Date:
November 19th 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 1734)
---------------------------------------
Vector Time (GMT): 2006/321/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3602283
96 A = 6719917
20 meter
Y = -5583281
01 meter E =
0015839
Z = -930043
76 I = 51
93147
XDOT = 3582
320114 Wp = 187
93587
YDOT = 3306
535560 meter/sec RA = 116
53589 deg
ZDOT = -5978
140751 TA = 2
20545
MA = 2
19847
Ha = 184
455 n
mi
Hp = 178
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11818516
92 X = 3668967
36
Y = -18317851
09 feet Y = -5542625
40 meter
Z = -3051324
68 Z = -912381
61
XDOT = 11753
018747 XDOT = 3574
121223
YDOT = 10848
213781 feet/sec YDOT = 3346
549412 meter/sec
ZDOT = -19613
322674 ZDOT = -5960
757180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5751331
13 X = 1753005
73
Y = 21036564
62 feet Y = 6411944
90 meter
Z = -2986089
78 Z = -910160
17
XDOT = -14460
303471 XDOT = -4407
500498
YDOT = 1180
227448 feet/sec YDOT = 359
733326 meter/sec
ZDOT = -19547
960266 ZDOT = -5958
218289
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
50908098
00020000 00000-0 20000-3 0 9000
2 25544 51
6287 117
2124 0011482 227
4079 132
6119 15
78192932 17352
Satellite: ISS
Catalog Number: 25544
Epoch time: 06321
50908098 = yrday
fracday
Element set: 900
Inclination: 51
6287 deg
RA of node: 117
2124 deg
Eccentricity:
0011482
Arg of perigee: 227
4079 deg
Mean anomaly: 132
6119 deg
Mean motion: 15
78192932 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1735
Checksum: 284
Coasting Arc #2 (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 = -2440905
94 A = 6710445
50 meter
Y = -4034497
06 meter E =
0004516
Z = 4774970
15 I = 51
91053
XDOT = 4431
245583 Wp = 213
03004
YDOT = -5746
533042 meter/sec RA = 111
35851 deg
ZDOT = -2595
045108 TA = 262
27457
MA = 262
32585
Ha = 184
407 n
mi
Hp = 178
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8008221
60 X = -2418806
85
Y = -13236538
92 feet Y = -4061669
31 meter
Z = 15665912
57 Z = 4763165
35
XDOT = 14538
207293 XDOT = 4507
781408
YDOT = -18853
454861 feet/sec YDOT = -5696
552329 meter/sec
ZDOT = -8513
927519 ZDOT = -2573
331860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15306823
59 X = 4665519
83
Y = 2536665
50 feet Y = 773175
65 meter
Z = 15621295
47 Z = 4761370
86
XDOT = 4903
507293 XDOT = 1494
589023
YDOT = 22248
515962 feet/sec YDOT = 6781
347665 meter/sec
ZDOT = -8433
571027 ZDOT = -2570
552449
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
52222356
00020000 00000-0 20000-3 0 9010
2 25544 51
6284 111
9755 0011563 230
1726 129
8422 15
78162044 17514
Satellite: ISS
Catalog Number: 25544
Epoch time: 06322
52222356 = yrday
fracday
Element set: 901
Inclination: 51
6284 deg
RA of node: 111
9755 deg
Eccentricity:
0011563
Arg of perigee: 230
1726 deg
Mean anomaly: 129
8422 deg
Mean motion: 15
78162044 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1751
Checksum: 266
Coasting Arc #3 (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 = -4018208
94 A = 6714986
84 meter
Y = 4132851
36 meter E =
0007627
Z = 3448811
61 I = 51
93673
XDOT = -2046
873613 Wp = 156
33498
YDOT = -5832
782231 meter/sec RA = 106
25612 deg
ZDOT = 4594
530768 TA = 244
36628
MA = 244
44509
Ha = 183
977 n
mi
Hp = 179
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13183100
20 X = -4080878
64
Y = 13559223
61 feet Y = 4087566
86 meter
Z = 11314998
74 Z = 3429138
62
XDOT = -6715
464608 XDOT = -2003
818590
YDOT = -19136
424644 feet/sec YDOT = -5855
431110 meter/sec
