 deg
RA of node: 153
5312 deg
Eccentricity:
0011786
Arg of perigee: 199
6058 deg
Mean anomaly: 160
4655 deg
Mean motion: 15
77879338 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1624
Checksum: 312
Coasting Arc #4 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2006/315/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1060512
50 A = 6709386
93 meter
Y = 4154468
00 meter E =
0016167
Z = -5170933
17 I = 51
78217
XDOT = -6867
572407 Wp = 144
21324
YDOT = 3264
493853 meter/sec RA = 147
41770 deg
ZDOT = 1203
332105 TA = 137
32499
MA = 137
19930
Ha = 186
052 n
mi
Hp = 177
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3479371
73 X = 1039097
56
Y = 13630144
36 feet Y = 4166207
87 meter
Z = -16965003
83 Z = -5165832
87
XDOT = -22531
405535 XDOT = -6909
411648
YDOT = 10710
281669 feet/sec YDOT = 3187
462828 meter/sec
ZDOT = 3947
939976 ZDOT = 1169
867696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11808578
76 X = -3599254
81
Y = -7688238
28 feet Y = -2343375
03 meter
Z = -16945402
85 Z = -5164958
79
XDOT = 8934
708247 XDOT = 2723
299074
YDOT = -22229
605025 feet/sec YDOT = -6775
583612 meter/sec
ZDOT = 3823
429988 ZDOT = 1165
381460
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 06315
49306123
00020000 00000-0 20000-3 0 9035
2 25544 51
6306 148
2950 0011778 203
3357 156
7275 15
77927836 16408
Satellite: ISS
Catalog Number: 25544
Epoch time: 06315
49306123 = yrday
fracday
Element set: 903
Inclination: 51
6306 deg
RA of node: 148
2950 deg
Eccentricity:
0011778
Arg of perigee: 203
3357 deg
Mean anomaly: 156
7275 deg
Mean motion: 15
77927836 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1640
Checksum: 295
Coasting Arc #5 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2006/316/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5882666
45 A = 6718709
37 meter
Y = -2259305
60 meter E =
0014738
Z = -2303500
03 I = 51
83703
XDOT = -38
969694 Wp = 185
57289
YDOT = 5450
669769 meter/sec RA = 142
29551 deg
ZDOT = -5457
095981 TA = 20
31779
MA = 20
25921
Ha = 185
903 n
mi
Hp = 177
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19300086
77 X = 5918683
20
Y = -7412419
96 feet Y = -2193320
86 meter
Z = -7557414
80 Z = -2274834
39
XDOT = -127
853326 XDOT = -73
407099
YDOT = 17882
774833 feet/sec YDOT = 5450
041727 meter/sec
ZDOT = -17903
858207 ZDOT = -5457
368660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9015721
89 X = -2747992
03
Y = 18648216
95 feet Y = 5683976
53 meter
Z = -7450677
86 Z = -2270966
61
XDOT = -10867
490845 XDOT = -3312
411209
YDOT = -12392
156431 feet/sec YDOT = -3777
129280 meter/sec
ZDOT = -17904
144383 ZDOT = -5457
183208
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 06316
50635633
00020000 00000-0 20000-3 0 9040
2 25544 51
6306 143
0607 0011743 207
7189 152
3352 15
77948669 16565
Satellite: ISS
Catalog Number: 25544
Epoch time: 06316
50635633 = yrday
fracday
Element set: 904
Inclination: 51
6306 deg
RA of node: 143
0607 deg
Eccentricity:
0011743
Arg of perigee: 207
7189 deg
Mean anomaly: 152
3352 deg
Mean motion: 15
77948669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1656
Checksum: 297
Coasting Arc #6 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2006/317/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1024620
15 A = 6713713
29 meter
Y = -5268572
72 meter E =
0008745
Z = 4024000
51 I = 51
84271
XDOT = 6405
