Date:
October 14th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4305 56 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 1181)
---------------------------------------
Vector Time (GMT): 2006/286/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4389077
46 A = 6712764
77 meter
Y = -387754
61 meter E =
0026588
Z = -5087637
69 I = 51
33651
XDOT = 2373
001201 Wp = 84
11382
YDOT = -7153
238572 meter/sec RA = 297
55300 deg
ZDOT = -1506
055561 TA = 171
37462
MA = 171
32884
Ha = 190
386 n
mi
Hp = 174
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14399860
44 X = -4359700
26
Y = -1272160
81 feet Y = -436671
37 meter
Z = -16691724
70 Z = -5108888
69
XDOT = 7785
437012 XDOT = 2460
129557
YDOT = -23468
630487 feet/sec YDOT = -7126
215174 meter/sec
ZDOT = -4941
127169 ZDOT = -1494
315890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14361486
62 X = 4377381
12
Y = -265739
98 feet Y = -80997
55 meter
Z = -16770960
96 Z = -5111788
90
XDOT = -5276
788183 XDOT = -1608
365038
YDOT = 23122
361378 feet/sec YDOT = 7047
695748 meter/sec
ZDOT = -4898
327464 ZDOT = -1493
010211
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
47675535
00020000 00000-0 20000-3 0 9003
2 25544 51
6353 298
0571 0012827 90
5254 269
7380 15
76840937 11829
Satellite: ISS
Catalog Number: 25544
Epoch time: 06286
47675535 = yrday
fracday
Element set: 900
Inclination: 51
6353 deg
RA of node: 298
0571 deg
Eccentricity:
0012827
Arg of perigee: 90
5254 deg
Mean anomaly: 269
7380 deg
Mean motion: 15
76840937 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1182
Checksum: 314
Coasting Arc #2 (Orbit 1197)
---------------------------------------
Vector Time (GMT): 2006/287/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2297902
81 A = 6723954
71 meter
Y = 6302142
55 meter E =
0024467
Z = 340442
29 I = 51
36150
XDOT = -4637
613700 Wp = 112
55065
YDOT = -1348
476265 meter/sec RA = 292
35814 deg
ZDOT = -6006
991442 TA = 63
72876
MA = 63
47755
Ha = 190
362 n
mi
Hp = 174
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7539051
22 X = -2369857
28
Y = 20676320
69 feet Y = 6276043
80 meter
Z = 1116936
64 Z = 329104
24
XDOT = -15215
268045 XDOT = -4593
009089
YDOT = -4424
134729 feet/sec YDOT = -1400
087215 meter/sec
ZDOT = -19707
977173 ZDOT = -6029
412787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4921851
21 X = 1500180
25
Y = -21452592
05 feet Y = -6538750
06 meter
Z = 1075524
61 Z = 327819
90
XDOT = 13974
022596 XDOT = 4259
282087
YDOT = 2156
862767 feet/sec YDOT = 657
411771 meter/sec
ZDOT = -19791
706959 ZDOT = -6032
512281
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
49073852
00020000 00000-0 20000-3 0 9011
2 25544 51
6341 292
8266 0012963 94
0881 266
1765 15
76879414 11982
Satellite: ISS
Catalog Number: 25544
Epoch time: 06287
49073852 = yrday
fracday
Element set: 901
Inclination: 51
6341 deg
RA of node: 292
8266 deg
Eccentricity:
0012963
Arg of perigee: 94
0881 deg
Mean anomaly: 266
1765 deg
Mean motion: 15
76879414 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1198
Checksum: 325
Coasting Arc #3 (Orbit 1213)
---------------------------------------
Vector Time (GMT): 2006/288/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3742915
33 A = 6711964
34 meter
Y = 1978579
92 meter E =
0015533
Z = 5194918
37 I = 51
31100
XDOT = -2802
792663 Wp = 90
79175
YDOT = 7156
678080 meter/sec RA = 287
17583 deg
ZDOT = -704
755800 TA = 5
93545
MA = 5
91706
Ha = 190
200 n
mi
Hp = 174
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12279905
95 X = 3695276
27
Y = 6491403
95 feet Y = 2020168
