Date:
October 10th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7427 1 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 1118)
---------------------------------------
Vector Time (GMT): 2006/282/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2266242
75 A = 6712380
66 meter
Y = 3552524
16 meter E =
0015530
Z = 5212552
95 I = 51
40411
XDOT = -6054
311672 Wp = 73
04363
YDOT = 4747
790796 meter/sec RA = 318
34192 deg
ZDOT = -597
629674 TA = 22
67719
MA = 22
60865
Ha = 190
369 n
mi
Hp = 175
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7435179
62 X = 2201027
21
Y = 11655263
00 feet Y = 3577502
01 meter
Z = 17101551
66 Z = 5223404
15
XDOT = -19863
227271 XDOT = -6104
048902
YDOT = 15576
741458 feet/sec YDOT = 4679
810022 meter/sec
ZDOT = -1960
727276 ZDOT = -627
163183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6227913
17 X = -1898267
93
Y = -12285754
48 feet Y = -3744697
97 meter
Z = 17142446
01 Z = 5225017
54
XDOT = 20315
544088 XDOT = 6192
177838
YDOT = -13213
944822 feet/sec YDOT = -4027
610382 meter/sec
ZDOT = -2070
122333 ZDOT = -630
973287
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
48403028
00020000 00000-0 20000-3 0 9006
2 25544 51
6351 318
6473 0012657 75
6042 284
6526 15
76754467 11197
Satellite: ISS
Catalog Number: 25544
Epoch time: 06282
48403028 = yrday
fracday
Element set: 900
Inclination: 51
6351 deg
RA of node: 318
6473 deg
Eccentricity:
0012657
Arg of perigee: 75
6042 deg
Mean anomaly: 284
6526 deg
Mean motion: 15
76754467 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1119
Checksum: 295
Coasting Arc #2 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2006/283/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5244685
86 A = 6723534
29 meter
Y = -3946265
04 meter E =
0026754
Z = 1408018
38 I = 51
42059
XDOT = 1948
730501 Wp = 69
21835
YDOT = 4689
053496 meter/sec RA = 313
18785 deg
ZDOT = 5804
176840 TA = 306
34538
MA = 306
59202
Ha = 190
579 n
mi
Hp = 174
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17206974
59 X = 5281583
68
Y = -12947063
77 feet Y = -3887409
76 meter
Z = 4619482
88 Z = 1433587
25
XDOT = 6393
472772 XDOT = 1867
955727
YDOT = 15384
033778 feet/sec YDOT = 4710
393608 meter/sec
ZDOT = 19042
574933 ZDOT = 5813
447814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18111095
69 X = -5520261
97
Y = 11610787
92 feet Y = 3538968
16 meter
Z = 4714220
36 Z = 1436894
37
XDOT = -4260
286239 XDOT = -1298
535246
YDOT = -14494
621206 feet/sec YDOT = -4417
960543 meter/sec
ZDOT = 19077
730808 ZDOT = 5814
892350
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
49809593
00020000 00000-0 20000-3 0 9016
2 25544 51
6346 313
4176 0013007 78
8718 281
3909 15
76730261 11352
Satellite: ISS
Catalog Number: 25544
Epoch time: 06283
49809593 = yrday
fracday
Element set: 901
Inclination: 51
6346 deg
RA of node: 313
4176 deg
Eccentricity:
0013007
Arg of perigee: 78
8718 deg
Mean anomaly: 281
3909 deg
Mean motion: 15
76730261 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1135
Checksum: 300
Coasting Arc #3 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2006/284/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1164209
17 A = 6714513
00 meter
Y = -4646294
61 meter E =
0023671
Z = -4726515
84 I = 51
37243
XDOT = 5910
678518 Wp = 94
43478
YDOT = -4150
806377 meter/sec RA = 307
97858 deg
ZDOT = 2633
999408 TA = 201
52786
MA = 201
62756
Ha = 190
497 n
mi
Hp = 174
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3819583
91 X = -1089206
15
Y = -15243748
72 feet Y = -4658893
98 meter
Z = -15506941
