Date:
October 3rd 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6727 44 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 1008)
---------------------------------------
Vector Time (GMT): 2006/275/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3993029
74 A = 6716499
42 meter
Y = 3110979
08 meter E =
0018581
Z = 4396645
99 I = 51
59701
XDOT = -6174
066549 Wp = 75
81197
YDOT = 3239
118165 meter/sec RA = 354
41047 deg
ZDOT = 3308
235870 TA = 340
99022
MA = 341
05948
Ha = 190
363 n
mi
Hp = 176
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13100491
28 X = 3936587
43
Y = 10206624
28 feet Y = 3155315
84 meter
Z = 14424691
56 Z = 4415907
00
XDOT = -20256
123847 XDOT = -6225
898784
YDOT = 10627
028100 feet/sec YDOT = 3169
786582 meter/sec
ZDOT = 10853
792224 ZDOT = 3278
116252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12140383
52 X = -3700388
90
Y = -11239301
93 feet Y = -3425739
23 meter
Z = 14496860
27 Z = 4418643
01
XDOT = 20298
744216 XDOT = 6187
057237
YDOT = -8040
783835 feet/sec YDOT = -2450
830913 meter/sec
ZDOT = 10741
998891 ZDOT = 3274
161262
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 06275
51168061
00020000 00000-0 20000-3 0 9007
2 25544 51
6376 354
5896 0012275 50
8487 309
3767 15
76508466 10092
Satellite: ISS
Catalog Number: 25544
Epoch time: 06275
51168061 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 354
5896 deg
Eccentricity:
0012275
Arg of perigee: 50
8487 deg
Mean anomaly: 309
3767 deg
Mean motion: 15
76508466 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1009
Checksum: 311
Coasting Arc #2 (Orbit 1023)
---------------------------------------
Vector Time (GMT): 2006/276/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5703562
66 A = 6723161
97 meter
Y = -2825245
54 meter E =
0018683
Z = -2153705
96 I = 51
59088
XDOT = 3901
496252 Wp = 48
79769
YDOT = 3706
258452 meter/sec RA = 349
21030 deg
ZDOT = 5513
170413 TA = 287
05806
MA = 287
26265
Ha = 190
602 n
mi
Hp = 176
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18712475
92 X = 5745193
37
Y = -9269178
27 feet Y = -2761232
46 meter
Z = -7065964
42 Z = -2125896
78
XDOT = 12800
184555 XDOT = 3832
980383
YDOT = 12159
640590 feet/sec YDOT = 3749
504298 meter/sec
ZDOT = 18087
829438 ZDOT = 5531
957305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19312439
39 X = -5886431
52
Y = 8034450
90 feet Y = 2448900
63 meter
Z = -6962726
32 Z = -2122238
98
XDOT = -11299
633187 XDOT = -3444
128195
YDOT = -11548
617453 feet/sec YDOT = -3520
018600 meter/sec
ZDOT = 18158
314103 ZDOT = 5534
654138
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 06276
46251659
00020000 00000-0 20000-3 0 9019
2 25544 51
6376 349
6892 0012396 53
2591 306
9710 15
76477635 10241
Satellite: ISS
Catalog Number: 25544
Epoch time: 06276
46251659 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 349
6892 deg
Eccentricity:
0012396
Arg of perigee: 53
2591 deg
Mean anomaly: 306
9710 deg
Mean motion: 15
76477635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1024
Checksum: 312
Coasting Arc #3 (Orbit 1039)
---------------------------------------
Vector Time (GMT): 2006/277/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2742530
35 A = 6713653
96 meter
Y = -3431456
88 meter E =
0025803
Z = -5099794
34 I = 51
53107
XDOT = 6822
883437 Wp = 68
34143
YDOT = -3197
278255 meter/sec RA = 344
08206 deg
ZDOT = -1514
608185 TA = 187
06194
MA = 187
09836
Ha = 190
515 n
mi
Hp = 175
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8997802
98 X = -2679181
54
Y = -11258060
63 feet Y = -3461771
54 meter