ZDOT = 15073
919844 ZDOT = 4584
690906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1915243
55 X = -583766
23
Y = -18858000
88 feet Y = -5747918
67 meter
Z = 11242042
40 Z = 3426574
52
XDOT = 17670
293923 XDOT = 5385
905588
YDOT = 7189
529195 feet/sec YDOT = 2191
368499 meter/sec
ZDOT = 15036
416345 ZDOT = 4583
099702
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
53533773
00020000 00000-0 20000-3 0 9021
2 25544 51
6293 106
7383 0011599 234
3946 125
6139 15
78251226 17679
Satellite: ISS
Catalog Number: 25544
Epoch time: 06323
53533773 = yrday
fracday
Element set: 902
Inclination: 51
6293 deg
RA of node: 106
7383 deg
Eccentricity:
0011599
Arg of perigee: 234
3946 deg
Mean anomaly: 125
6139 deg
Mean motion: 15
78251226 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1767
Checksum: 302
Coasting Arc #4 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2006/324/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1179392
31 A = 6716302
70 meter
Y = 5926953
05 meter E =
0006978
Z = -2931425
94 I = 51
94955
XDOT = -4696
746062 Wp = 232
40870
YDOT = 3436
838094 meter/sec RA = 101
05944 deg
ZDOT = 5046
912029 TA = 93
93317
MA = 93
85339
Ha = 183
664 n
mi
Hp = 179
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3869397
35 X = 1127269
41
Y = 19445384
02 feet Y = 5939850
52 meter
Z = -9617539
18 Z = -2925822
31
XDOT = -15409
271858 XDOT = -4759
345927
YDOT = 11275
715531 feet/sec YDOT = 3383
965972 meter/sec
ZDOT = 16558
110330 ZDOT = 5023
942807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17598768
48 X = -5364104
63
Y = -9153968
47 feet Y = -2790129
59 meter
Z = -9595856
64 Z = -2924817
10
XDOT = 286
349299 XDOT = 87
279266
YDOT = -17860
799540 feet/sec YDOT = -5443
971700 meter/sec
ZDOT = 16472
740140 ZDOT = 5020
891195
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 06324
48511135
00020000 00000-0 20000-3 0 9035
2 25544 51
6307 101
8291 0011454 238
0311 121
9741 15
78273845 17822
Satellite: ISS
Catalog Number: 25544
Epoch time: 06324
48511135 = yrday
fracday
Element set: 903
Inclination: 51
6307 deg
RA of node: 101
8291 deg
Eccentricity:
0011454
Arg of perigee: 238
0311 deg
Mean anomaly: 121
9741 deg
Mean motion: 15
78273845 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1782
Checksum: 269
Coasting Arc #5 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2006/325/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4128987
88 A = 6708955
70 meter
Y = -1655005
96 meter E =
0003443
Z = -5024012
04 I = 51
92996
XDOT = 702
260388 Wp = 126
03572
YDOT = 7441
292165 meter/sec RA = 95
95268 deg
ZDOT = -1877
020683 TA = 125
95811
MA = 125
92617
Ha = 183
371 n
mi
Hp = 179
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13546548
16 X = 4171593
94
Y = -5429809
58 feet Y = -1608594
51 meter
Z = -16482979
14 Z = -5003849
55
XDOT = 2304
003897 XDOT = 628
117110
YDOT = 24413
688207 feet/sec YDOT = 7448
730899 meter/sec
ZDOT = -6158
204340 ZDOT = -1873
788215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4092843
01 X = -1247498
55
Y = 14096495
29 feet Y = 4296611
77 meter
Z = -16407859
61 Z = -5001115
61
XDOT = -19672
742355 XDOT = -5996
251870
YDOT = -12853
680381 feet/sec YDOT = -3917
801780 meter/sec
ZDOT = -6145
199720 ZDOT = -1873
056875
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 06325
49817779
00020000 00000-0 20000-3 0 9041
2 25544 51
6313 96
5933 0011353 242
6253 117
3757 15
78324715 17982
Satellite: ISS
Catalog Number: 25544
Epoch time: 06325
49817779 = yrday
fracday
Element set: 904