935591 Wp = 151
10789
YDOT = -1746
612815 meter/sec RA = 137
09665 deg
ZDOT = -3921
937307 TA = 339
17395
MA = 339
20956
Ha = 185
573 n
mi
Hp = 178
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3361614
68 X = 1063909
83
Y = -17285343
57 feet Y = -5256895
32 meter
Z = 13202101
43 Z = 4029073
42
XDOT = 21016
849051 XDOT = 6444
042635
YDOT = -5730
357004 feet/sec YDOT = -1674
764879 meter/sec
ZDOT = -12867
248384 ZDOT = -3890
724417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9697038
31 X = 2955657
28
Y = 14682273
12 feet Y = 4475156
85 meter
Z = 13220338
18 Z = 4029559
08
XDOT = -10047
459479 XDOT = -3062
465649
YDOT = 18105
447640 feet/sec YDOT = 5518
540441 meter/sec
ZDOT = -12750
922537 ZDOT = -3886
481189
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 06317
51962669
00020000 00000-0 20000-3 0 9055
2 25544 51
6307 137
8246 0011786 212
0901 147
9547 15
77999030 16726
Satellite: ISS
Catalog Number: 25544
Epoch time: 06317
51962669 = yrday
fracday
Element set: 905
Inclination: 51
6307 deg
RA of node: 137
8246 deg
Eccentricity:
0011786
Arg of perigee: 212
0901 deg
Mean anomaly: 147
9547 deg
Mean motion: 15
77999030 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1672
Checksum: 313
Coasting Arc #7 (Orbit 1687)
---------------------------------------
Vector Time (GMT): 2006/318/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5106700
51 A = 6712701
07 meter
Y = 601501
88 meter E =
0012845
Z = 4320631
40 I = 51
85833
XDOT = 2188
016619 Wp = 169
27277
YDOT = -6513
619921 meter/sec RA = 131
99481 deg
ZDOT = 3478
879735 TA = 245
60779
MA = 245
74189
Ha = 185
363 n
mi
Hp = 178
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16754266
76 X = -5134036
19
Y = 1973431
37 feet Y = 544242
97 meter
Z = 14175299
87 Z = 4295756
31
XDOT = 7178
532215 XDOT = 2243
790194
YDOT = -21370
144097 feet/sec YDOT = -6488
840546 meter/sec
ZDOT = 11413
647425 ZDOT = 3489
644587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10460316
49 X = 3188304
47
Y = -13334334
36 feet Y = -4064305
11 meter
Z = 14082482
69 Z = 4292340
72
XDOT = 9177
853748 XDOT = 2797
409823
YDOT = 19344
143837 feet/sec YDOT = 5896
095042 meter/sec
ZDOT = 11452
976657 ZDOT = 3490
867285
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 06318
53287427
00020000 00000-0 20000-3 0 9061
2 25544 51
6297 132
5881 0011730 215
8860 144
1518 15
78029187 16887
Satellite: ISS
Catalog Number: 25544
Epoch time: 06318
53287427 = yrday
fracday
Element set: 906
Inclination: 51
6297 deg
RA of node: 132
5881 deg
Eccentricity:
0011730
Arg of perigee: 215
8860 deg
Mean anomaly: 144
1518 deg
Mean motion: 15
78029187 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1688
Checksum: 310
Coasting Arc #8 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2006/319/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2632705
17 A = 6719142
84 meter
Y = 5908022
98 meter E =
0004448
Z = -1825198
28 I = 51
89855
XDOT = -5164
051018 Wp = 219
36715
YDOT = -541
058745 meter/sec RA = 126
80234 deg
ZDOT = 5686
497395 TA = 120
44382
MA = 120
39987
Ha = 185
112 n
mi
Hp = 178
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8637484
17 X = -2689707
20
Y = 19383277
49 feet Y = 5878263
93 meter
Z = -5988183
34 Z = -1838126
54
XDOT = -16942
424600 XDOT = -5185
241503
YDOT = -1775
127117 feet/sec YDOT = -598
924627 meter/sec
ZDOT = 18656
487516 ZDOT = 5661