74 Z = -4731989
59
XDOT = 19391
989890 XDOT = 5943
858380
YDOT = -13618
131157 feet/sec YDOT = -4084
524433 meter/sec
ZDOT = 8641
730342 ZDOT = 2662
794533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2836466
78 X = 864555
07
Y = 15435793
18 feet Y = 4704829
76 meter
Z = -15527945
25 Z = -4732917
71
XDOT = -18981
415592 XDOT = -5785
535472
YDOT = 12257
297345 feet/sec YDOT = 3736
024231 meter/sec
ZDOT = 8748
467485 ZDOT = 2666
532889
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
44875572
00020000 00000-0 20000-3 0 9023
2 25544 51
6348 308
5143 0012957 82
4321 277
8315 15
76790966 11503
Satellite: ISS
Catalog Number: 25544
Epoch time: 06284
44875572 = yrday
fracday
Element set: 902
Inclination: 51
6348 deg
RA of node: 308
5143 deg
Eccentricity:
0012957
Arg of perigee: 82
4321 deg
Mean anomaly: 277
8315 deg
Mean motion: 15
76790966 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1150
Checksum: 308
Coasting Arc #4 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2006/285/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5033451
64 A = 6719699
73 meter
Y = 3171040
56 meter E =
0017537
Z = -3139761
14 I = 51
37489
XDOT = -750
324420 Wp = 89
83029
YDOT = -5945
548747 meter/sec RA = 302
84760 deg
ZDOT = -4825
065173 TA = 126
85730
MA = 126
69638
Ha = 190
439 n
mi
Hp = 174
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16513948
97 X = -5053283
95
Y = 10403676
37 feet Y = 3114642
90 meter
Z = -10301053
60 Z = -3164262
09
XDOT = -2461
694291 XDOT = -660
345079
YDOT = -19506
393526 feet/sec YDOT = -5953
436076 meter/sec
ZDOT = -15830
266314 ZDOT = -4828
491879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16872257
00 X = 5142663
93
Y = -9715632
59 feet Y = -2961324
81 meter
Z = -10391925
95 Z = -3167459
03
XDOT = 858
638385 XDOT = 261
712980
YDOT = 18357
262066 feet/sec YDOT = 5595
293478 meter/sec
ZDOT = -15843
815406 ZDOT = -4829
194936
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
46276941
00020000 00000-0 20000-3 0 9032
2 25544 51
6354 303
2838 0013083 86
4400 273
8261 15
76851320 11661
Satellite: ISS
Catalog Number: 25544
Epoch time: 06285
46276941 = yrday
fracday
Element set: 903
Inclination: 51
6354 deg
RA of node: 303
2838 deg
Eccentricity:
0013083
Arg of perigee: 86
4400 deg
Mean anomaly: 273
8261 deg
Mean motion: 15
76851320 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1166
Checksum: 285
Coasting Arc #5 (Orbit 1181)
---------------------------------------
Vector Time (GMT): 2006/286/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 233992
82 A = 6718395
70 meter
Y = 5683217
09 meter E =
0025188
Z = 3554483
93 I = 51
35557
XDOT = -5562
352594 Wp = 88
07082
YDOT = 3010
022114 meter/sec RA = 297
61913 deg
ZDOT = -4418
798205 TA = 49
20182
MA = 48
98359
Ha = 190
355 n
mi
Hp = 174
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 767692
97 X = 153157
69
Y = 18645725
37 feet Y = 5685381
70 meter
Z = 11661692
69 Z = 3555424
43
XDOT = -18249
188301 XDOT = -5574
131734
YDOT = 9875
400635 feet/sec YDOT = 2947
755020 meter/sec
ZDOT = -14497
369438 ZDOT = -4445
848944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -254051
79 X = -77434
99
Y = -18657133
55 feet Y = -5686694
31 meter
Z = 11665947
41 Z = 3555780
77
XDOT = 17040
968406 XDOT = 5194
087170
YDOT = -9416
583075 feet/sec YDOT = -2870
174521 meter/sec
ZDOT = -14597
767857 ZDOT = -4449
399643
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
47675623
00020000 00000-0 20000-3 0 9045
2 25544 51
6345 298
0538 0013044 89
8684 270
3975 15
76906267 11820
