Date:
October 12th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4520 84 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 1150)
---------------------------------------
Vector Time (GMT): 2006/284/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4171177
72 A = 6724132
22 meter
Y = 5267576
18 meter E =
0022360
Z = -87499
84 I = 51
40487
XDOT = -3729
711857 Wp = 108
16404
YDOT = -3032
441611 meter/sec RA = 307
77872 deg
ZDOT = -6020
937936 TA = 72
79058
MA = 72
54595
Ha = 190
405 n
mi
Hp = 174
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13684966
26 X = -4229345
40
Y = 17282074
07 feet Y = 5220606
53 meter
Z = -287072
95 Z = -107904
97
XDOT = -12236
587457 XDOT = -3666
276300
YDOT = -9948
955417 feet/sec YDOT = -3073
794500 meter/sec
ZDOT = -19753
733385 ZDOT = -6038
903191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9725070
27 X = 2964201
42
Y = -19781872
19 feet Y = -6029514
64 meter
Z = -362405
13 Z = -110461
09
XDOT = 12512
300459 XDOT = 3813
749180
YDOT = 6454
231989 feet/sec YDOT = 1967
249910 meter/sec
ZDOT = -19821
064787 ZDOT = -6041
460547
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 06284
51212143
00020000 00000-0 20000-3 0 9008
2 25544 51
6351 308
1888 0012886 83
1185 277
1445 15
76829739 11515
Satellite: ISS
Catalog Number: 25544
Epoch time: 06284
51212143 = yrday
fracday
Element set: 900
Inclination: 51
6351 deg
RA of node: 308
1888 deg
Eccentricity:
0012886
Arg of perigee: 83
1185 deg
Mean anomaly: 277
1445 deg
Mean motion: 15
76829739 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1151
Checksum: 295
Coasting Arc #2 (Orbit 1166)
---------------------------------------
Vector Time (GMT): 2006/285/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2755555
65 A = 6712420
19 meter
Y = 3312229
41 meter E =
0016479
Z = 5133722
11 I = 51
34844
XDOT = -4867
098544 Wp = 79
15904
YDOT = 5874
004198 meter/sec RA = 302
59162 deg
ZDOT = -1171
176643 TA = 22
08098
MA = 22
01008
Ha = 190
314 n
mi
Hp = 174
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9040536
92 X = 2693374
00
Y = 10866894
38 feet Y = 3342695
76 meter
Z = 16842920
29 Z = 5146957
82
XDOT = -15968
171077 XDOT = -4926
731295
YDOT = 19271
667316 feet/sec YDOT = 5819
244210 meter/sec
ZDOT = -3842
443054 ZDOT = -1194
966048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11189007
35 X = -3410409
44
Y = -8540985
64 feet Y = -2603292
42 meter
Z = 16892671
31 Z = 5148886
22
XDOT = 10510
941741 XDOT = 3203
735043
YDOT = -21583
550551 feet/sec YDOT = -6578
666208 meter/sec
ZDOT = -3930
309104 ZDOT = -1197
958215
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 06285
52612689
00020000 00000-0 20000-3 0 9010
2 25544 51
6343 302
9590 0012917 86
8256 273
4386 15
76861659 11679
Satellite: ISS
Catalog Number: 25544
Epoch time: 06285
52612689 = yrday
fracday
Element set: 901
Inclination: 51
6343 deg
RA of node: 302
9590 deg
Eccentricity:
0012917
Arg of perigee: 86
8256 deg
Mean anomaly: 273
4386 deg
Mean motion: 15
76861659 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1167
Checksum: 321
Coasting Arc #3 (Orbit 1182)
---------------------------------------
Vector Time (GMT): 2006/286/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4241131
42 A = 6722425
77 meter
Y = -4835253
69 meter E =
0026602
Z = 1921338
02 I = 51
36807
XDOT = 2662
538134 Wp = 78
12573
YDOT = 4584
435600 meter/sec RA = 297
44240 deg
ZDOT = 5600
211305 TA = 303
36873
MA = 303
62303
Ha = 190
387 n
mi
Hp = 174
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13914473
16 X = 4285551
08
Y = -15863693
21 feet Y = -4787578