Z = -16731608
74 Z = -5112963
47
XDOT = 22384
788178 XDOT = 6865
486467
YDOT = -10489
758054 feet/sec YDOT = -3120
742896 meter/sec
ZDOT = -4969
186960 ZDOT = -1481
358812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8359036
48 X = 2547834
32
Y = 11669246
67 feet Y = 3556786
38 meter
Z = -16781129
58 Z = -5114888
30
XDOT = -22035
115487 XDOT = -6716
303200
YDOT = 8800
771016 feet/sec YDOT = 2682
475006 meter/sec
ZDOT = -4845
733187 ZDOT = -1476
979475
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 06277
47671913
00020000 00000-0 20000-3 0 9021
2 25544 51
6370 344
4610 0012333 57
5053 302
7301 15
76524118 10404
Satellite: ISS
Catalog Number: 25544
Epoch time: 06277
47671913 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 344
4610 deg
Eccentricity:
0012333
Arg of perigee: 57
5053 deg
Mean anomaly: 302
7301 deg
Mean motion: 15
76524118 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1040
Checksum: 257
Coasting Arc #4 (Orbit 1055)
---------------------------------------
Vector Time (GMT): 2006/278/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6121345
82 A = 6724779
61 meter
Y = 2741416
55 meter E =
0021024
Z = 446058
61 I = 51
54148
XDOT = -2341
468079 Wp = 96
38248
YDOT = -4211
728186 meter/sec RA = 338
90286 deg
ZDOT = -6008
444592 TA = 78
75633
MA = 78
52010
Ha = 190
550 n
mi
Hp = 175
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20083155
58 X = -6153712
66
Y = 8994148
79 feet Y = 2672783
34 meter
Z = 1463446
89 Z = 416242
01
XDOT = -7681
981887 XDOT = -2265
009758
YDOT = -13818
005858 feet/sec YDOT = -4237
484839 meter/sec
ZDOT = -19712
744724 ZDOT = -6019
633421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20355403
84 X = 6204327
09
Y = -8378376
38 feet Y = -2553729
12 meter
Z = 1352727
38 Z = 412311
31
XDOT = 6538
006767 XDOT = 1992
784463
YDOT = 12557
560258 feet/sec YDOT = 3827
544366 meter/sec
ZDOT = -19754
993032 ZDOT = -6021
321876
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 06278
49089965
00020000 00000-0 20000-3 0 9035
2 25544 51
6363 339
2326 0012546 61
4868 298
7558 15
76577291 10561
Satellite: ISS
Catalog Number: 25544
Epoch time: 06278
49089965 = yrday
fracday
Element set: 903
Inclination: 51
6363 deg
RA of node: 339
2326 deg
Eccentricity:
0012546
Arg of perigee: 61
4868 deg
Mean anomaly: 298
7558 deg
Mean motion: 15
76577291 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1056
Checksum: 338
Coasting Arc #5 (Orbit 1071)
---------------------------------------
Vector Time (GMT): 2006/279/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1360054
24 A = 6712633
27 meter
Y = 3970046
41 meter E =
0015153
Z = 5227819
18 I = 51
47548
XDOT = -7066
481970 Wp = 64
67941
YDOT = 3061
422556 meter/sec RA = 333
73783 deg
ZDOT = -479
005139 TA = 29
91508
MA = 29
82856
Ha = 190
395 n
mi
Hp = 175
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4462120
21 X = 1290163
37
Y = 13025086
66 feet Y = 3984865
02 meter
Z = 17151637
72 Z = 5234256
27
XDOT = -23183
995963 XDOT = -7097
863067
YDOT = 10044
037256 feet/sec YDOT = 2982
225730 meter/sec
ZDOT = -1571
539169 ZDOT = -513
411129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4194548
18 X = -1278498
28
Y = -13081578
24 feet Y = -3987265
05 meter
Z = 17176150
67 Z = 5235290
73
XDOT = 22352
031346 XDOT = 6812
899154
YDOT = -9430
395772 feet/sec YDOT = -2874
384631 meter/sec
ZDOT = -1699
308539 ZDOT = -517
949243
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 06279
50505554
00020000 00000-0 20000-3 0 9046
2 25544 51
6366 334
0037 0012406 64
6488 295
5959 15
76650691 10728
