Date:
September 30th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 960)
---------------------------------------
Vector Time (GMT): 2006/272/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6594876
84 A = 6725442
88 meter
Y = -1309498
73 meter E =
0015731
Z = -189925
66 I = 51
71082
XDOT = 1084
763094 Wp = 87
26535
YDOT = -4649
296893 meter/sec RA = 9
95295 deg
ZDOT = -6038
178288 TA = 94
79629
MA = 94
61664
Ha = 190
378 n
mi
Hp = 176
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21636735
04 X = -6578821
06
Y = -4296255
67 feet Y = -1383156
52 meter
Z = -623115
68 Z = -221924
99
XDOT = 3558
934035 XDOT = 1166
004311
YDOT = -15253
598731 feet/sec YDOT = -4636
712184 meter/sec
ZDOT = -19810
296220 ZDOT = -6032
711138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19753404
86 X = 6020837
80
Y = 9810509
17 feet Y = 2990243
20 meter
Z = -742492
84 Z = -226311
82
XDOT = -6818
563071 XDOT = -2078
298024
YDOT = 12320
386024 feet/sec YDOT = 3755
253660 meter/sec
ZDOT = -19790
534540 ZDOT = -6032
154928
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 06272
46883213
00020000 00000-0 20000-3 0 9001
2 25544 51
6372 10
2699 0011969 39
6340 320
5697 15
76359565 9614
Satellite: ISS
Catalog Number: 25544
Epoch time: 06272
46883213 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 10
2699 deg
Eccentricity:
0011969
Arg of perigee: 39
6340 deg
Mean anomaly: 320
5697 deg
Mean motion: 15
76359565 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 961
Checksum: 307
Coasting Arc #2 (Orbit 976)
---------------------------------------
Vector Time (GMT): 2006/273/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1590215
22 A = 6713736
30 meter
Y = 3970133
15 meter E =
0015970
Z = 5167304
76 I = 51
64421
XDOT = -7477
780617 Wp = 45
66188
YDOT = -1517
717201 meter/sec RA = 4
79049 deg
ZDOT = -1122
063348 TA = 55
10532
MA = 54
95532
Ha = 190
496 n
mi
Hp = 176
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5217241
55 X = -1659593
66
Y = 13025371
22 feet Y = 3951962
51 meter
Z = 16953099
60 Z = 5159410
94
XDOT = -24533
400976 XDOT = -7454
802700
YDOT = -4979
387144 feet/sec YDOT = -1601
209397 meter/sec
ZDOT = -3681
310196 ZDOT = -1158
334922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8342200
93 X = 2542702
84
Y = -11325474
44 feet Y = -3452004
61 meter
Z = 16924207
61 Z = 5158498
48
XDOT = 21717
730384 XDOT = 6619
564221
YDOT = 10229
279814 feet/sec YDOT = 3117
884487 meter/sec
ZDOT = -3816
635348 ZDOT = -1163
310454
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 06273
48314018
00020000 00000-0 20000-3 0 9017
2 25544 51
6380 5
0425 0012093 43
1430 317
0680 15
76391976 9773
Satellite: ISS
Catalog Number: 25544
Epoch time: 06273
48314018 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 5
0425 deg
Eccentricity:
0012093
Arg of perigee: 43
1430 deg
Mean anomaly: 317
0680 deg
Mean motion: 15
76391976 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 977
Checksum: 272
Coasting Arc #3 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2006/274/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6339674
14 A = 6723938
03 meter
Y = 1340987
95 meter E =
0025960
Z = 1742004
17 I = 51
65096
XDOT = -2538
907132 Wp = 56
51307
YDOT = 4529
596678 meter/sec RA = 359
66371 deg
ZDOT = 5706
448565 TA = 322
81852
MA = 322
99802
Ha = 190
437 n
mi
Hp = 176
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20799455
83 X = 6315745
46
Y = 4399566
76 feet Y = 1411747
90 meter
Z = 5715236
79 Z = 1772744
33
XDOT = -8329
747809 XDOT = -2617
090034
YDOT = 14860
