Date:
October 26th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6113 9 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
299/14:46:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
9
000/00:00:00
000 0
0 0
0 175
2
Coasting Arc #1 (Orbit 1370)
---------------------------------------
Vector Time (GMT): 2006/298/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4955850
78 A = 6720386
16 meter
Y = 3818609
64 meter E =
0025383
Z = 2414455
48 I = 51
38158
XDOT = -1507
456881 Wp = 119
33047
YDOT = 5356
582218 meter/sec RA = 235
57068 deg
ZDOT = -5347
840669 TA = 33
23027
MA = 33
07112
Ha = 189
188 n
mi
Hp = 175
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16259352
94 X = 4901052
88
Y = 12528246
85 feet Y = 3873722
24 meter
Z = 7921441
85 Z = 2438398
75
XDOT = -4945
724674 XDOT = -1541
263269
YDOT = 17574
088643 feet/sec YDOT = 5339
536167 meter/sec
ZDOT = -17545
409019 ZDOT = -5355
246044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16833898
65 X = -5130972
31
Y = -11683879
30 feet Y = -3561246
41 meter
Z = 8011216
46 Z = 2441818
78
XDOT = 3093
114052 XDOT = 942
781163
YDOT = -16571
363015 feet/sec YDOT = -5050
951447 meter/sec
ZDOT = -17572
279712 ZDOT = -5356
030856
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 06298
45327867
00020000 00000-0 20000-3 0 9006
2 25544 51
6309 236
2733 0012339 134
9529 225
2638 15
77236127 13714
Satellite: ISS
Catalog Number: 25544
Epoch time: 06298
45327867 = yrday
fracday
Element set: 900
Inclination: 51
6309 deg
RA of node: 236
2733 deg
Eccentricity:
0012339
Arg of perigee: 134
9529 deg
Mean anomaly: 225
2638 deg
Mean motion: 15
77236127 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1371
Checksum: 302
Coasting Arc #2 (Orbit 1386)
---------------------------------------
Vector Time (GMT): 2006/299/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1944717
51 A = 6711662
05 meter
Y = -3971350
94 meter E =
0017268
Z = 5041611
06 I = 51
37002
XDOT = 5733
792684 Wp = 135
47866
YDOT = 4894
873614 meter/sec RA = 230
42763 deg
ZDOT = 1628
530496 TA = 298
75347
MA = 298
92684
Ha = 189
051 n
mi
Hp = 175
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6380306
80 X = 1964489
29
Y = -13029366
59 feet Y = -3949493
74 meter
Z = 16540718
71 Z = 5051106
57
XDOT = 18811
655786 XDOT = 5670
720060
YDOT = 16059
296633 feet/sec YDOT = 4958
639321 meter/sec
ZDOT = 5342
947821 ZDOT = 1656
233045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5385203
20 X = -1641409
93
Y = 13428253
59 feet Y = 4092931
69 meter
Z = 16575574
69 Z = 5052235
17
XDOT = -18854
628451 XDOT = -5746
890752
YDOT = -14347
622187 feet/sec YDOT = -4373
155243 meter/sec
ZDOT = 5446
892477 ZDOT = 1660
212827
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 06299
46701309
00020000 00000-0 20000-3 0 9016
2 25544 51
6312 231
0422 0012267 139
4291 220
7790 15
77288295 13871
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
46701309 = yrday
fracday
Element set: 901
Inclination: 51
6312 deg
RA of node: 231
0422 deg
Eccentricity:
0012267
Arg of perigee: 139
4291 deg
Mean anomaly: 220
7790 deg
Mean motion: 15
77288295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1387
Checksum: 289
Coasting Arc #3 (Orbit 1389)
---------------------------------------
Vector Time (GMT): 2006/299/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5037552
97 A = 6714202
58 meter
Y = 479073
50 meter E =
0017464
Z = 4395535
16 I = 51
38566
XDOT = 2233
633201 Wp = 109
99080
YDOT = 6621
309271 meter/sec RA = 229
36241 deg
ZDOT = -3276
946627 TA = 12
94570
MA = 12
90092
Ha = 188
901 n
mi
Hp = 175
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16527404
75 X = 5010468
24
Y = 1571763
46 feet Y = 535254
53 meter
Z = 14421047
11 Z = 4419942
46
XDOT = 7328
192917 XDOT = 2175
346013
YDOT = 21723
455615 feet/sec YDOT = 6645
961273 meter/sec
ZDOT = -10751
137229 ZDOT = -3266
236584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5610377