68 meter
Z = 6303602
43 Z = 1942049
46
XDOT = 8735
361331 XDOT = 2583
871372
YDOT = 15040
799211 feet/sec YDOT = 4613
769636 meter/sec
ZDOT = 18373
396671 ZDOT = 5612
955035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9576217
88 X = -2918831
21
Y = 18777502
81 feet Y = 5723382
86 meter
Z = 6380138
61 Z = 1944666
25
XDOT = -10682
127465 XDOT = -3255
912451
YDOT = -11772
710752 feet/sec YDOT = -3588
322237 meter/sec
ZDOT = 18421
487496 ZDOT = 5614
869389
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 06286
54011817
00020000 00000-0 20000-3 0 9020
2 25544 51
6344 297
7293 0012963 90
1337 270
1313 15
76856351 11835
Satellite: ISS
Catalog Number: 25544
Epoch time: 06286
54011817 = yrday
fracday
Element set: 902
Inclination: 51
6344 deg
RA of node: 297
7293 deg
Eccentricity:
0012963
Arg of perigee: 90
1337 deg
Mean anomaly: 270
1313 deg
Mean motion: 15
76856351 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1183
Checksum: 287
Coasting Arc #4 (Orbit 1197)
---------------------------------------
Vector Time (GMT): 2006/287/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1932516
84 A = 6715394
71 meter
Y = -4670063
21 meter E =
0022205
Z = -4442846
66 I = 51
33300
XDOT = 4834
450135 Wp = 100
76554
YDOT = -5044
153953 meter/sec RA = 292
22218 deg
ZDOT = 3208
765322 TA = 201
49937
MA = 201
59277
Ha = 190
335 n
mi
Hp = 174
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6340278
35 X = -1858569
22
Y = -15321729
70 feet Y = -4691260
21 meter
Z = -14576268
56 Z = -4452055
28
XDOT = 15861
056873 XDOT = 4874
907545
YDOT = -16549
061524 feet/sec YDOT = -4989
866253 meter/sec
ZDOT = 10527
445281 ZDOT = 3232
349501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10045956
45 X = 3062007
53
Y = 13153463
34 feet Y = 4009175
63 meter
Z = -14611204
49 Z = -4453495
13
XDOT = -9969
942346 XDOT = -3038
838427
YDOT = 19371
051220 feet/sec YDOT = 5904
296412 meter/sec
ZDOT = 10614
658305 ZDOT = 3235
347852
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 06287
49071871
00020000 00000-0 20000-3 0 9032
2 25544 51
6348 292
8261 0012833 93
6826 266
5807 15
76871798 11982
Satellite: ISS
Catalog Number: 25544
Epoch time: 06287
49071871 = yrday
fracday
Element set: 903
Inclination: 51
6348 deg
RA of node: 292
8261 deg
Eccentricity:
0012833
Arg of perigee: 93
6826 deg
Mean anomaly: 266
5807 deg
Mean motion: 15
76871798 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1198
Checksum: 336
Coasting Arc #5 (Orbit 1213)
---------------------------------------
Vector Time (GMT): 2006/288/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4193387
91 A = 6718188
05 meter
Y = 3832574
40 meter E =
0018254
Z = -3601213
31 I = 51
33198
XDOT = -1800
409675 Wp = 92
37493
YDOT = -6064
872511 meter/sec RA = 287
09137 deg
ZDOT = -4377
892089 TA = 130
91777
MA = 130
75956
Ha = 190
266 n
mi
Hp = 174
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13757834
35 X = -4218438
48
Y = 12574062
98 feet Y = 3785541
49 meter
Z = -11815004
30 Z = -3621645
81
XDOT = -5906
855890 XDOT = -1711
190486
YDOT = -19897
875692 feet/sec YDOT = -6084
506903 meter/sec
ZDOT = -14363
163023 ZDOT = -4386
421729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9659054
25 X = 2944079
73
Y = -15883793
98 feet Y = -4841380
41 meter
Z = -11890632
96 Z = -3624264
93
XDOT = 9968
853848 XDOT = 3038
506653
YDOT = 16790
396037 feet/sec YDOT = 5117
712712 meter/sec
ZDOT = -14395
762411 ZDOT = -4387
828383
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 06288
50467804
00020000 00000-0 20000-3 0 9041
2 25544 51
6334 287
5949 0012875 97
7983 262