Satellite: ISS
Catalog Number: 25544
Epoch time: 06286
47675623 = yrday
fracday
Element set: 904
Inclination: 51
6345 deg
RA of node: 298
0538 deg
Eccentricity:
0013044
Arg of perigee: 89
8684 deg
Mean anomaly: 270
3975 deg
Mean motion: 15
76906267 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1182
Checksum: 327
Coasting Arc #6 (Orbit 1197)
---------------------------------------
Vector Time (GMT): 2006/287/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4641960
14 A = 6715216
24 meter
Y = -1961969
30 meter E =
0021991
Z = 4421851
12 I = 51
33270
XDOT = -117
205905 Wp = 101
01888
YDOT = 7013
165955 meter/sec RA = 292
48994 deg
ZDOT = 3217
129064 TA = 316
62190
MA = 316
79477
Ha = 190
303 n
mi
Hp = 174
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15229528
03 X = 4642073
45
Y = -6436907
15 feet Y = -1910059
71 meter
Z = 14507385
57 Z = 4444402
19
XDOT = -384
533809 XDOT = -211
247730
YDOT = 23009
074654 feet/sec YDOT = 7011
329468 meter/sec
ZDOT = 10554
885380 ZDOT = 3216
331270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15193174
60 X = -4630879
62
Y = 6332619
45 feet Y = 1930182
41 meter
Z = 14591158
63 Z = 4447385
15
XDOT = 1062
955294 XDOT = 323
988773
YDOT = -21897
466158 feet/sec YDOT = -6674
347685 meter/sec
ZDOT = 10552
844752 ZDOT = 3216
507080
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
49071838
00020000 00000-0 20000-3 0 9057
2 25544 51
6341 292
8235 0013212 93
9200 266
3475 15
76921918 11986
Satellite: ISS
Catalog Number: 25544
Epoch time: 06287
49071838 = yrday
fracday
Element set: 905
Inclination: 51
6341 deg
RA of node: 292
8235 deg
Eccentricity:
0013212
Arg of perigee: 93
9200 deg
Mean anomaly: 266
3475 deg
Mean motion: 15
76921918 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1198
Checksum: 305
Coasting Arc #7 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2006/288/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 382651
64 A = 6722024
73 meter
Y = -6429794
78 meter E =
0017853
Z = -1929699
86 I = 51
34773
XDOT = 5109
256005 Wp = 78
10355
YDOT = -1360
973691 meter/sec RA = 287
26907 deg
ZDOT = 5595
158037 TA = 260
33599
MA = 260
53771
Ha = 190
267 n
mi
Hp = 174
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1255418
75 X = 463896
24
Y = -21095127
24 feet Y = -6425061
53 meter
Z = -6331036
30 Z = -1927643
50
XDOT = 16762
650936 XDOT = 5096
914443
YDOT = -4465
136783 feet/sec YDOT = -1303
908089 meter/sec
ZDOT = 18356
817707 ZDOT = 5619
948988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1072622
98 X = -326935
48
Y = 21107250
42 feet Y = 6433489
93 meter
Z = -6324235
13 Z = -1927626
87
XDOT = -15074
942122 XDOT = -4594
842359
YDOT = 4715
218827 feet/sec YDOT = 1437
198698 meter/sec
ZDOT = 18449
019670 ZDOT = 5623
261195
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
44128287
00020000 00000-0 20000-3 0 9065
2 25544 51
6350 287
9205 0013192 97
8037 262
4626 15
76998549 12133
Satellite: ISS
Catalog Number: 25544
Epoch time: 06288
44128287 = yrday
fracday
Element set: 906
Inclination: 51
6350 deg
RA of node: 287
9205 deg
Eccentricity:
0013192
Arg of perigee: 97
8037 deg
Mean anomaly: 262
4626 deg
Mean motion: 15
76998549 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1213
Checksum: 320
Coasting Arc #8 (Orbit 1228)
---------------------------------------
Vector Time (GMT): 2006/289/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4299338
16 A = 6711990
58 meter
Y = 303245
55 meter E =
0027123
Z = -5168610
80 I = 51
30600
XDOT = 747
774778 Wp = 90
98026
YDOT = -7573
875606 meter/sec RA = 282