70 X = -1710043
12
Y = 15540740
64 feet Y = 4736817
75 meter
Z = 14512104
96 Z = 4423289
59
XDOT = -21744
756634 XDOT = -6627
801822
YDOT = 2165
291877 feet/sec YDOT = 659
980964 meter/sec
ZDOT = -10710
303559 ZDOT = -3264
500525
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 06299
65708562
00020000 00000-0 20000-3 0 9026
2 25544 51
6343 230
0621 0012184 139
6206 220
5865 15
77308058 13906
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
65708562 = yrday
fracday
Element set: 902
Inclination: 51
6343 deg
RA of node: 230
0621 deg
Eccentricity:
0012184
Arg of perigee: 139
6206 deg
Mean anomaly: 220
5865 deg
Mean motion: 15
77308058 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1390
Checksum: 284
Coasting Arc #4 (Orbit 1405)
---------------------------------------
Vector Time (GMT): 2006/300/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1352723
11 A = 6716852
60 meter
Y = -5436289
60 meter E =
0022010
Z = 3699008
35 I = 51
41390
XDOT = 6274
850197 Wp = 120
25686
YDOT = 1360
489761 meter/sec RA = 224
23432 deg
ZDOT = 4264
382783 TA = 284
56591
MA = 284
80992
Ha = 188
997 n
mi
Hp = 175
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4438067
94 X = -1309802
71
Y = -17835595
80 feet Y = -5451176
74 meter
Z = 12135854
15 Z = 3692540
61
XDOT = 20586
778861 XDOT = 6238
454613
YDOT = 4463
549085 feet/sec YDOT = 1430
454861 meter/sec
ZDOT = 13990
757161 ZDOT = 4294
778321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18394202
70 X = 5606552
98
Y = -246977
85 feet Y = -75278
85 meter
Z = 12110994
57 Z = 3691431
15
XDOT = -9114
944812 XDOT = -2778
235179
YDOT = 17574
150632 feet/sec YDOT = 5356
601113 meter/sec
ZDOT = 14104
273207 ZDOT = 4298
982474
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 06300
67079313
00020000 00000-0 20000-3 0 9037
2 25544 51
6343 224
8298 0012219 143
4657 216
7344 15
77303065 14069
Satellite: ISS
Catalog Number: 25544
Epoch time: 06300
67079313 = yrday
fracday
Element set: 903
Inclination: 51
6343 deg
RA of node: 224
8298 deg
Eccentricity:
0012219
Arg of perigee: 143
4657 deg
Mean anomaly: 216
7344 deg
Mean motion: 15
77303065 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1406
Checksum: 278
Coasting Arc #5 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2006/301/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5824326
91 A = 6719043
47 meter
Y = -1796940
94 meter E =
0013411
Z = -2847494
02 I = 51
44313
XDOT = -694
879180 Wp = 128
09910
YDOT = -5752
572315 meter/sec RA = 219
00744 deg
ZDOT = 5059
540612 TA = 199
13157
MA = 199
18199
Ha = 188
763 n
mi
Hp = 175
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19108684
09 X = -5789967
55
Y = -5895475
52 feet Y = -1861879
52 meter
Z = -9342171
99 Z = -2875705
71
XDOT = -2279
787335 XDOT = -655
080209
YDOT = -18873
268751 feet/sec YDOT = -5760
120588 meter/sec
ZDOT = 16599
542690 ZDOT = 5056
261193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9856278
04 X = 3004193
55
Y = -17342747
98 feet Y = -5286069
58 meter
Z = -9447618
34 Z = -2879634
07
XDOT = 17677
098668 XDOT = 5387
979674
YDOT = 1024
774917 feet/sec YDOT = 312
351395 meter/sec
ZDOT = 16586
523015 ZDOT = 5055
572215
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 06301
62112097
00020000 00000-0 20000-3 0 9041
2 25544 51
6341 219
9243 0012080 147
7558 212
4348 15
77348998 14213
Satellite: ISS
Catalog Number: 25544
Epoch time: 06301
62112097 = yrday
fracday
Element set: 904
Inclination: 51
6341 deg
RA of node: 219
9243 deg
Eccentricity:
0012080
Arg of perigee: 147
7558 deg
Mean anomaly: 212
4348 deg
Mean motion: 15
77348998 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1421
Checksum: 286
Coasting Arc #6 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2006/302/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -269483
55 A = 6711915
05 meter
Y = 4556174
61 meter E =
0019306
Z = -4934278