4644 15
76908747 12144
Satellite: ISS
Catalog Number: 25544
Epoch time: 06288
50467804 = yrday
fracday
Element set: 904
Inclination: 51
6334 deg
RA of node: 287
5949 deg
Eccentricity:
0012875
Arg of perigee: 97
7983 deg
Mean anomaly: 262
4644 deg
Mean motion: 15
76908747 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1214
Checksum: 337
Coasting Arc #6 (Orbit 1229)
---------------------------------------
Vector Time (GMT): 2006/289/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1286457
98 A = 6719614
41 meter
Y = 5824017
46 meter E =
0025936
Z = 3068715
78 I = 51
32939
XDOT = -4749
695110 Wp = 97
84851
YDOT = 3634
372499 meter/sec RA = 281
85967 deg
ZDOT = -4874
850681 TA = 46
27945
MA = 46
06495
Ha = 190
141 n
mi
Hp = 174
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4220662
66 X = 1206330
03
Y = 19107668
84 feet Y = 5837955
43 meter
Z = 10067965
16 Z = 3074770
61
XDOT = -15582
989206 XDOT = -4766
300856
YDOT = 11923
794288 feet/sec YDOT = 3581
165771 meter/sec
ZDOT = -15993
604596 ZDOT = -4897
965305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9605008
19 X = -2927606
50
Y = -17034965
68 feet Y = -5192257
54 meter
Z = 10091317
36 Z = 3075833
53
XDOT = 10055
809747 XDOT = 3065
010811
YDOT = -15256
226691 feet/sec YDOT = -4650
097895 meter/sec
ZDOT = -16079
253006 ZDOT = -4900
956316
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 06289
51862047
00020000 00000-0 20000-3 0 9052
2 25544 51
6326 282
3642 0012824 100
8898 259
3711 15
76968445 12302
Satellite: ISS
Catalog Number: 25544
Epoch time: 06289
51862047 = yrday
fracday
Element set: 905
Inclination: 51
6326 deg
RA of node: 282
3642 deg
Eccentricity:
0012824
Arg of perigee: 100
8898 deg
Mean anomaly: 259
3711 deg
Mean motion: 15
76968445 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1230
Checksum: 306
Coasting Arc #7 (Orbit 1245)
---------------------------------------
Vector Time (GMT): 2006/290/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4098878
36 A = 6713860
89 meter
Y = -2401505
95 meter E =
0019999
Z = 4730876
86 I = 51
30459
XDOT = 1223
678201 Wp = 110
09973
YDOT = 7173
370813 meter/sec RA = 276
72353 deg
ZDOT = 2565
618620 TA = 314
60316
MA = 314
76616
Ha = 190
048 n
mi
Hp = 174
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13447763
66 X = 4102445
74
Y = -7878956
52 feet Y = -2355649
85 meter
Z = 15521249
53 Z = 4750798
17
XDOT = 4014
692262 XDOT = 1130
910199
YDOT = 23534
681145 feet/sec YDOT = 7186
536091 meter/sec
ZDOT = 8417
383924 ZDOT = 2571
337627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10251831
44 X = -3124758
22
Y = 11641320
11 feet Y = 3548274
37 meter
Z = 15595162
98 Z = 4753405
67
XDOT = -10236
331291 XDOT = -3120
033777
YDOT = -20388
670331 feet/sec YDOT = -6214
466717 meter/sec
ZDOT = 8439
675484 ZDOT = 2572
413087
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 06290
53254775
00020000 00000-0 20000-3 0 9060
2 25544 51
6318 277
1336 0012767 104
9488 255
3092 15
76963974 12468
Satellite: ISS
Catalog Number: 25544
Epoch time: 06290
53254775 = yrday
fracday
Element set: 906
Inclination: 51
6318 deg
RA of node: 277
1336 deg
Eccentricity:
0012767
Arg of perigee: 104
9488 deg
Mean anomaly: 255
3092 deg
Mean motion: 15
76963974 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1246
Checksum: 320
Coasting Arc #8 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2006/291/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -869911
41 A = 6722840
39 meter
Y = -6538968
45 meter E =
0017925
Z = -1302009
74 I = 51
33338
XDOT = 4710
345427 Wp = 80
52217
YDOT = -1772
