Date:
September 25th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3875 01 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
263/05:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 190
3
000/00:00:00
000 0
0 0
0 179
1
Coasting Arc #1 (Orbit 806)
---------------------------------------
Vector Time (GMT): 2006/262/15:45:24
000
Vector Time (MET): N/A
Weight (LBS) : 465373
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3460279
09 A = 6714537
64 meter
Y = 2287919
64 meter E =
0011531
Z = 5277282
12 I = 51
88826
XDOT = -3993
758216 Wp = 12
82529
YDOT = -6586
962469 meter/sec RA = 60
21787 deg
ZDOT = 247
949113 TA = 74
89508
MA = 74
76754
Ha = 190
051 n
mi
Hp = 179
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11352621
67 X = -3511241
64
Y = 7506298
04 feet Y = 2248940
24 meter
Z = 17313917
72 Z = 5260348
29
XDOT = -13102
881285 XDOT = -3921
009553
YDOT = -21610
769256 feet/sec YDOT = -6631
216113 meter/sec
ZDOT = 813
481342 ZDOT = 228
724662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 648932
46 X = 197794
61
Y = -13673889
27 feet Y = -4167801
45 meter
Z = 17251142
42 Z = 5258148
21
XDOT = 24191
707564 XDOT = 7373
632466
YDOT = 2037
566661 feet/sec YDOT = 621
050318 meter/sec
ZDOT = 740
959902 ZDOT = 225
844578
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 06262
70449562
00020000 00000-0 20000-3 0 9002
2 25544 51
6349 60
5710 0011689 1
1508 358
9681 15
75957702 8072
Satellite: ISS
Catalog Number: 25544
Epoch time: 06262
70449562 = yrday
fracday
Element set: 900
Inclination: 51
6349 deg
RA of node: 60
5710 deg
Eccentricity:
0011689
Arg of perigee: 1
1508 deg
Mean anomaly: 358
9681 deg
Mean motion: 15
75957702 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 807
Checksum: 296
Coasting Arc #2 (Orbit 815)
---------------------------------------
Vector Time (GMT): 2006/263/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5011766
05 A = 6719653
92 meter
Y = -1939083
52 meter E =
0018493
Z = 4035143
09 I = 51
89663
XDOT = -609
096563 Wp = 37
93713
YDOT = -6607
928929 meter/sec RA = 57
22682 deg
ZDOT = -3908
247438 TA = 92
32764
MA = 92
11588
Ha = 190
313 n
mi
Hp = 179
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16442801
99 X = -5009312
35
Y = -6361822
57 feet Y = -1995113
87 meter
Z = 13238658
44 Z = 4010802
16
XDOT = -1998
348303 XDOT = -516
175065
YDOT = -21679
556853 feet/sec YDOT = -6614
220895 meter/sec
ZDOT = -12822
334115 ZDOT = -3910
980266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8395086
75 X = -2558822
44
Y = 15580784
06 feet Y = 4749022
98 meter
Z = 13147710
35 Z = 4007422
11
XDOT = -20613
183629 XDOT = -6282
898370
YDOT = -211
154950 feet/sec YDOT = -64
360029 meter/sec
ZDOT = -12833
418355 ZDOT = -3911
625914
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 06263
27520526
00020000 00000-0 20000-3 0 9016
2 25544 51
6347 57
6351 0012298 3
9252 356
2006 15
75946547 8168
Satellite: ISS
Catalog Number: 25544
Epoch time: 06263
27520526 = yrday
fracday
Element set: 901
Inclination: 51
6347 deg
RA of node: 57
6351 deg
Eccentricity:
0012298
Arg of perigee: 3
9252 deg
Mean anomaly: 356
2006 deg
Mean motion: 15
75946547 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 816
Checksum: 286
Coasting Arc #3 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2006/264/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 391432
53 A = 6720097
82 meter
Y = 5461128
59 meter E =