30 I = 51
44173
XDOT = -6919
525832 Wp = 112
12264
YDOT = -2647
590808 meter/sec RA = 213
87233 deg
ZDOT = -2080
437222 TA = 137
72557
MA = 137
57659
Ha = 188
565 n
mi
Hp = 175
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -884132
39 X = -296441
16
Y = 14948079
44 feet Y = 4553010
57 meter
Z = -16188577
09 Z = -4935652
77
XDOT = -22701
856403 XDOT = -6879
299307
YDOT = -8686
321548 feet/sec YDOT = -2724
743783 meter/sec
ZDOT = -6825
581438 ZDOT = -2113
955113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14493955
88 X = -4417757
75
Y = -3742516
76 feet Y = -1140719
11 meter
Z = -16193072
86 Z = -4935648
61
XDOT = 12734
177334 XDOT = 3881
377251
YDOT = -19434
913683 feet/sec YDOT = -5923
761691 meter/sec
ZDOT = -6950
946774 ZDOT = -2118
648577
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 06302
63478205
00020000 00000-0 20000-3 0 9050
2 25544 51
6336 214
6912 0012013 151
9803 208
2011 15
77396520 14379
Satellite: ISS
Catalog Number: 25544
Epoch time: 06302
63478205 = yrday
fracday
Element set: 905
Inclination: 51
6336 deg
RA of node: 214
6912 deg
Eccentricity:
0012013
Arg of perigee: 151
9803 deg
Mean anomaly: 208
2011 deg
Mean motion: 15
77396520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1437
Checksum: 261
Coasting Arc #7 (Orbit 1452)
---------------------------------------
Vector Time (GMT): 2006/303/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6100095
94 A = 6722347
67 meter
Y = 2700941
71 meter E =
0024913
Z = 700728
22 I = 51
50146
XDOT = -1371
637315 Wp = 141
19775
YDOT = 4675
029241 meter/sec RA = 208
67472 deg
ZDOT = -5984
246213 TA = 31
13174
MA = 30
98438
Ha = 188
561 n
mi
Hp = 175
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20013438
12 X = 6066036
21
Y = 8861357
30 feet Y = 2768965
91 meter
Z = 2298977
11 Z = 730280
15
XDOT = -4500
122423 XDOT = -1394
741467
YDOT = 15338
022445 feet/sec YDOT = 4659
561749 meter/sec
ZDOT = -19633
353718 ZDOT = -5990
965750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12341799
56 X = -3761780
51
Y = 18061577
98 feet Y = 5505168
97 meter
Z = 2409572
35 Z = 734437
65
XDOT = -12970
266809 XDOT = -3953
337324
YDOT = -6200
647758 feet/sec YDOT = -1889
957437 meter/sec
ZDOT = -19657
764359 ZDOT = -5991
686577
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 06303
64842209
00020000 00000-0 20000-3 0 9062
2 25544 51
6338 209
4589 0012231 155
9353 204
2386 15
77382343 14536
Satellite: ISS
Catalog Number: 25544
Epoch time: 06303
64842209 = yrday
fracday
Element set: 906
Inclination: 51
6338 deg
RA of node: 209
4589 deg
Eccentricity:
0012231
Arg of perigee: 155
9353 deg
Mean anomaly: 204
2386 deg
Mean motion: 15
77382343 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1453
Checksum: 290
Coasting Arc #8 (Orbit 1468)
---------------------------------------
Vector Time (GMT): 2006/304/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2163830
46 A = 6710314
27 meter
Y = -3596750
60 meter E =
0012306
Z = 5229051
36 I = 51
48702
XDOT = 6889
616856 Wp = 147
82983
YDOT = 3430
963375 meter/sec RA = 203
50493 deg
ZDOT = -500
763579 TA = 306
87341
MA = 306
98615
Ha = 188
266 n
mi
Hp = 175
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7099181
30 X = 2178486
88
Y = -11800362
87 feet Y = -3572471
46 meter
Z = 17155680
32 Z = 5239599
02
XDOT = 22603
729843 XDOT = 6853
171945
YDOT = 11256
441518 feet/sec YDOT = 3507
803115 meter/sec
ZDOT = -1642
925128 ZDOT = -467
381935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10488240
68 X = 3196815
76
Y = 8849273
90 feet Y = 2697258
69 meter
Z = 17194518
45 Z = 5240889
22
XDOT = -14175
995807 XDOT = -4320
843522
YDOT = 19689
045103 feet/sec YDOT = 6001
220947 meter/sec
ZDOT = -1517
932227 ZDOT = -462
665743
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 06304
66203629
00020000 00000-0 20000-3 0 9073
2 25544 51
6335 204
2257 0012025 160
1671 199
9963 15
77460981 14693
Satellite: ISS