358489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8030024
75 X = -2447551
54
Y = -19628173
80 feet Y = -5982667
37 meter
Z = -6035678
47 Z = -1839674
80
XDOT = 11650
469561 XDOT = 3551
063122
YDOT = -10485
167257 feet/sec YDOT = -3195
878980 meter/sec
ZDOT = 18562
528133 ZDOT = 5657
858575
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 06319
48277137
00020000 00000-0 20000-3 0 9074
2 25544 51
6295 127
6785 0011720 218
6262 141
4066 15
78067309 17033
Satellite: ISS
Catalog Number: 25544
Epoch time: 06319
48277137 = yrday
fracday
Element set: 907
Inclination: 51
6295 deg
RA of node: 127
6785 deg
Eccentricity:
0011720
Arg of perigee: 218
6262 deg
Mean anomaly: 141
4066 deg
Mean motion: 15
78067309 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1703
Checksum: 299
Coasting Arc #9 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2006/320/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3831565
01 A = 6708514
59 meter
Y = 1649423
11 meter E =
0010302
Z = -5259284
83 I = 51
87894
XDOT = -3658
136517 Wp = 136
52833
YDOT = 6756
666441 meter/sec RA = 121
67510 deg
ZDOT = -553
998499 TA = 128
27304
MA = 128
18031
Ha = 184
901 n
mi
Hp = 178
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12570751
34 X = 3838385
39
Y = 5411493
16 feet Y = 1692308
06 meter
Z = -17254871
48 Z = -5240654
06
XDOT = -12001
760226 XDOT = -3730
727336
YDOT = 22167
540818 feet/sec YDOT = 6715
353266 meter/sec
ZDOT = -1817
580378 ZDOT = -571
946299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12579205
77 X = -3834141
92
Y = 5610313
42 feet Y = 1710023
53 meter
Z = -17185069
18 Z = -5238009
09
XDOT = -7696
619148 XDOT = -2345
929516
YDOT = -22946
793062 feet/sec YDOT = -6994
182525 meter/sec
ZDOT = -1883
717338 ZDOT = -574
157044
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 06320
49597124
00020000 00000-0 20000-3 0 9089
2 25544 51
6294 122
4428 0011585 222
1022 137
9254 15
78110629 17192
Satellite: ISS
Catalog Number: 25544
Epoch time: 06320
49597124 = yrday
fracday
Element set: 908
Inclination: 51
6294 deg
RA of node: 122
4428 deg
Eccentricity:
0011585
Arg of perigee: 222
1022 deg
Mean anomaly: 137
9254 deg
Mean motion: 15
78110629 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1719
Checksum: 283
Coasting Arc #10 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2006/321/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3582019
97 A = 6719981
29 meter
Y = -5601709
28 meter E =
0015860
Z = -897283
21 I = 51
93219
XDOT = 3608
611502 Wp = 187
49225
YDOT = 3265
594134 meter/sec RA = 116
52995 deg
ZDOT = -5984
802163 TA = 2
28809
MA = 2
28084
Ha = 184
470 n
mi
Hp = 178
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11752034
01 X = 3648751
79
Y = -18378311
30 feet Y = -5561280
00 meter
Z = -2943842
57 Z = -879719
39
XDOT = 11839
276582 XDOT = 3600
900831
YDOT = 10713
891516 feet/sec YDOT = 3305
904720 meter/sec
ZDOT = -19635
177700 ZDOT = -5967
289681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5841118
99 X = 1780373
07
Y = 21026926
95 feet Y = 6409007
33 meter
Z = -2878977
34 Z = -877512
29
XDOT = -14418
559985 XDOT = -4394
777083
YDOT = 1327
633847 feet/sec YDOT = 404
662796 meter/sec
ZDOT = -19569
339184 ZDOT = -5964
734583
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 06321
50914477
00020000 00000-0 20000-3 0 9097
2 25544 51
6294 117
2060 0011443 227
3298 132