881488 feet/sec YDOT = 4500
768058 meter/sec
ZDOT = 18721
944110 ZDOT = 5693
924600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19213113
75 X = -5856157
07
Y = -9028043
78 feet Y = -2751747
74 meter
Z = 5829937
17 Z = 1776964
85
XDOT = 10946
823278 XDOT = 3336
591735
YDOT = -11139
838227 feet/sec YDOT = -3395
422691 meter/sec
ZDOT = 18675
874687 ZDOT = 5692
406605
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 06274
49742641
00020000 00000-0 20000-3 0 9027
2 25544 51
6384 359
8151 0012151 47
2069 313
0115 15
76419936 9935
Satellite: ISS
Catalog Number: 25544
Epoch time: 06274
49742641 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 359
8151 deg
Eccentricity:
0012151
Arg of perigee: 47
2069 deg
Mean anomaly: 313
0115 deg
Mean motion: 15
76419936 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 993
Checksum: 294
Coasting Arc #4 (Orbit 1007)
---------------------------------------
Vector Time (GMT): 2006/275/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2821370
71 A = 6715856
49 meter
Y = -3968475
41 meter E =
0019850
Z = -4639991
63 I = 51
59574
XDOT = 6954
576376 Wp = 77
62842
YDOT = 1609
705183 meter/sec RA = 354
47099 deg
ZDOT = 2866
475727 TA = 220
69007
MA = 220
83854
Ha = 190
463 n
mi
Hp = 176
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9256465
57 X = 2888077
33
Y = -13019932
45 feet Y = -3936552
38 meter
Z = -15223069
64 Z = -4626123
29
XDOT = 22816
851628 XDOT = 6922
134707
YDOT = 5281
184982 feet/sec YDOT = 1687
293765 meter/sec
ZDOT = 9404
447923 ZDOT = 2900
182285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11884849
30 X = -3622502
07
Y = 10747365
09 feet Y = 3275796
88 meter
Z = -15171919
65 Z = -4624401
11
XDOT = -20346
978107 XDOT = -6201
758927
YDOT = -9113
914640 feet/sec YDOT = -2777
921182 meter/sec
ZDOT = 9530
240063 ZDOT = 2904
817171
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
44830036
00020000 00000-0 20000-3 0 9030
2 25544 51
6385 354
9150 0012145 50
5358 309
6879 15
76468139 10087
Satellite: ISS
Catalog Number: 25544
Epoch time: 06275
44830036 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 354
9150 deg
Eccentricity:
0012145
Arg of perigee: 50
5358 deg
Mean anomaly: 309
6879 deg
Mean motion: 15
76468139 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1008
Checksum: 299
Coasting Arc #5 (Orbit 1023)
---------------------------------------
Vector Time (GMT): 2006/276/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5705314
00 A = 6720520
82 meter
Y = -1530457
19 meter E =
0015915
Z = -3224935
38 I = 51
58370
XDOT = 3919
681869 Wp = 65
06724
YDOT = -4585
451534 meter/sec RA = 349
36013 deg
ZDOT = -4770
046426 TA = 152
63694
MA = 152
55303
Ha = 190
478 n
mi
Hp = 175
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18718221
80 X = -5672110
02
Y = -5021185
01 feet Y = -1594071
66 meter
Z = -10580496
64 Z = -3252571
09
XDOT = 12859
848653 XDOT = 3993
837746
YDOT = -15044
132330 feet/sec YDOT = -4541
205063 meter/sec
ZDOT = -15649
758614 ZDOT = -4750
824273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17323531
98 X = 5280212
55
Y = 8560702
03 feet Y = 2609301
98 meter
Z = -10683663
03 Z = -3256380
49
XDOT = -15004
960564 XDOT = -4573
511980
YDOT = 10969
770107 feet/sec YDOT = 3343
585929 meter/sec
ZDOT = -15578
745907 ZDOT = -4748
401753
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
46254511
00020000 00000-0 20000-3 0 9042
2 25544 51
6385 349
6867 0012152 54
2802 305
9491 15
76477021 10243
Satellite: ISS
Catalog Number: 25544
Epoch time: 06276