Catalog Number: 25544
Epoch time: 06304
66203629 = yrday
fracday
Element set: 907
Inclination: 51
6335 deg
RA of node: 204
2257 deg
Eccentricity:
0012025
Arg of perigee: 160
1671 deg
Mean anomaly: 199
9963 deg
Mean motion: 15
77460981 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1469
Checksum: 298
Coasting Arc #9 (Orbit 1484)
---------------------------------------
Vector Time (GMT): 2006/305/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5694330
96 A = 6721150
63 meter
Y = -3205335
21 meter E =
0016492
Z = 1573546
18 I = 51
54993
XDOT = 3634
537218 Wp = 108
16540
YDOT = -3606
365449 meter/sec RA = 198
35210 deg
ZDOT = 5752
162462 TA = 269
22848
MA = 269
41744
Ha = 188
107 n
mi
Hp = 176
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18682188
19 X = -5665709
37
Y = -10516191
63 feet Y = -3268852
30 meter
Z = 5162553
07 Z = 1545952
26
XDOT = 11924
334704 XDOT = 3646
650530
YDOT = -11831
907640 feet/sec YDOT = -3565
654153 meter/sec
ZDOT = 18871
924087 ZDOT = 5769
848862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13159853
28 X = 4011123
28
Y = -16955513
47 feet Y = -5168040
51 meter
Z = 5059171
94 Z = 1542035
61
XDOT = 8723
733330 XDOT = 2658
993919
YDOT = 12475
547126 feet/sec YDOT = 3802
546764 meter/sec
ZDOT = 18937
389482 ZDOT = 5772
116314
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 06305
67562819
00020000 00000-0 20000-3 0 9085
2 25544 51
6328 198
9918 0012019 164
7669 195
3860 15
77519156 14851
Satellite: ISS
Catalog Number: 25544
Epoch time: 06305
67562819 = yrday
fracday
Element set: 908
Inclination: 51
6328 deg
RA of node: 198
9918 deg
Eccentricity:
0012019
Arg of perigee: 164
7669 deg
Mean anomaly: 195
3860 deg
Mean motion: 15
77519156 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1485
Checksum: 338
Coasting Arc #10 (Orbit 1499)
---------------------------------------
Vector Time (GMT): 2006/306/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4143850
93 A = 6713101
63 meter
Y = 2732382
84 meter E =
0019480
Z = -4537821
26 I = 51
54969
XDOT = -5904
591194 Wp = 141
96862
YDOT = -3869
110453 meter/sec RA = 193
14430 deg
ZDOT = 3054
090557 TA = 158
53727
MA = 158
45548
Ha = 187
950 n
mi
Hp = 176
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13595311
45 X = -4152052
42
Y = 8964510
63 feet Y = 2685997
99 meter
Z = -14887865
04 Z = -4557972
56
XDOT = -19372
018354 XDOT = -5875
723974
YDOT = -12693
931934 feet/sec YDOT = -3934
977364 meter/sec
ZDOT = 10019
982141 ZDOT = 3025
475654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7126066
74 X = -2172025
14
Y = -14566458
63 feet Y = -4439856
59 meter
Z = -14962651
03 Z = -4560616
03
XDOT = 14056
688948 XDOT = 4284
478791
YDOT = -17086
285737 feet/sec YDOT = -5207
899893 meter/sec
ZDOT = 9912
693750 ZDOT = 3021
389055
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 06306
62585225
00020000 00000-0 20000-3 0 9098
2 25544 51
6319 194
0845 0011971 168
2080 191
9368 15
77529713 15002
Satellite: ISS
Catalog Number: 25544
Epoch time: 06306
62585225 = yrday
fracday
Element set: 909
Inclination: 51
6319 deg
RA of node: 194
0845 deg
Eccentricity:
0011971
Arg of perigee: 168
2080 deg
Mean anomaly: 191
9368 deg
Mean motion: 15
77529713 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1500
Checksum: 302
Coasting Arc #11 (Orbit 1515)
---------------------------------------
Vector Time (GMT): 2006/307/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4412667
63 A = 6716397
06 meter
Y = 3527718
52 meter E =
0013032
Z = -3628376
76 I = 51
58803
XDOT = -5740
288182 Wp = 147
53092
YDOT = 2696
170438 meter/sec RA = 188
02607 deg
ZDOT = -4377
736679 TA = 76
07274
MA = 75
92783
Ha = 187
843 n
mi
Hp = 176
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14477255
99 X = 4390518
73
Y = 11573879
65 feet Y = 3576939
50 meter
Z = -11904123
24 Z = -3606993
29
XDOT = -18832
966477 XDOT = -5748
743639
YDOT = 8845
703536 feet/sec YDOT = 2631