11463 deg
ZDOT = -1071
680928 TA = 168
75889
MA = 168
69818
Ha = 190
218 n
mi
Hp = 174
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14105440
16 X = -4277301
21
Y = 994900
09 feet Y = 255291
02 meter
Z = -16957384
52 Z = -5189443
61
XDOT = 2453
329325 XDOT = 837
617396
YDOT = -24848
673247 feet/sec YDOT = -7565
011272 meter/sec
ZDOT = -3516
013542 ZDOT = -1067
829747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13978930
31 X = 4260777
96
Y = -1380261
13 feet Y = -420703
59 meter
Z = -17034980
04 Z = -5192261
92
XDOT = -1888
662199 XDOT = -575
664238
YDOT = 23887
907181 feet/sec YDOT = 7281
034109 meter/sec
ZDOT = -3502
685844 ZDOT = -1067
618645
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
45519208
00020000 00000-0 20000-3 0 9075
2 25544 51
6345 282
6893 0013047 101
4523 258
8108 15
76986391 12296
Satellite: ISS
Catalog Number: 25544
Epoch time: 06289
45519208 = yrday
fracday
Element set: 907
Inclination: 51
6345 deg
RA of node: 282
6893 deg
Eccentricity:
0013047
Arg of perigee: 101
4523 deg
Mean anomaly: 258
8108 deg
Mean motion: 15
76986391 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1229
Checksum: 313
Coasting Arc #9 (Orbit 1244)
---------------------------------------
Vector Time (GMT): 2006/290/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -888102
68 A = 6723545
90 meter
Y = 6655983
40 meter E =
0024358
Z = -99004
75 I = 51
33948
XDOT = -4764
259538 Wp = 119
57870
YDOT = -708
583487 meter/sec RA = 276
92420 deg
ZDOT = -6018
515627 TA = 61
50308
MA = 61
25799
Ha = 190
157 n
mi
Hp = 174
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2913722
69 X = -961983
85
Y = 21837215
88 feet Y = 6645639
05 meter
Z = -324818
74 Z = -103498
97
XDOT = -15630
772761 XDOT = -4726
744838
YDOT = -2324
748974 feet/sec YDOT = -761
650606 meter/sec
ZDOT = -19745
786177 ZDOT = -6041
569452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1932687
09 X = 589083
02
Y = -21945568
03 feet Y = -6689009
13 meter
Z = -340659
77 Z = -103833
10
XDOT = 14009
639592 XDOT = 4270
138148
YDOT = 1487
345943 feet/sec YDOT = 453
343043 meter/sec
ZDOT = -19831
797696 ZDOT = -6044
731938
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
46907422
00020000 00000-0 20000-3 0 9088
2 25544 51
6331 277
4577 0013176 105
0954 255
1670 15
77038078 12456
Satellite: ISS
Catalog Number: 25544
Epoch time: 06290
46907422 = yrday
fracday
Element set: 908
Inclination: 51
6331 deg
RA of node: 277
4577 deg
Eccentricity:
0013176
Arg of perigee: 105
0954 deg
Mean anomaly: 255
1670 deg
Mean motion: 15
77038078 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1245
Checksum: 296
Coasting Arc #10 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2006/291/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4051531
03 A = 6711812
27 meter
Y = 1534968
70 meter E =
0015890
Z = 5112248
58 I = 51
29770
XDOT = -1243
449982 Wp = 96
31340
YDOT = 7511
416863 meter/sec RA = 271
72986 deg
ZDOT = -1268
238347 TA = 5
85016
MA = 5
83162
Ha = 189
905 n
mi
Hp = 174
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13292424
65 X = 4009230
98
Y = 5035986
56 feet Y = 1580038
95 meter
Z = 16772469
08 Z = 5131828
33
XDOT = -4079
560310 XDOT = -1321
190319
YDOT = 24643
756113 feet/sec YDOT = 7497
077176 meter/sec
ZDOT = -4160
886966 ZDOT = -1274
468368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13485971
79 X = -4110524
20
Y = -4209290
24 feet Y = -1282991
67 meter
Z = 16845648
50 Z = 5134553
66
XDOT = 2216
725792 XDOT = 675
658021
YDOT = -23864
192619 feet/sec YDOT = -7273
805910 meter/sec