Satellite: ISS
Catalog Number: 25544
Epoch time: 06279
50505554 = yrday
fracday
Element set: 904
Inclination: 51
6366 deg
RA of node: 334
0037 deg
Eccentricity:
0012406
Arg of perigee: 64
6488 deg
Mean anomaly: 295
5959 deg
Mean motion: 15
76650691 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1072
Checksum: 306
Coasting Arc #6 (Orbit 1087)
---------------------------------------
Vector Time (GMT): 2006/280/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6085636
73 A = 6723988
25 meter
Y = -2529717
35 meter E =
0026638
Z = 1272696
81 I = 51
48781
XDOT = 819
359338 Wp = 63
16130
YDOT = 4956
533090 meter/sec RA = 328
58805 deg
ZDOT = 5852
288950 TA = 310
86211
MA = 311
09267
Ha = 190
573 n
mi
Hp = 175
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19965999
76 X = 6107289
41
Y = -8299597
59 feet Y = -2461543
21 meter
Z = 4175514
48 Z = 1302314
26
XDOT = 2688
186803 XDOT = 735
443835
YDOT = 16261
591504 feet/sec YDOT = 4965
226902 meter/sec
ZDOT = 19200
423063 ZDOT = 5856
065243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19909646
69 X = -6068460
31
Y = 8378528
58 feet Y = 2553775
51 meter
Z = 4285512
29 Z = 1306224
15
XDOT = -2035
591478 XDOT = -620
448283
YDOT = -14799
181847 feet/sec YDOT = -4510
790627 meter/sec
ZDOT = 19215
153565 ZDOT = 5856
778807
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 06280
51919321
00020000 00000-0 20000-3 0 9051
2 25544 51
6357 328
7751 0012717 68
2350 292
0166 15
76625678 10880
Satellite: ISS
Catalog Number: 25544
Epoch time: 06280
51919321 = yrday
fracday
Element set: 905
Inclination: 51
6357 deg
RA of node: 328
7751 deg
Eccentricity:
0012717
Arg of perigee: 68
2350 deg
Mean anomaly: 292
0166 deg
Mean motion: 15
76625678 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1088
Checksum: 303
Coasting Arc #7 (Orbit 1102)
---------------------------------------
Vector Time (GMT): 2006/281/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -92140
21 A = 6714518
93 meter
Y = -4707081
27 meter E =
0023360
Z = -4807310
40 I = 51
43196
XDOT = 6800
733205 Wp = 88
68534
YDOT = -2621
755054 meter/sec RA = 323
38688 deg
ZDOT = 2447
505060 TA = 205
28276
MA = 205
39727
Ha = 190
541 n
mi
Hp = 175
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -302297
26 X = -16144
49
Y = -15443180
02 feet Y = -4707686
97 meter
Z = -15772015
74 Z = -4807573
18
XDOT = 22312
116815 XDOT = 6817
654747
YDOT = -8601
558577 feet/sec YDOT = -2545
610746 meter/sec
ZDOT = 8029
872243 ZDOT = 2480
585090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 541985
53 X = 165197
19
Y = 15434986
66 feet Y = 4704583
93 meter
Z = -15773620
76 Z = -4807799
61
XDOT = -20954
946158 XDOT = -6387
067589
YDOT = 9031
367015 feet/sec YDOT = 2752
760666 meter/sec
ZDOT = 8152
757028 ZDOT = 2484
960342
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 06281
46992373
00020000 00000-0 20000-3 0 9065
2 25544 51
6350 323
8726 0012734 71
6151 288
6397 15
76679082 11030
Satellite: ISS
Catalog Number: 25544
Epoch time: 06281
46992373 = yrday
fracday
Element set: 906
Inclination: 51
6350 deg
RA of node: 323
8726 deg
Eccentricity:
0012734
Arg of perigee: 71
6151 deg
Mean anomaly: 288
6397 deg
Mean motion: 15
76679082 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1103
Checksum: 307
Coasting Arc #8 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2006/282/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5721156
33 A = 6720537
65 meter
Y = 1940934
88 meter E =
0016778
Z = -2960499
34 I = 51
43112
XDOT = 582
836004 Wp = 84
02231
YDOT = -5837
894501 meter/sec RA = 318