Inclination: 51
6313 deg
RA of node: 96
5933 deg
Eccentricity:
0011353
Arg of perigee: 242
6253 deg
Mean anomaly: 117
3757 deg
Mean motion: 15
78324715 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1798
Checksum: 315
Coasting Arc #6 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2006/326/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -71336
44 A = 6719789
35 meter
Y = -6707384
13 meter E =
0013156
Z = 209066
90 I = 51
96849
XDOT = 4751
262929 Wp = 185
06987
YDOT = -238
427554 meter/sec RA = 90
78759 deg
ZDOT = -6069
686271 TA = 352
66347
MA = 352
68270
Ha = 182
970 n
mi
Hp = 179
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -234043
45 X = 2656
13
Y = -22005853
43 feet Y = -6707768
17 meter
Z = 685915
03 Z = 208899
16
XDOT = 15588
132969 XDOT = 4783
062090
YDOT = -782
242631 feet/sec YDOT = -185
117668 meter/sec
ZDOT = -19913
668869 ZDOT = -6046
526858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17737253
35 X = 5406314
82
Y = 13027056
35 feet Y = 3970646
78 meter
Z = 684461
51 Z = 208623
87
XDOT = -7853
311258 XDOT = -2393
689271
YDOT = 11727
410389 feet/sec YDOT = 3574
514687 meter/sec
ZDOT = -19827
167718 ZDOT = -6043
320720
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 06326
51121892
00020000 00000-0 20000-3 0 9050
2 25544 51
6312 91
3557 0011389 246
9201 113
0764 15
78358852 18144
Satellite: ISS
Catalog Number: 25544
Epoch time: 06326
51121892 = yrday
fracday
Element set: 905
Inclination: 51
6312 deg
RA of node: 91
3557 deg
Eccentricity:
0011389
Arg of perigee: 246
9201 deg
Mean anomaly: 113
0764 deg
Mean motion: 15
78358852 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1814
Checksum: 286
Coasting Arc #7 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2006/327/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4131180
83 A = 6708363
77 meter
Y = -1274155
92 meter E =
0006984
Z = 5135194
98 I = 51
93038
XDOT = 549
444261 Wp = 261
45871
YDOT = -7548
800563 meter/sec RA = 85
63102 deg
ZDOT = -1433
665101 TA = 202
20036
MA = 202
23061
Ha = 182
695 n
mi
Hp = 179
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13553742
87 X = -4141572
33
Y = -4180301
57 feet Y = -1320411
93 meter
Z = 16847752
57 Z = 5115099
88
XDOT = 1802
638650 XDOT = 640
779788
YDOT = -24766
406047 feet/sec YDOT = -7542
145481 meter/sec
ZDOT = -4703
625659 ZDOT = -1430
775091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11392697
50 X = 3472494
20
Y = -8597386
11 feet Y = -2620483
29 meter
Z = 16772508
14 Z = 5112260
48
XDOT = 18354
541028 XDOT = 5594
464105
YDOT = 15182
379202 feet/sec YDOT = 4627
589181 meter/sec
ZDOT = -4693
748415 ZDOT = -1430
654517
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 06327
52423625
00020000 00000-0 20000-3 0 9062
2 25544 51
6326 86
1192 0011220 251
0296 108
9653 15
78366002 18305
Satellite: ISS
Catalog Number: 25544
Epoch time: 06327
52423625 = yrday
fracday
Element set: 906
Inclination: 51
6326 deg
RA of node: 86
1192 deg
Eccentricity:
0011220
Arg of perigee: 251
0296 deg
Mean anomaly: 108
9653 deg
Mean motion: 15
78366002 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1830
Checksum: 269
Coasting Arc #8 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2006/328/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1067505
38 A = 6716515
31 meter
Y = 6087574
93 meter E =
0002526
Z = 2627175
91 I = 51
95629
XDOT = -4694
784678 Wp = 89
81844
YDOT = -3097
532045 meter/sec RA = 80
51770 deg
ZDOT = 5265
512574 TA = 299
96594
MA = 299
99102
Ha = 182
134 n
mi