0016407
Z = 3877467
34 I = 51
88231
XDOT = -6028
626254 Wp = 50
60135
YDOT = -2492
255167 meter/sec RA = 52
14483 deg
ZDOT = 4117
482792 TA = 356
67206
MA = 356
68296
Ha = 190
440 n
mi
Hp = 178
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1284227
45 X = 311500
33
Y = 17917088
56 feet Y = 5465059
19 meter
Z = 12721349
53 Z = 3879174
33
XDOT = -19778
957527 XDOT = -6020
311414
YDOT = -8176
690182 feet/sec YDOT = -2559
623790 meter/sec
ZDOT = 13508
801811 ZDOT = 4088
216165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17942438
67 X = 5468855
31
Y = 747907
78 feet Y = 227962
29 meter
Z = 12728454
94 Z = 3879633
07
XDOT = -10239
463642 XDOT = -3120
988518
YDOT = 17534
174176 feet/sec YDOT = 5344
416289 meter/sec
ZDOT = 13399
429162 ZDOT = 4084
146008
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 06264
28978912
00020000 00000-0 20000-3 0 9025
2 25544 51
6353 52
4083 0012345 7
8079 352
3275 15
75935271 8328
Satellite: ISS
Catalog Number: 25544
Epoch time: 06264
28978912 = yrday
fracday
Element set: 902
Inclination: 51
6353 deg
RA of node: 52
4083 deg
Eccentricity:
0012345
Arg of perigee: 7
8079 deg
Mean anomaly: 352
3275 deg
Mean motion: 15
75935271 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 832
Checksum: 295
Coasting Arc #4 (Orbit 846)
---------------------------------------
Vector Time (GMT): 2006/265/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5492368
88 A = 6722537
79 meter
Y = 2338754
70 meter E =
0015012
Z = -3080799
34 I = 51
87238
XDOT = 232
655789 Wp = 25
63520
YDOT = 5918
127407 meter/sec RA = 46
96028 deg
ZDOT = 4929
562504 TA = 298
70288
MA = 298
85369
Ha = 190
558 n
mi
Hp = 178
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18019582
95 X = 5480774
42
Y = 7673079
74 feet Y = 2400108
33 meter
Z = -10107609
40 Z = -3054145
69
XDOT = 763
306393 XDOT = 142
514172
YDOT = 19416
428501 feet/sec YDOT = 5920
225505 meter/sec
ZDOT = 16173
105327 ZDOT = 4930
473291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9303288
86 X = 2835642
45
Y = -17292603
31 feet Y = -5270785
49 meter
Z = -10007995
67 Z = -3050437
08
XDOT = 18134
926628 XDOT = 5527
525636
YDOT = 436
326742 feet/sec YDOT = 132
992391 meter/sec
ZDOT = 16177
305161 ZDOT = 4930
842613
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 06265
24094985
00020000 00000-0 20000-3 0 9032
2 25544 51
6355 47
5087 0012402 10
3727 349
7691 15
75960051 8474
Satellite: ISS
Catalog Number: 25544
Epoch time: 06265
24094985 = yrday
fracday
Element set: 903
Inclination: 51
6355 deg
RA of node: 47
5087 deg
Eccentricity:
0012402
Arg of perigee: 10
3727 deg
Mean anomaly: 349
7691 deg
Mean motion: 15
75960051 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 847
Checksum: 298
Coasting Arc #5 (Orbit 862)
---------------------------------------
Vector Time (GMT): 2006/266/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73574
02 A = 6717095
93 meter
Y = -4853792
93 meter E =
0020519
Z = -4661172
09 I = 51
83395
XDOT = 6544
366755 Wp = 39
81826
YDOT = 2850
698213 meter/sec RA = 41
87049 deg
ZDOT = -2856
677002 TA = 201
93668
MA = 202
02464
Ha = 190
534 n
mi
Hp = 178
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 241384
57 X = 150487
66
Y = -15924517
49 feet Y = -4852540
54 meter
Z = -15292559
36 Z = -4660627
43
XDOT = 21471
019538 XDOT = 6525
880802
YDOT = 9352
684426 feet/sec YDOT = 2923
777344 meter/sec
ZDOT = -9372
299875 ZDOT = -2824