931979 meter/sec
ZDOT = -14362
653145 ZDOT = -4405
644392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13147482
91 X = -4007352
79
Y = 13137499
35 feet Y = 4004309
80 meter
Z = -11823856
60 Z = -3603911
49
XDOT = -5705
652392 XDOT = -1739
082849
YDOT = -18676
247994 feet/sec YDOT = -5692
520389 meter/sec
ZDOT = -14466
384263 ZDOT = -4409
353923
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 06307
63940193
00020000 00000-0 20000-3 0 9101
2 25544 51
6311 188
8516 0011936 172
2400 187
8951 15
77555640 15169
Satellite: ISS
Catalog Number: 25544
Epoch time: 06307
63940193 = yrday
fracday
Element set: 910
Inclination: 51
6311 deg
RA of node: 188
8516 deg
Eccentricity:
0011936
Arg of perigee: 172
2400 deg
Mean anomaly: 187
8951 deg
Mean motion: 15
77555640 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1516
Checksum: 292
Coasting Arc #12 (Orbit 1531)
---------------------------------------
Vector Time (GMT): 2006/308/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5702045
61 A = 6718120
58 meter
Y = -2015947
29 meter E =
0019439
Z = 2895552
48 I = 51
62351
XDOT = 4052
516662 Wp = 134
67661
YDOT = 4201
429000 meter/sec RA = 182
80991 deg
ZDOT = -5048
112161 TA = 11
89893
MA = 11
85307
Ha = 187
414 n
mi
Hp = 176
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18707498
73 X = 5710097
89
Y = -6614000
28 feet Y = -1952138
84 meter
Z = 9499844
11 Z = 2923273
49
XDOT = 13295
658339 XDOT = 4029
758132
YDOT = 13784
215879 feet/sec YDOT = 4246
619265 meter/sec
ZDOT = -16562
047773 ZDOT = -5028
479645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4788504
81 X = 1459536
27
Y = 19204569
65 feet Y = 5853552
83 meter
Z = 9602982
49 Z = 2926989
06
XDOT = -13608
044924 XDOT = -4147
732093
YDOT = 11649
367611 feet/sec YDOT = 3550
727248 meter/sec
ZDOT = -16488
218265 ZDOT = -5025
608927
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 06308
65292776
00020000 00000-0 20000-3 0 9112
2 25544 51
6314 183
6176 0011811 176
9249 183
1990 15
77630260 15323
Satellite: ISS
Catalog Number: 25544
Epoch time: 06308
65292776 = yrday
fracday
Element set: 911
Inclination: 51
6314 deg
RA of node: 183
6176 deg
Eccentricity:
0011811
Arg of perigee: 176
9249 deg
Mean anomaly: 183
1990 deg
Mean motion: 15
77630260 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1532
Checksum: 297
Coasting Arc #13 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2006/309/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2493923
59 A = 6711421
37 meter
Y = -3807907
47 meter E =
0016227
Z = 4932276
21 I = 51
62707
XDOT = 7154
965226 Wp = 161
26763
YDOT = -1949
711666 meter/sec RA = 177
68639 deg
ZDOT = 2095
526451 TA = 268
34465
MA = 268
53053
Ha = 187
550 n
mi
Hp = 176
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8182164
02 X = -2475118
62
Y = -12493134
75 feet Y = -3835690
96 meter
Z = 16182008
55 Z = 4920205
84
XDOT = 23474
295360 XDOT = 7166
055356
YDOT = -6396
691816 feet/sec YDOT = -1869
638950 meter/sec
ZDOT = 6875
086783 ZDOT = 2130
313335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13108265
87 X = 3995399
44
Y = -7257551
20 feet Y = -2212101
61 meter
Z = 16136447
61 Z = 4918389
23
XDOT = 3994
153064 XDOT = 1217
417854
YDOT = 22912
550706 feet/sec YDOT = 6983
745455 meter/sec
ZDOT = 7004
608663 ZDOT = 2135
004720
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 06309
66643544
00020000 00000-0 20000-3 0 9128
2 25544 51
6297 178
3832 0011886 179
9056 180
2113 15
77587604 15489
Satellite: ISS
Catalog Number: 25544
Epoch time: 06309
66643544 = yrday
fracday
Element set: 912
Inclination: 51
6297 deg
RA of node: 178
3832 deg
Eccentricity:
0011886
Arg of perigee: 179
9056 deg
Mean anomaly: 180
2113 deg
Mean motion: 15
77587604 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1548
Checksum: 319
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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