46254511 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 349
6867 deg
Eccentricity:
0012152
Arg of perigee: 54
2802 deg
Mean anomaly: 305
9491 deg
Mean motion: 15
76477021 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1024
Checksum: 287
Coasting Arc #6 (Orbit 1039)
---------------------------------------
Vector Time (GMT): 2006/277/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3950411
30 A = 6719516
03 meter
Y = 4077704
24 meter E =
0023712
Z = 3581729
66 I = 51
55251
XDOT = -6020
899510 Wp = 71
70723
YDOT = -1931
066916 meter/sec RA = 344
14937 deg
ZDOT = -4411
076784 TA = 65
34899
MA = 65
10222
Ha = 190
596 n
mi
Hp = 175
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12960667
00 X = -4013114
60
Y = 13378294
76 feet Y = 4033178
22 meter
Z = 11751081
55 Z = 3562385
91
XDOT = -19753
607317 XDOT = -5977
430292
YDOT = -6335
521378 feet/sec YDOT = -1998
153222 meter/sec
ZDOT = -14472
036693 ZDOT = -4440
220665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15198090
41 X = 4632377
96
Y = -10846734
78 feet Y = -3306084
76 meter
Z = 11679553
50 Z = 3559927
91
XDOT = 17441
101002 XDOT = 5316
047585
YDOT = 8626
922313 feet/sec YDOT = 2629
485921 meter/sec
ZDOT = -14580
875966 ZDOT = -4444
250994
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
47676854
00020000 00000-0 20000-3 0 9053
2 25544 51
6384 344
4590 0012338 57
9053 302
3307 15
76510603 10401
Satellite: ISS
Catalog Number: 25544
Epoch time: 06277
47676854 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 344
4590 deg
Eccentricity:
0012338
Arg of perigee: 57
9053 deg
Mean anomaly: 302
3307 deg
Mean motion: 15
76510603 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1040
Checksum: 286
Coasting Arc #7 (Orbit 1055)
---------------------------------------
Vector Time (GMT): 2006/278/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4729974
94 A = 6716460
54 meter
Y = 1896820
88 meter E =
0019653
Z = 4356700
63 I = 51
51611
XDOT = -5029
023443 Wp = 82
02565
YDOT = 4790
565365 meter/sec RA = 339
03724 deg
ZDOT = 3364
001982 TA = 334
08613
MA = 334
18442
Ha = 190
353 n
mi
Hp = 175
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15518290
49 X = 4687248
66
Y = 6223165
60 feet Y = 1949475
59 meter
Z = 14293637
24 Z = 4379575
07
XDOT = -16499
420744 XDOT = -5098
560281
YDOT = 15717
077968 feet/sec YDOT = 4733
939549 meter/sec
ZDOT = 11036
751911 ZDOT = 3339
401451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14235876
75 X = -4339095
23
Y = -8627521
60 feet Y = -2629668
58 meter
Z = 14379112
62 Z = 4382753
53
XDOT = 18245
326415 XDOT = 5561
175491
YDOT = -11807
643980 feet/sec YDOT = -3598
969885 meter/sec
ZDOT = 10945
739278 ZDOT = 3336
261332
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
49096853
00020000 00000-0 20000-3 0 9062
2 25544 51
6384 339
2307 0012234 61
4419 298
7975 15
76571166 10567
Satellite: ISS
Catalog Number: 25544
Epoch time: 06278
49096853 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 339
2307 deg
Eccentricity:
0012234
Arg of perigee: 61
4419 deg
Mean anomaly: 298
7975 deg
Mean motion: 15
76571166 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1056
Checksum: 321
Coasting Arc #8 (Orbit 1070)
---------------------------------------
Vector Time (GMT): 2006/279/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4719681
61 A = 6722888
94 meter
Y = -4256198
55 meter E =
0018266
Z = -2186273
83 I = 51
51077
XDOT = 4786
061707 Wp = 56
19654
YDOT = 2510
162541 meter/sec RA = 333
83024 deg
ZDOT = 5487
985117 TA = 279
24680
MA = 279
45335
Ha = 190
565 n
mi
Hp = 175