566644 meter/sec RA = 271
50948 deg
ZDOT = 5826
101383 TA = 265
11836
MA = 265
32304
Ha = 190
092 n
mi
Hp = 174
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2854040
05 X = -790402
09
Y = -21453308
58 feet Y = -6548251
80 meter
Z = -4271685
51 Z = -1306042
32
XDOT = 15453
889196 XDOT = 4701
513906
YDOT = -5815
507362 feet/sec YDOT = -1719
941994 meter/sec
ZDOT = 19114
505849 ZDOT = 5848
963190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9691264
47 X = 2953897
41
Y = 19347688
95 feet Y = 5897175
59 meter
Z = -4287611
89 Z = -1306864
10
XDOT = -11191
092071 XDOT = -3411
044863
YDOT = 9808
942788 feet/sec YDOT = 2989
765762 meter/sec
ZDOT = 19199
462423 ZDOT = 5851
996147
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 06291
48308869
00020000 00000-0 20000-3 0 9070
2 25544 51
6317 272
2302 0012948 108
8267 251
4303 15
77019679 12619
Satellite: ISS
Catalog Number: 25544
Epoch time: 06291
48308869 = yrday
fracday
Element set: 907
Inclination: 51
6317 deg
RA of node: 272
2302 deg
Eccentricity:
0012948
Arg of perigee: 108
8267 deg
Mean anomaly: 251
4303 deg
Mean motion: 15
77019679 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1261
Checksum: 301
Coasting Arc #9 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2006/292/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4171357
58 A = 6711616
53 meter
Y = 617363
33 meter E =
0027138
Z = -5244427
99 I = 51
29553
XDOT = -741
851400 Wp = 98
84647
YDOT = -7643
645620 meter/sec RA = 266
34141 deg
ZDOT = -315
234547 TA = 168
17284
MA = 168
10898
Ha = 190
032 n
mi
Hp = 174
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13685556
35 X = -4152474
05
Y = 2025470
24 feet Y = 570822
16 meter
Z = -17206128
57 Z = -5264646
97
XDOT = -2433
895670 XDOT = -654
792578
YDOT = -25077
577495 feet/sec YDOT = -7651
454663 meter/sec
ZDOT = -1034
234077 ZDOT = -318
626593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12069238
12 X = 3678703
78
Y = -6567703
92 feet Y = -2001836
16 meter
Z = -17281394
59 Z = -5267369
07
XDOT = 10409
994098 XDOT = 3172
966201
YDOT = 21840
189396 feet/sec YDOT = 6656
889728 meter/sec
ZDOT = -1047
930123 ZDOT = -319
409101
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 06292
49698307
00020000 00000-0 20000-3 0 9082
2 25544 51
6314 266
9978 0012755 112
2225 248
0294 15
76997878 12777
Satellite: ISS
Catalog Number: 25544
Epoch time: 06292
49698307 = yrday
fracday
Element set: 908
Inclination: 51
6314 deg
RA of node: 266
9978 deg
Eccentricity:
0012755
Arg of perigee: 112
2225 deg
Mean anomaly: 248
0294 deg
Mean motion: 15
76997878 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1277
Checksum: 341
Coasting Arc #10 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2006/293/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 416580
87 A = 6723268
61 meter
Y = 6659342
52 meter E =
0022658
Z = -764134
61 I = 51
33890
XDOT = -4879
012928 Wp = 126
88131
YDOT = -362
805840 meter/sec RA = 261
16354 deg
ZDOT = -5956
438405 TA = 61
49711
MA = 61
26912
Ha = 189
898 n
mi
Hp = 174
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1366735
12 X = 345796
32
Y = 21848236
61 feet Y = 6663605
14 meter
Z = -2507003
33 Z = -762283
14
XDOT = -16007
260264 XDOT = -4845
657402
YDOT = -1190
307875 feet/sec YDOT = -417
179506 meter/sec
ZDOT = -19542
120751 ZDOT = -5980
060142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9139994
38 X = -2785870
29
Y = -19892537
93 feet Y = -6063245
56 meter
Z = -2499182
06 Z = -761750
69
XDOT = 13814
079210 XDOT = 4210
531343
YDOT = -3936
627002 feet/sec YDOT = -1199
883910 meter/sec