Hp = 179
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3502314
24 X = -1148260
68
Y = 19972358
68 feet Y = 6075185
58 meter
Z = 8619343
53 Z = 2621794
61
XDOT = -15402
836870 XDOT = -4685
377983
YDOT = -10162
506708 feet/sec YDOT = -3149
979894 meter/sec
ZDOT = 17275
303722 ZDOT = 5242
727385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14338409
44 X = -4370347
20
Y = -14349386
50 feet Y = -4373693
01 meter
Z = 8599972
14 Z = 2621271
51
XDOT = 16160
924295 XDOT = 4925
849725
YDOT = -5837
772665 feet/sec YDOT = -1779
353108 meter/sec
ZDOT = 17189
778521 ZDOT = 5239
444493
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 06328
53722448
00020000 00000-0 20000-3 0 9070
2 25544 51
6335 80
8821 0011311 254
9547 105
0367 15
78461079 18464
Satellite: ISS
Catalog Number: 25544
Epoch time: 06328
53722448 = yrday
fracday
Element set: 907
Inclination: 51
6335 deg
RA of node: 80
8821 deg
Eccentricity:
0011311
Arg of perigee: 254
9547 deg
Mean anomaly: 105
0367 deg
Mean motion: 15
78461079 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1846
Checksum: 296
Coasting Arc #9 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2006/329/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4002363
48 A = 6713732
12 meter
Y = 3948686
51 meter E =
0006337
Z = -3667143
68 I = 51
94080
XDOT = -1951
937671 Wp = 241
48210
YDOT = 6042
254252 meter/sec RA = 75
32189 deg
ZDOT = 4367
161573 TA = 74
58347
MA = 74
51348
Ha = 181
675 n
mi
Hp = 179
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13131113
79 X = 3975725
75
Y = 12955008
23 feet Y = 3993294
70 meter
Z = -12031311
30 Z = -3647764
19
XDOT = -6403
994982 XDOT = -2040
573015
YDOT = 19823
668805 feet/sec YDOT = 6019
930442 meter/sec
ZDOT = 14327
957917 ZDOT = 4357
464464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18117446
09 X = -5522197
57
Y = 3710192
97 feet Y = 1130866
82 meter
Z = -11958405
19 Z = -3644921
90
XDOT = -12550
765027 XDOT = -3825
473180
YDOT = -15129
361715 feet/sec YDOT = -4611
429451 meter/sec
ZDOT = 14292
447092 ZDOT = 4356
337874
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 06329
48688137
00020000 00000-0 20000-3 0 9082
2 25544 51
6336 75
9731 0011313 259
9284 100
0605 15
78449945 18610
Satellite: ISS
Catalog Number: 25544
Epoch time: 06329
48688137 = yrday
fracday
Element set: 908
Inclination: 51
6336 deg
RA of node: 75
9731 deg
Eccentricity:
0011313
Arg of perigee: 259
9284 deg
Mean anomaly: 100
0605 deg
Mean motion: 15
78449945 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1861
Checksum: 314
Coasting Arc #10 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2006/330/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2397744
28 A = 6709888
80 meter
Y = -4168360
69 meter E =
0002545
Z = -4679927
03 I = 51
92017
XDOT = 4384
011763 Wp = 341
22392
YDOT = 5681
289851 meter/sec RA = 70
22030 deg
ZDOT = -2811
351964 TA = 261
15453
MA = 261
18335
Ha = 181
351 n
mi
Hp = 179
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7866615
11 X = 2466911
67
Y = -13675724
06 feet Y = -4141160
53 meter
Z = -15354091
31 Z = -4668111
16
XDOT = 14383
240692 XDOT = 4333
814090
YDOT = 18639
402397 feet/sec YDOT = 5730
033944 meter/sec
ZDOT = -9223
595682 ZDOT = -2790
175586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7145567
00 X = 2177968
82
Y = 14113423
97 feet Y = 4301771
63 meter
Z = -15310431
66 Z = -4666619
57
XDOT = -22463
591811 XDOT = -6846
902784
YDOT = 1444
031111 feet/sec YDOT = 440
140683 meter/sec
ZDOT = -9143
759321 ZDOT = -2787