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15484519
72 X = 4777544
91
Y = -13963906
00 feet Y = -4203097
13 meter
Z = -7172814
39 Z = -2163204
32
XDOT = 15702
302188 XDOT = 4730
976980
YDOT = 8235
441406 feet/sec YDOT = 2563
375473 meter/sec
ZDOT = 18005
200515 ZDOT = 5511
102093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17372845
63 X = -5295243
35
Y = 11582863
73 feet Y = 3530456
86 meter
Z = -7087438
94 Z = -2160251
39
XDOT = -13409
606306 XDOT = -4087
248002
YDOT = -9129
329217 feet/sec YDOT = -2782
619545 meter/sec
ZDOT = 18091
658825 ZDOT = 5514
337610
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
44176364
00020000 00000-0 20000-3 0 9075
2 25544 51
6378 334
3301 0012312 63
9857 296
2574 15
76548589 10718
Satellite: ISS
Catalog Number: 25544
Epoch time: 06279
44176364 = yrday
fracday
Element set: 907
Inclination: 51
6378 deg
RA of node: 334
3301 deg
Eccentricity:
0012312
Arg of perigee: 63
9857 deg
Mean anomaly: 296
2574 deg
Mean motion: 15
76548589 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1071
Checksum: 315
Coasting Arc #9 (Orbit 1086)
---------------------------------------
Vector Time (GMT): 2006/280/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3570255
81 A = 6713492
41 meter
Y = -2576569
45 meter E =
0026090
Z = -5091256
81 I = 51
45354
XDOT = 5718
163452 Wp = 73
34686
YDOT = -4902
226146 meter/sec RA = 328
69583 deg
ZDOT = -1528
079593 TA = 181
92040
MA = 181
93044
Ha = 190
509 n
mi
Hp = 175
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11713437
70 X = -3516445
98
Y = -8453311
83 feet Y = -2616193
58 meter
Z = -16703598
45 Z = -5108470
56
XDOT = 18760
378781 XDOT = 5779
979127
YDOT = -16083
419115 feet/sec YDOT = -4837
936969 meter/sec
ZDOT = -5013
384493 ZDOT = -1500
149620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10453893
81 X = 3186346
83
Y = 9860082
27 feet Y = 3005353
08 meter
Z = -16768070
45 Z = -5110907
87
XDOT = -19958
598971 XDOT = -6083
380966
YDOT = 12805
694658 feet/sec YDOT = 3903
175732 meter/sec
ZDOT = -4909
990215 ZDOT = -1496
565018
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
45592343
00020000 00000-0 20000-3 0 9088
2 25544 51
6368 329
1012 0012306 68
2353 292
0120 15
76587287 10876
Satellite: ISS
Catalog Number: 25544
Epoch time: 06280
45592343 = yrday
fracday
Element set: 908
Inclination: 51
6368 deg
RA of node: 329
1012 deg
Eccentricity:
0012306
Arg of perigee: 68
2353 deg
Mean anomaly: 292
0120 deg
Mean motion: 15
76587287 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1087
Checksum: 286
Coasting Arc #10 (Orbit 1102)
---------------------------------------
Vector Time (GMT): 2006/281/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5177148
47 A = 6724564
79 meter
Y = 4262535
79 meter E =
0022226
Z = 437192
50 I = 51
46772
XDOT = -3371
816389 Wp = 101
45427
YDOT = -3453
549526 meter/sec RA = 323
51008 deg
ZDOT = -6004
445208 TA = 73
77533
MA = 73
53089
Ha = 190
509 n
mi
Hp = 175
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16985395
23 X = -5226551
81
Y = 13984697
48 feet Y = 4204365
84 meter
Z = 1434358
58 Z = 411921
05
XDOT = -11062
389728 XDOT = -3303
778474
YDOT = -11330
543063 feet/sec YDOT = -3490
874944 meter/sec
ZDOT = -19699
623387 ZDOT = -6020
660452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18426731
28 X = 5616467
69
Y = -12032899
84 feet Y = -3667627
87 meter
Z = 1340781
50 Z = 408670
20
XDOT = 8764
839929 XDOT = 2671
523210
YDOT = 11121
536131 feet/sec YDOT = 3389
844213 meter/sec
ZDOT = -19760
489606 ZDOT = -6022
997232