ZDOT = -4183
073341 ZDOT = -1275
000754
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
48292773
00020000 00000-0 20000-3 0 9098
2 25544 51
6324 272
2263 0013053 108
7363 251
5219 15
77096832 12610
Satellite: ISS
Catalog Number: 25544
Epoch time: 06291
48292773 = yrday
fracday
Element set: 909
Inclination: 51
6324 deg
RA of node: 272
2263 deg
Eccentricity:
0013053
Arg of perigee: 108
7363 deg
Mean anomaly: 251
5219 deg
Mean motion: 15
77096832 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1261
Checksum: 290
Coasting Arc #11 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2006/292/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1293770
61 A = 6721311
49 meter
Y = -6251849
35 meter E =
0025210
Z = 2080137
96 I = 51
33066
XDOT = 4592
377412 Wp = 90
33625
YDOT = 2805
838631 meter/sec RA = 266
57760 deg
ZDOT = 5518
978319 TA = 293
04073
MA = 293
30638
Ha = 189
865 n
mi
Hp = 174
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4244654
23 X = 1353478
39
Y = -20511316
75 feet Y = -6237047
72 meter
Z = 6824599
61 Z = 2086568
62
XDOT = 15066
855025 XDOT = 4533
850143
YDOT = 9205
507318 feet/sec YDOT = 2856
866234 meter/sec
ZDOT = 18106
884250 ZDOT = 5541
146146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2572445
56 X = -784081
41
Y = 20779746
33 feet Y = 6333666
68 meter
Z = 6847702
56 Z = 2087179
74
XDOT = -14132
181213 XDOT = -4307
488834
YDOT = -7805
891383 feet/sec YDOT = -2379
235693 meter/sec
ZDOT = 18189
885365 ZDOT = 5544
277059
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
49675291
00020000 00000-0 20000-3 0 9102
2 25544 51
6323 266
9955 0012993 113
0659 247
1877 15
77160195 12778
Satellite: ISS
Catalog Number: 25544
Epoch time: 06292
49675291 = yrday
fracday
Element set: 910
Inclination: 51
6323 deg
RA of node: 266
9955 deg
Eccentricity:
0012993
Arg of perigee: 113
0659 deg
Mean anomaly: 247
1877 deg
Mean motion: 15
77160195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1277
Checksum: 322
Coasting Arc #12 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2006/293/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3981890
77 A = 6715140
09 meter
Y = -3316657
78 meter E =
0021742
Z = -4293002
85 I = 51
31262
XDOT = 1794
649283 Wp = 113
83590
YDOT = -6626
656314 meter/sec RA = 261
35018 deg
ZDOT = 3460
151500 TA = 191
35072
MA = 191
39984
Ha = 189
849 n
mi
Hp = 174
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13063946
09 X = -3923652
39
Y = -10881423
17 feet Y = -3360860
11 meter
Z = -14084655
01 Z = -4312205
65
XDOT = 5887
956965 XDOT = 1851
806921
YDOT = -21740
998407 feet/sec YDOT = -6606
267770 meter/sec
ZDOT = 11352
203085 ZDOT = 3469
009318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13972349
66 X = 4258772
18
Y = 9581830
11 feet Y = 2920541
82 meter
Z = -14156678
32 Z = -4314955
55
XDOT = -3008
412567 XDOT = -916
964150
YDOT = 21181
717386 feet/sec YDOT = 6456
187459 meter/sec
ZDOT = 11384
297502 ZDOT = 3469
933878
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
44719003
00020000 00000-0 20000-3 0 9119
2 25544 51
6321 262
0902 0012959 115
9110 244
3392 15
77147500 12923
Satellite: ISS
Catalog Number: 25544
Epoch time: 06293
44719003 = yrday
fracday
Element set: 911
Inclination: 51
6321 deg
RA of node: 262
0902 deg
Eccentricity:
0012959
Arg of perigee: 115
9110 deg
Mean anomaly: 244
3392 deg
Mean motion: 15
77147500 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1292
Checksum: 264
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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