017841
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 06330
49982320
00020000 00000-0 20000-3 0 9097
2 25544 51
6339 70
7359 0011286 263
8050 96
1830 15
78494433 18770
Satellite: ISS
Catalog Number: 25544
Epoch time: 06330
49982320 = yrday
fracday
Element set: 909
Inclination: 51
6339 deg
RA of node: 70
7359 deg
Eccentricity:
0011286
Arg of perigee: 263
8050 deg
Mean anomaly: 96
1830 deg
Mean motion: 15
78494433 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1877
Checksum: 309
Coasting Arc #11 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2006/331/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3503745
13 A = 6718868
31 meter
Y = -5635043
30 meter E =
0008204
Z = 1019892
25 I = 51
93974
XDOT = 3600
316921 Wp = 178
16302
YDOT = -3315
279887 meter/sec RA = 65
03963 deg
ZDOT = -5955
530203 TA = 350
71224
MA = 350
72740
Ha = 180
941 n
mi
Hp = 179
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11495226
82 X = -3445427
37
Y = -18487674
86 feet Y = -5673898
14 meter
Z = 3346103
17 Z = 1003012
11
XDOT = 11812
063389 XDOT = 3666
052344
YDOT = -10876
902515 feet/sec YDOT = -3274
651090 meter/sec
ZDOT = -19539
141086 ZDOT = -5937
880354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21779722
78 X = 6638459
50
Y = 27772
61 feet Y = 8465
09 meter
Z = 3282327
22 Z = 1000453
34
XDOT = 2913
179495 XDOT = 887
937110
YDOT = 14283
632447 feet/sec YDOT = 4353
651170 meter/sec
ZDOT = -19473
569819 ZDOT = -5935
544081
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 06331
51274035
00020000 00000-0 20000-3 0 9100
2 25544 51
6338 65
4986 0011140 267
8325 92
1565 15
78534871 18934
Satellite: ISS
Catalog Number: 25544
Epoch time: 06331
51274035 = yrday
fracday
Element set: 910
Inclination: 51
6338 deg
RA of node: 65
4986 deg
Eccentricity:
0011140
Arg of perigee: 267
8325 deg
Mean anomaly: 92
1565 deg
Mean motion: 15
78534871 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1893
Checksum: 296
Coasting Arc #12 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2006/332/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3893313
40 A = 6707098
21 meter
Y = 1506498
18 meter E =
0008717
Z = 5256977
15 I = 51
88819
XDOT = -3447
901765 Wp = 281
31232
YDOT = -6862
595063 meter/sec RA = 59
89257 deg
ZDOT = -586
030509 TA = 174
24187
MA = 174
23184
Ha = 180
806 n
mi
Hp = 179
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12773337
92 X = -3935407
59
Y = 4942579
34 feet Y = 1462725
30 meter
Z = 17247300
37 Z = 5237961
11
XDOT = -11312
013664 XDOT = -3368
060154
YDOT = -22515
075666 feet/sec YDOT = -6900
704961 meter/sec
ZDOT = -1922
672273 ZDOT = -602
587068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2391481
11 X = 728923
44
Y = -13576032
32 feet Y = -4137974
65 meter
Z = 17176402
04 Z = 5235367
34
XDOT = 24129
717409 XDOT = 7354
737866
YDOT = 1735
059481 feet/sec YDOT = 528
846130 meter/sec
ZDOT = -1985
387899 ZDOT = -605
146232
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 06332
52563107
00020000 00000-0 20000-3 0 9114
2 25544 51
6344 60
2603 0011165 272
8675 87
1212 15
78617169 19094
Satellite: ISS
Catalog Number: 25544
Epoch time: 06332
52563107 = yrday
fracday
Element set: 911
Inclination: 51
6344 deg
RA of node: 60
2603 deg
Eccentricity:
0011165
Arg of perigee: 272
8675 deg
Mean anomaly: 87
1212 deg
Mean motion: 15
78617169 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1909
Checksum: 280
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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