25886 deg
ZDOT = -4976
134096 TA = 130
22813
MA = 130
08121
Ha = 190
524 n
mi
Hp = 174
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18770197
93 X = -5728052
98
Y = 6367896
58 feet Y = 1876919
12 meter
Z = -9712924
34 Z = -2988310
22
XDOT = 1912
191614 XDOT = 672
246611
YDOT = -19153
197183 feet/sec YDOT = -5830
877084 meter/sec
ZDOT = -16325
899266 ZDOT = -4973
085309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18458312
75 X = 5626093
73
Y = -7081158
61 feet Y = -2158337
14 meter
Z = -9816273
21 Z = -2992000
07
XDOT = -1782
549442 XDOT = -543
321070
YDOT = 17869
715066 feet/sec YDOT = 5446
689152 meter/sec
ZDOT = -16315
313235 ZDOT = -4972
907474
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 06282
48401562
00020000 00000-0 20000-3 0 9074
2 25544 51
6352 318
6424 0012851 75
6390 284
6200 15
76722122 11198
Satellite: ISS
Catalog Number: 25544
Epoch time: 06282
48401562 = yrday
fracday
Element set: 907
Inclination: 51
6352 deg
RA of node: 318
6424 deg
Eccentricity:
0012851
Arg of perigee: 75
6390 deg
Mean anomaly: 284
6200 deg
Mean motion: 15
76722122 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1119
Checksum: 274
Coasting Arc #9 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2006/283/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1017714
98 A = 6718154
91 meter
Y = 5471339
25 meter E =
0024415
Z = 3745949
07 I = 51
40290
XDOT = -6224
482048 Wp = 80
52198
YDOT = 1742
963084 meter/sec RA = 313
03548 deg
ZDOT = -4209
662756 TA = 53
87862
MA = 53
65287
Ha = 190
446 n
mi
Hp = 174
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3338959
90 X = -1097018
18
Y = 17950588
09 feet Y = 5459515
16 meter
Z = 12289859
15 Z = 3740812
30
XDOT = -20421
529029 XDOT = -6223
059231
YDOT = 5718
382821 feet/sec YDOT = 1673
365461 meter/sec
ZDOT = -13811
229515 ZDOT = -4239
898518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2404559
70 X = 732909
80
Y = -18111949
34 feet Y = -5520522
16 meter
Z = 12271441
96 Z = 3740335
51
XDOT = 18675
276201 XDOT = 5692
224186
YDOT = -7014
943523 feet/sec YDOT = -2138
154786 meter/sec
ZDOT = -13923
643453 ZDOT = -4243
926525
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 06283
49808294
00020000 00000-0 20000-3 0 9080
2 25544 51
6350 313
4127 0012769 78
7734 281
4865 15
76784054 11355
Satellite: ISS
Catalog Number: 25544
Epoch time: 06283
49808294 = yrday
fracday
Element set: 908
Inclination: 51
6350 deg
RA of node: 313
4127 deg
Eccentricity:
0012769
Arg of perigee: 78
7734 deg
Mean anomaly: 281
4865 deg
Mean motion: 15
76784054 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1135
Checksum: 317
Coasting Arc #10 (Orbit 1150)
---------------------------------------
Vector Time (GMT): 2006/284/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5085267
46 A = 6716213
52 meter
Y = -998613
01 meter E =
0022225
Z = 4253814
86 I = 51
37785
XDOT = -1641
204258 Wp = 93
50565
YDOT = 6673
074575 meter/sec RA = 307
91173 deg
ZDOT = 3511
487347 TA = 320
79372
MA = 320
95451
Ha = 190
403 n
mi
Hp = 174
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16683948
35 X = 5075391
49
Y = -3276289
39 feet Y = -941802
04 meter
Z = 13956085
49 Z = 4278495
54
XDOT = -5384
528406 XDOT = -1732
760014
YDOT = 21893
289288 feet/sec YDOT = 6654
209731 meter/sec
ZDOT = 11520
627778 ZDOT = 3503
291976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16324523
76 X = -4975714
84
Y = 4475125
55 feet Y = 1364018
27 meter
Z = 14047907
39 Z = 4281802
17
XDOT = 4168
233485 XDOT = 1270
477566
YDOT = -21040
915329 feet/sec YDOT = -6413
270992 meter/sec