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
47006119
00020000 00000-0 20000-3 0 9093
2 25544 51
6365 323
8720 0012539 71
7449 288
5079 15
76654042 11039
Satellite: ISS
Catalog Number: 25544
Epoch time: 06281
47006119 = yrday
fracday
Element set: 909
Inclination: 51
6365 deg
RA of node: 323
8720 deg
Eccentricity:
0012539
Arg of perigee: 71
7449 deg
Mean anomaly: 288
5079 deg
Mean motion: 15
76654042 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1103
Checksum: 294
Coasting Arc #11 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2006/282/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2341893
81 A = 6712476
56 meter
Y = 3492768
71 meter E =
0015137
Z = 5219827
84 I = 51
40543
XDOT = -6015
756837 Wp = 73
37987
YDOT = 4806
106528 meter/sec RA = 318
33902 deg
ZDOT = -511
449463 TA = 21
51636
MA = 21
45281
Ha = 190
334 n
mi
Hp = 175
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7683378
64 X = 2277305
50
Y = 11459214
91 feet Y = 3518596
03 meter
Z = 17125419
43 Z = 5231048
09
XDOT = -19736
735031 XDOT = -6066
567686
YDOT = 15768
066036 feet/sec YDOT = 4738
550894 meter/sec
ZDOT = -1677
983802 ZDOT = -540
798277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6493092
90 X = -1979094
72
Y = -12113562
16 feet Y = -3692213
75 meter
Z = 17167680
70 Z = 5232709
08
XDOT = 20221
456239 XDOT = 6163
499862
YDOT = -13396
692839 feet/sec YDOT = -4083
311977 meter/sec
ZDOT = -1786
683090 ZDOT = -544
581006
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
48417551
00020000 00000-0 20000-3 0 9103
2 25544 51
6365 318
6427 0012375 75
4072 284
8464 15
76708682 11190
Satellite: ISS
Catalog Number: 25544
Epoch time: 06282
48417551 = yrday
fracday
Element set: 910
Inclination: 51
6365 deg
RA of node: 318
6427 deg
Eccentricity:
0012375
Arg of perigee: 75
4072 deg
Mean anomaly: 284
8464 deg
Mean motion: 15
76708682 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1119
Checksum: 305
Coasting Arc #12 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2006/283/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 450477
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5214441
31 A = 6723786
46 meter
Y = -4016704
50 meter E =
0026399
Z = 1320580
35 I = 51
42239
XDOT = 2052
839434 Wp = 68
43806
YDOT = 4609
604063 meter/sec RA = 313
18395 deg
ZDOT = 5831
378109 TA = 306
13563
MA = 306
37965
Ha = 190
556 n
mi
Hp = 175
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17107747
07 X = 5252553
81
Y = -13178164
36 feet Y = -3958180
64 meter
Z = 4332612
70 Z = 1346005
25
XDOT = 6735
037512 XDOT = 1972
813194
YDOT = 15123
372909 feet/sec YDOT = 4632
112564 meter/sec
ZDOT = 19131
817942 ZDOT = 5841
156674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18031207
95 X = -5495912
18
Y = 11848607
52 feet Y = 3611455
57 meter
Z = 4426804
52 Z = 1349290
02
XDOT = -4602
746081 XDOT = -1402
917005
YDOT = -14266
322929 feet/sec YDOT = -4348
375229 meter/sec
ZDOT = 19168
854388 ZDOT = 5842
666818
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
49827201
00020000 00000-0 20000-3 0 9113
2 25544 51
6360 313
4134 0012723 78
6121 281
6472 15
76678904 11355
Satellite: ISS
Catalog Number: 25544
Epoch time: 06283
49827201 = yrday
fracday
Element set: 911
Inclination: 51
6360 deg
RA of node: 313
4134 deg
Eccentricity:
0012723
Arg of perigee: 78
6121 deg
Mean anomaly: 281
6472 deg
Mean motion: 15
76678904 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1135
Checksum: 280
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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