99 meter
Z = 17043695
42 Z = 5212985
81
XDOT = -9195
513985 XDOT = -2879
187723
YDOT = 23479
914962 feet/sec YDOT = 7124
908544 meter/sec
ZDOT = -2312
190945 ZDOT = -718
557510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12979653
50 X = -3956198
39
Y = -4706838
14 feet Y = -1434644
26 meter
Z = 17111289
81 Z = 5215521
13
XDOT = 5434
405005 XDOT = 1656
406646
YDOT = -23594
227658 feet/sec YDOT = -7191
520590 meter/sec
ZDOT = -2362
664031 ZDOT = -720
139997
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
50470606
00020000 00000-0 20000-3 0 9023
2 25544 51
6333 287
5964 0012935 97
6398 262
6236 15
76914366 12149
Satellite: ISS
Catalog Number: 25544
Epoch time: 06288
50470606 = yrday
fracday
Element set: 902
Inclination: 51
6333 deg
RA of node: 287
5964 deg
Eccentricity:
0012935
Arg of perigee: 97
6398 deg
Mean anomaly: 262
6236 deg
Mean motion: 15
76914366 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1214
Checksum: 314
Coasting Arc #4 (Orbit 1229)
---------------------------------------
Vector Time (GMT): 2006/289/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550921
61 A = 6722766
08 meter
Y = -6014363
04 meter E =
0025471
Z = 1553524
21 I = 51
34048
XDOT = 4016
433622 Wp = 80
94526
YDOT = 3207
171387 meter/sec RA = 282
01711 deg
ZDOT = 5745
260728 TA = 296
28824
MA = 296
54971
Ha = 190
218 n
mi
Hp = 174
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8369165
38 X = 2610438
67
Y = -19732162
20 feet Y = -5985504
39 meter
Z = 5096864
20 Z = 1566061
43
XDOT = 13177
275664 XDOT = 3952
362452
YDOT = 10522
215837 feet/sec YDOT = 3251
727317 meter/sec
ZDOT = 18849
280604 ZDOT = 5764
616959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5116084
14 X = -1559382
45
Y = 20802806
38 feet Y = 6340695
38 meter
Z = 5142772
48 Z = 1567517
05
XDOT = -13055
271376 XDOT = -3979
246715
YDOT = -7949
584844 feet/sec YDOT = -2423
033460 meter/sec
ZDOT = 18921
848273 ZDOT = 5767
379354
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
51865836
00020000 00000-0 20000-3 0 9039
2 25544 51
6332 282
3667 0012862 101
4547 258
8063 15
76939911 12306
Satellite: ISS
Catalog Number: 25544
Epoch time: 06289
51865836 = yrday
fracday
Element set: 903
Inclination: 51
6332 deg
RA of node: 282
3667 deg
Eccentricity:
0012862
Arg of perigee: 101
4547 deg
Mean anomaly: 258
8063 deg
Mean motion: 15
76939911 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1230
Checksum: 307
Coasting Arc #5 (Orbit 1244)
---------------------------------------
Vector Time (GMT): 2006/290/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3302125
56 A = 6714495
45 meter
Y = -3603430
32 meter E =
0023548
Z = -4626452
91 I = 51
30750
XDOT = 3063
033539 Wp = 106
86032
YDOT = -6451
442897 meter/sec RA = 276
79886 deg
ZDOT = 2843
853086 TA = 191
40643
MA = 191
45989
Ha = 190
206 n
mi
Hp = 174
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10833745
26 X = -3239111
40
Y = -11822277
95 feet Y = -3640004
41 meter
Z = -15178651
29 Z = -4642341
55
XDOT = 10049
322633 XDOT = 3121
131764
YDOT = -21166
151237 feet/sec YDOT = -6416
865380 meter/sec
ZDOT = 9330
226661 ZDOT = 2858
874865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12653501
06 X = 3856787
12
Y = 9757519
74 feet Y = 2974092
02 meter
Z = -15238355
11 Z = -4644650
64
XDOT = -5426
073230 XDOT = -1653
867120
YDOT = 21666
967020 feet/sec YDOT = 6604
091548 meter/sec
ZDOT = 9385
328625 ZDOT = 2860
648165
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
46922485
00020000 00000-0 20000-3 0 9040
2 25544 51
6329 277
4626 0012786 104
6711 255
5872 15