ZDOT = 11490
970207 ZDOT = 3502
447719
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
51212951
00020000 00000-0 20000-3 0 9094
2 25544 51
6346 308
1828 0012980 83
0659 277
1982 15
76794104 11516
Satellite: ISS
Catalog Number: 25544
Epoch time: 06284
51212951 = yrday
fracday
Element set: 909
Inclination: 51
6346 deg
RA of node: 308
1828 deg
Eccentricity:
0012980
Arg of perigee: 83
0659 deg
Mean anomaly: 277
1982 deg
Mean motion: 15
76794104 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1151
Checksum: 302
Coasting Arc #11 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2006/285/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1764606
04 A = 6721869
59 meter
Y = -6083693
89 meter E =
0017853
Z = -2254298
98 I = 51
38185
XDOT = 5433
265611 Wp = 73
06344
YDOT = -423
938120 meter/sec RA = 302
69086 deg
ZDOT = 5437
660049 TA = 261
52488
MA = 261
72727
Ha = 190
440 n
mi
Hp = 174
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5789389
91 X = 1843454
73
Y = -19959625
64 feet Y = -6063520
17 meter
Z = -7395994
02 Z = -2245535
02
XDOT = 17825
674578 XDOT = 5411
186792
YDOT = -1390
873096 feet/sec YDOT = -363
303912 meter/sec
ZDOT = 17840
092025 ZDOT = 5464
001584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4013209
45 X = -1223226
24
Y = 20402647
29 feet Y = 6218726
89 meter
Z = -7364139
62 Z = -2244589
76
XDOT = -16042
479855 XDOT = -4889
747860
YDOT = 3270
817125 feet/sec YDOT = 996
945060 meter/sec
ZDOT = 17938
183405 ZDOT = 5467
558302
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
46277661
00020000 00000-0 20000-3 0 9100
2 25544 51
6355 303
2800 0013001 86
6614 273
6038 15
76850272 11665
Satellite: ISS
Catalog Number: 25544
Epoch time: 06285
46277661 = yrday
fracday
Element set: 910
Inclination: 51
6355 deg
RA of node: 303
2800 deg
Eccentricity:
0013001
Arg of perigee: 86
6614 deg
Mean anomaly: 273
6038 deg
Mean motion: 15
76850272 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1166
Checksum: 277
Coasting Arc #12 (Orbit 1181)
---------------------------------------
Vector Time (GMT): 2006/286/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4393521
27 A = 6712767
60 meter
Y = -373879
45 meter E =
0026676
Z = -5084920
97 I = 51
33716
XDOT = 2361
446913 Wp = 84
00276
YDOT = -7154
377920 meter/sec RA = 297
54593 deg
ZDOT = -1518
404576 TA = 171
36396
MA = 171
31797
Ha = 190
419 n
mi
Hp = 174
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14414439
86 X = -4364312
09
Y = -1226638
60 feet Y = -422846
83 meter
Z = -16682811
58 Z = -5106193
96
XDOT = 7747
529241 XDOT = 2448
648858
YDOT = -23472
368503 feet/sec YDOT = -7127
483316 meter/sec
ZDOT = -4981
642310 ZDOT = -1506
720857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14371161
74 X = 4380330
10
Y = -312565
67 feet Y = -95270
02 meter
Z = -16762127
97 Z = -5109096
60
XDOT = -5242
335595 XDOT = -1597
863889
YDOT = 23121
341116 feet/sec YDOT = 7047
384772 meter/sec
ZDOT = -4939
051252 ZDOT = -1505
422821
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
47677704
00020000 00000-0 20000-3 0 9115
2 25544 51
6358 298
0496 0012933 90
3322 269
9325 15
76844243 11827
Satellite: ISS
Catalog Number: 25544
Epoch time: 06286
47677704 = yrday
fracday
Element set: 911
Inclination: 51
6358 deg
RA of node: 298
0496 deg
Eccentricity:
0012933
Arg of perigee: 90
3322 deg
Mean anomaly: 269
9325 deg
Mean motion: 15
76844243 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1182
Checksum: 314
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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