6904 15
78179346 17354
Satellite: ISS
Catalog Number: 25544
Epoch time: 06321
50914477 = yrday
fracday
Element set: 909
Inclination: 51
6294 deg
RA of node: 117
2060 deg
Eccentricity:
0011443
Arg of perigee: 227
3298 deg
Mean anomaly: 132
6904 deg
Mean motion: 15
78179346 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1735
Checksum: 293
Coasting Arc #11 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2006/322/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2468898
92 A = 6710420
04 meter
Y = -3998220
60 meter E =
0004551
Z = 4791118
81 I = 51
91094
XDOT = 4410
439615 Wp = 213
77706
YDOT = -5780
038284 meter/sec RA = 111
35330 deg
ZDOT = -2555
602827 TA = 261
11596
MA = 261
16749
Ha = 184
426 n
mi
Hp = 178
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8100062
08 X = -2447281
84
Y = -13117521
66 feet Y = -4025708
58 meter
Z = 15718893
74 Z = 4779176
85
XDOT = 14469
946244 XDOT = 4487
160038
YDOT = -18963
380198 feet/sec YDOT = -5730
289206 meter/sec
ZDOT = -8384
523711 ZDOT = -2533
990211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15277075
97 X = 4656452
76
Y = 2389124
35 feet Y = 728205
10 meter
Z = 15673769
02 Z = 4777364
80
XDOT = 5021
012531 XDOT = 1530
404620
YDOT = 22270
426757 feet/sec YDOT = 6788
026076 meter/sec
ZDOT = -8304
547443 ZDOT = -2531
226061
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 06322
52229640
00020000 00000-0 20000-3 0 9103
2 25544 51
6291 111
9692 0011523 230
0714 129
9439 15
78147574 17514
Satellite: ISS
Catalog Number: 25544
Epoch time: 06322
52229640 = yrday
fracday
Element set: 910
Inclination: 51
6291 deg
RA of node: 111
9692 deg
Eccentricity:
0011523
Arg of perigee: 230
0714 deg
Mean anomaly: 129
9439 deg
Mean motion: 15
78147574 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1751
Checksum: 279
Coasting Arc #12 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2006/323/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4003238
69 A = 6715123
60 meter
Y = 4174171
27 meter E =
0007553
Z = 3416413
65 I = 51
93769
XDOT = -2084
481641 Wp = 155
12295
YDOT = -5794
164154 meter/sec RA = 106
25079 deg
ZDOT = 4626
400641 TA = 245
11589
MA = 245
19442
Ha = 183
996 n
mi
Hp = 179
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13133985
19 X = -4066214
16
Y = 13694787
64 feet Y = 4129052
47 meter
Z = 11208706
21 Z = 3396812
65
XDOT = -6838
850528 XDOT = -2042
010478
YDOT = -19009
724916 feet/sec YDOT = -5817
236854 meter/sec
ZDOT = 15178
479793 ZDOT = 4616
376657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2051149
86 X = -625190
48
Y = -18906761
29 feet Y = -5762780
84 meter
Z = 11136024
07 Z = 3394260
14
XDOT = 17648
966434 XDOT = 5379
404969
YDOT = 7023
078104 feet/sec YDOT = 2140
634206 meter/sec
ZDOT = 15140
293486 ZDOT = 4614
761454
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 06323
53541967
00020000 00000-0 20000-3 0 9115
2 25544 51
6301 106
7322 0011560 234
2988 125
7103 15
78236912 17672
Satellite: ISS
Catalog Number: 25544
Epoch time: 06323
53541967 = yrday
fracday
Element set: 911
Inclination: 51
6301 deg
RA of node: 106
7322 deg
Eccentricity:
0011560
Arg of perigee: 234
2988 deg
Mean anomaly: 125
7103 deg
Mean motion: 15
78236912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1767
Checksum: 279
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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