76924641 12457
Satellite: ISS
Catalog Number: 25544
Epoch time: 06290
46922485 = yrday
fracday
Element set: 904
Inclination: 51
6329 deg
RA of node: 277
4626 deg
Eccentricity:
0012786
Arg of perigee: 104
6711 deg
Mean anomaly: 255
5872 deg
Mean motion: 15
76924641 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1245
Checksum: 309
Coasting Arc #6 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2006/291/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2821622
76 A = 6718862
10 meter
Y = 5109789
26 meter E =
0017509
Z = -3337626
59 I = 51
31937
XDOT = -3573
947389 Wp = 103
86881
YDOT = -4990
379095 meter/sec RA = 271
66359 deg
ZDOT = -4643
186555 TA = 115
61512
MA = 115
43409
Ha = 190
129 n
mi
Hp = 174
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9257292
53 X = -2862337
63
Y = 16764400
46 feet Y = 5078008
47 meter
Z = -10950218
46 Z = -3351433
40
XDOT = -11725
549176 XDOT = -3495
322595
YDOT = -16372
634826 feet/sec YDOT = -5029
905610 meter/sec
ZDOT = -15233
551690 ZDOT = -4660
357749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5807118
78 X = 1770009
81
Y = -18218284
10 feet Y = -5552932
99 meter
Z = -11000971
24 Z = -3353096
03
XDOT = 13239
467896 XDOT = 4035
389815
YDOT = 13409
517230 feet/sec YDOT = 4087
220852 meter/sec
ZDOT = -15298
229488 ZDOT = -4662
900348
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
48314709
00020000 00000-0 20000-3 0 9058
2 25544 51
6317 272
2306 0012851 108
6597 251
5964 15
76959617 12618
Satellite: ISS
Catalog Number: 25544
Epoch time: 06291
48314709 = yrday
fracday
Element set: 905
Inclination: 51
6317 deg
RA of node: 272
2306 deg
Eccentricity:
0012851
Arg of perigee: 108
6597 deg
Mean anomaly: 251
5964 deg
Mean motion: 15
76959617 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1261
Checksum: 308
Coasting Arc #7 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2006/292/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984349
10 A = 6718700
07 meter
Y = 4995923
91 meter E =
0024867
Z = 3331897
88 I = 51
31960
XDOT = -3401
520569 Wp = 101
17200
YDOT = 5143
080208 meter/sec RA = 266
43012 deg
ZDOT = -4640
528146 TA = 39
29749
MA = 39
11728
Ha = 189
919 n
mi
Hp = 174
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9791171
59 X = 2912076
14
Y = 16390826
47 feet Y = 5028892
66 meter
Z = 10931423
49 Z = 3346220
25
XDOT = -11159
844386 XDOT = -3436
235147
YDOT = 16873
622730 feet/sec YDOT = 5104
848139 meter/sec
ZDOT = -15224
829875 ZDOT = -4657
137659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12939093
85 X = -3943835
81
Y = -13997183
28 feet Y = -4266341
46 meter
Z = 10985488
76 Z = 3348376
97
XDOT = 6286
866255 XDOT = 1916
236834
YDOT = -17871
192657 feet/sec YDOT = -5447
139522 meter/sec
ZDOT = -15286
019807 ZDOT = -4659
178837
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
49705218
00020000 00000-0 20000-3 0 9060
2 25544 51
6314 266
9994 0012679 111
9369 248
3144 15
77018988 12779
Satellite: ISS
Catalog Number: 25544
Epoch time: 06292
49705218 = yrday
fracday
Element set: 906
Inclination: 51
6314 deg
RA of node: 266
9994 deg
Eccentricity:
0012679
Arg of perigee: 111
9369 deg
Mean anomaly: 248
3144 deg
Mean motion: 15
77018988 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1277
Checksum: 331
Coasting Arc #8 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2006/293/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3145193
21 A = 6714274
28 meter
Y = -3744350
59 meter E =
0020872
Z = 4589136
99 I = 51
30761
XDOT = 3309
962520 Wp = 115
96915
YDOT = 6341
947340 meter/sec RA = 261
29621 deg