ZDOT = -19630
203812 ZDOT = -5983
286122
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 06293
51086011
00020000 00000-0 20000-3 0 9090
2 25544 51
6318 261
7661 0012695 115
5816 244
6662 15
77047119 12932
Satellite: ISS
Catalog Number: 25544
Epoch time: 06293
51086011 = yrday
fracday
Element set: 909
Inclination: 51
6318 deg
RA of node: 261
7661 deg
Eccentricity:
0012695
Arg of perigee: 115
5816 deg
Mean anomaly: 244
6662 deg
Mean motion: 15
77047119 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1293
Checksum: 294
Coasting Arc #11 (Orbit 1308)
---------------------------------------
Vector Time (GMT): 2006/294/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4373883
03 A = 6712676
48 meter
Y = 1205813
64 meter E =
0016091
Z = 4932757
90 I = 51
30900
XDOT = 209
025409 Wp = 100
36393
YDOT = 7450
487034 meter/sec RA = 255
95799 deg
ZDOT = -2003
957386 TA = 9
08033
MA = 9
05127
Ha = 189
675 n
mi
Hp = 174
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14350009
93 X = 4336111
28
Y = 3956081
49 feet Y = 1254513
86 meter
Z = 16183588
91 Z = 4953914
99
XDOT = 685
778901 XDOT = 135
432620
YDOT = 24443
855099 feet/sec YDOT = 7452
412902 meter/sec
ZDOT = -6574
663341 ZDOT = -2003
121019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14702580
25 X = -4481346
46
Y = 1686340
01 feet Y = 513996
43 meter
Z = 16262604
56 Z = 4956841
87
XDOT = -9721
850791 XDOT = -2963
220121
YDOT = -21313
276372 feet/sec YDOT = -6496
286638 meter/sec
ZDOT = -6570
515351 ZDOT = -2002
693079
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 06294
52471999
00020000 00000-0 20000-3 0 9107
2 25544 51
6317 256
5352 0012569 119
6872 240
5545 15
77070857 13095
Satellite: ISS
Catalog Number: 25544
Epoch time: 06294
52471999 = yrday
fracday
Element set: 910
Inclination: 51
6317 deg
RA of node: 256
5352 deg
Eccentricity:
0012569
Arg of perigee: 119
6872 deg
Mean anomaly: 240
5545 deg
Mean motion: 15
77070857 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1309
Checksum: 314
Coasting Arc #12 (Orbit 1324)
---------------------------------------
Vector Time (GMT): 2006/295/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 114797
52 A = 6720178
03 meter
Y = -6161205
08 meter E =
0024256
Z = 2666586
01 I = 51
34371
XDOT = 5203
294268 Wp = 100
25660
YDOT = 2356
142432 meter/sec RA = 250
81612 deg
ZDOT = 5175
799923 TA = 290
31146
MA = 290
57197
Ha = 189
668 n
mi
Hp = 174
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 376632
27 X = 170730
25
Y = -20213927
44 feet Y = -6159608
54 meter
Z = 8748641
77 Z = 2667279
76
XDOT = 17071
175421 XDOT = 5151
416971
YDOT = 7730
126089 feet/sec YDOT = 2414
038648 meter/sec
ZDOT = 16980
970877 ZDOT = 5200
952205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7606775
62 X = 2318545
21
Y = 18731025
87 feet Y = 5709216
68 meter
Z = 8750376
09 Z = 2667114
63
XDOT = -17282
283428 XDOT = -5267
639989
YDOT = -1025
932324 feet/sec YDOT = -312
704172 meter/sec
ZDOT = 17075
037046 ZDOT = 5204
471291
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 06295
53856120
00020000 00000-0 20000-3 0 9113
2 25544 51
6324 251
3043 0012620 124
2854 235
9507 15
77135071 13257
Satellite: ISS
Catalog Number: 25544
Epoch time: 06295
53856120 = yrday
fracday
Element set: 911
Inclination: 51
6324 deg
RA of node: 251
3043 deg
Eccentricity:
0012620
Arg of perigee: 124
2854 deg
Mean anomaly: 235
9507 deg
Mean motion: 15
77135071 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1325
Checksum: 262
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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