ZDOT = 2886
809929 TA = 305
28385
MA = 305
47892
Ha = 189
841 n
mi
Hp = 174
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10318875
35 X = 3164535
59
Y = -12284614
79 feet Y = -3709070
88 meter
Z = 15056223
73 Z = 4604463
88
XDOT = 10859
457086 XDOT = 3224
776060
YDOT = 20806
913844 feet/sec YDOT = 6378
485039 meter/sec
ZDOT = 9471
161186 ZDOT = 2902
682807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7199879
28 X = -2194523
20
Y = 14277431
89 feet Y = 4351761
24 meter
Z = 15112825
65 Z = 4606389
26
XDOT = -14181
792513 XDOT = -4322
610358
YDOT = -17306
898810 feet/sec YDOT = -5275
142757 meter/sec
ZDOT = 9531
193088 ZDOT = 2905
107653
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
51094217
00020000 00000-0 20000-3 0 9075
2 25544 51
6311 261
7687 0012619 116
1340 244
1124 15
77033488 12930
Satellite: ISS
Catalog Number: 25544
Epoch time: 06293
51094217 = yrday
fracday
Element set: 907
Inclination: 51
6311 deg
RA of node: 261
7687 deg
Eccentricity:
0012619
Arg of perigee: 116
1340 deg
Mean anomaly: 244
1124 deg
Mean motion: 15
77033488 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1293
Checksum: 277
Coasting Arc #9 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2006/294/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2772564
71 A = 6722364
68 meter
Y = -5919311
50 meter E =
0016052
Z = -1583585
63 I = 51
34092
XDOT = 3895
971501 Wp = 89
74193
YDOT = -3345
225579 meter/sec RA = 256
07718 deg
ZDOT = 5733
175559 TA = 252
70853
MA = 252
88423
Ha = 189
901 n
mi
Hp = 174
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9096340
92 X = -2698475
11
Y = -19420313
33 feet Y = -5949901
68 meter
Z = -5195490
91 Z = -1596874
87
XDOT = 12782
058729 XDOT = 3905
237236
YDOT = -10975
149538 feet/sec YDOT = -3301
606591 meter/sec
ZDOT = 18809
631099 ZDOT = 5752
125359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13503737
21 X = 4115939
10
Y = 16643779
40 feet Y = 5073023
96 meter
Z = -5245836
67 Z = -1598931
02
XDOT = -8426
493406 XDOT = -2568
395190
YDOT = 12735
993282 feet/sec YDOT = 3881
930752 meter/sec
ZDOT = 18879
790714 ZDOT = 5754
560210
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
46144940
00020000 00000-0 20000-3 0 9080
2 25544 51
6312 256
8645 0012826 119
4199 240
8248 15
77056635 13084
Satellite: ISS
Catalog Number: 25544
Epoch time: 06294
46144940 = yrday
fracday
Element set: 908
Inclination: 51
6312 deg
RA of node: 256
8645 deg
Eccentricity:
0012826
Arg of perigee: 119
4199 deg
Mean anomaly: 240
8248 deg
Mean motion: 15
77056635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1308
Checksum: 306
Coasting Arc #10 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2006/295/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3724243
30 A = 6711549
74 meter
Y = 2028296
80 meter E =
0026003
Z = -5223330
76 I = 51
31301
XDOT = -2975
370067 Wp = 102
61960
YDOT = -7060
487444 meter/sec RA = 250
91509 deg
ZDOT = -628
474583 TA = 161
41617
MA = 161
32103
Ha = 189
791 n
mi
Hp = 174
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12218646
01 X = -3721272
44
Y = 6654517
05 feet Y = 1986666
69 meter
Z = -17136911
93 Z = -5241416
52
XDOT = -9761
712817 XDOT = -2893
144470
YDOT = -23164
328886 feet/sec YDOT = -7093
299956 meter/sec
ZDOT = -2061
924486 ZDOT = -642
729420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9986543
95 X = 3043898
60
Y = -9567745
06 feet Y = -2916248
69 meter
Z = -17204035
93 Z = -5243790
15
XDOT = 14719
434463 XDOT = 4486
483624
YDOT = 19120
280399 feet/sec YDOT = 5827
861466 meter/sec
ZDOT = -2116
026693 ZDOT = -644
964936
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
47530754
00020000 00000-0 20000-3 0 9095
2 25544 51
6317 251
6321 0012646 123
2157 237
0222 15
77056818 13241
Satellite: ISS
Catalog Number: 25544
Epoch time: 06295
47530754 = yrday
fracday
Element set: 909
Inclination: 51
6317 deg
RA of node: 251
6321 deg
Eccentricity:
0012646
Arg of perigee: 123
2157 deg
Mean anomaly: 237
0222 deg
Mean motion: 15
77056818 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1324
Checksum: 278
Coasting Arc #11 (Orbit 1339)
---------------------------------------
Vector Time (GMT): 2006/296/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2377135
83 A = 6723267
61 meter
Y = 6258285
37 meter E =
0023609
Z = -506595
22 I = 51
36420
XDOT = -4669
432162 Wp = 132
57701
YDOT = 1303
829627 meter/sec RA = 245
73358 deg
ZDOT = -5996
035370 TA = 52
96640
MA = 52
75067
Ha = 189
645 n
mi
Hp = 174
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7799002
08 X = 2309439
17
Y = 20532432
30 feet Y = 6284489
30 meter
Z = -1662057
82 Z = -495211
23
XDOT = -15319
659323 XDOT = -4654
536136
YDOT = 4277
656256 feet/sec YDOT = 1251
696679 meter/sec
ZDOT = -19672
032054 ZDOT = -6018
684022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13164057
65 X = -4012404
77
Y = -17585642
65 feet Y = -5360103
88 meter
Z = -1618766
40 Z = -493400
00
XDOT = 12160
567293 XDOT = 3706
540911
YDOT = -7344
077174 feet/sec YDOT = -2238
474723 meter/sec
ZDOT = -19756
265865 ZDOT = -6021
709836
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 06296
48914873
00020000 00000-0 20000-3 0 9107
2 25544 51
6324 246
4007 0012542 126
8289 233
4028 15
77100624 13409
Satellite: ISS
Catalog Number: 25544
Epoch time: 06296
48914873 = yrday
fracday
Element set: 910
Inclination: 51
6324 deg
RA of node: 246
4007 deg
Eccentricity:
0012542
Arg of perigee: 126
8289 deg
Mean anomaly: 233
4028 deg
Mean motion: 15
77100624 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1340
Checksum: 278
Coasting Arc #12 (Orbit 1355)
---------------------------------------
Vector Time (GMT): 2006/297/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4441906
34 A = 6712189
41 meter
Y = -287340
70 meter E =
0014648
Z = 5010867
66 I = 51
34009
XDOT = 2422
362013 Wp = 110
61610
YDOT = 7117
753067 meter/sec RA = 240
53485 deg
ZDOT = -1740
167437 TA = 356
16223
MA = 356
17345
Ha = 189
433 n
mi
Hp = 175
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14573183
53 X = 4420446
63
Y = -942718
84 feet Y = -237788
90 meter
Z = 16439854
52 Z = 5032394
99
XDOT = 7947
381931 XDOT = 2351
043959
YDOT = 23352
208224 feet/sec YDOT = 7144
442527 meter/sec
ZDOT = -5709
210752 ZDOT = -1728
572367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13575313
26 X = -4137755
48
Y = 5131655
07 feet Y = 1564128
46 meter
Z = 16520054
47 Z = 5035312
60
XDOT = -14077
276170 XDOT = -4290
753777
YDOT = -19013
668777 feet/sec YDOT = -5795
366243 meter/sec
ZDOT = -5665
014593 ZDOT = -1726
696448
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 06297
50297351
00020000 00000-0 20000-3 0 9117
2 25544 51
6324 241
1702 0012484 130
8932 229
3316 15
77121575 13567
Satellite: ISS
Catalog Number: 25544
Epoch time: 06297
50297351 = yrday
fracday
Element set: 911
Inclination: 51
6324 deg
RA of node: 241
1702 deg
Eccentricity:
0012484
Arg of perigee: 130
8932 deg
Mean anomaly: 229
3316 deg
Mean motion: 15
77121575 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1356
Checksum: 276
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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