929349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15855293
20 X = -4832693
37
Y = -1516607
33 feet Y = -462261
91 meter
Z = -15291189
47 Z = -4660754
55
XDOT = 10826
754078 XDOT = 3299
994643
YDOT = -19605
843960 feet/sec YDOT = -5975
861239 meter/sec
ZDOT = -9253
644542 ZDOT = -2820
510856
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 06266
25551090
00020000 00000-0 20000-3 0 9040
2 25544 51
6354 42
2822 0012422 13
8806 346
2697 15
75988233 8638
Satellite: ISS
Catalog Number: 25544
Epoch time: 06266
25551090 = yrday
fracday
Element set: 904
Inclination: 51
6354 deg
RA of node: 42
2822 deg
Eccentricity:
0012422
Arg of perigee: 13
8806 deg
Mean anomaly: 346
2697 deg
Mean motion: 15
75988233 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 863
Checksum: 290
Coasting Arc #6 (Orbit 878)
---------------------------------------
Vector Time (GMT): 2006/267/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5921141
61 A = 6725053
04 meter
Y = -2588631
07 meter E =
0017902
Z = 1861192
32 I = 51
83912
XDOT = 475
595951 Wp = 69
77431
YDOT = -5194
754439 meter/sec RA = 36
69486 deg
ZDOT = -5662
255472 TA = 89
61685
MA = 89
41171
Ha = 190
672 n
mi
Hp = 178
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19426317
63 X = -5900796
57
Y = -8492884
08 feet Y = -2654730
65 meter
Z = 6106274
01 Z = 1832476
67
XDOT = 1560
354171 XDOT = 561
155639
YDOT = -17043
157607 feet/sec YDOT = -5188
958122 meter/sec
ZDOT = -18576
953647 ZDOT = -5659
736758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9601213
65 X = -2926449
92
Y = 18937442
29 feet Y = 5772132
41 meter
Z = 5998954
50 Z = 1828481
33
XDOT = -15537
715910 XDOT = -4735
895809
YDOT = -1942
873377 feet/sec YDOT = -592
187805 meter/sec
ZDOT = -18568
272321 ZDOT = -5659
609403
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 06267
27006176
00020000 00000-0 20000-3 0 9054
2 25544 51
6358 37
0560 0012456 18
4126 341
7487 15
75995089 8797
Satellite: ISS
Catalog Number: 25544
Epoch time: 06267
27006176 = yrday
fracday
Element set: 905
Inclination: 51
6358 deg
RA of node: 37
0560 deg
Eccentricity:
0012456
Arg of perigee: 18
4126 deg
Mean anomaly: 341
7487 deg
Mean motion: 15
75995089 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 879
Checksum: 313
Coasting Arc #7 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2006/268/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -804707
43 A = 6714985
46 meter
Y = 4247109
76 meter E =
0012221
Z = 5129853
85 I = 51
78161
XDOT = -6968
560419 Wp = 41
60536
YDOT = -2995
700716 meter/sec RA = 31
58398 deg
ZDOT = 1394
146229 TA = 35
13265
MA = 35
05212
Ha = 190
799 n
mi
Hp = 177
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2640116
24 X = -877059
71
Y = 13934087
16 feet Y = 4237706
88 meter
Z = 16830229
17 Z = 5125768
49
XDOT = -22862
731033 XDOT = -6941
316782
YDOT = -9828
414421 feet/sec YDOT = -3073
474599 meter/sec
ZDOT = 4573
970568 ZDOT = 1360
358782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13811783
90 X = 4209831
73
Y = 3294921
05 feet Y = 1004291
94 meter
Z = 16815580
08 Z = 5125388
81
XDOT = -10507
009067 XDOT = -3202
536364
YDOT = 21463
638763 feet/sec YDOT = 6542
117095 meter/sec
ZDOT = 4447
708633 ZDOT = 1355
661591
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 06268
28459994
00020000 00000-0 20000-3 0 9067
2 25544 51
6356 31
8291 0012504 21
8734 338
2961 15
76004880 8952
Satellite: ISS
Catalog Number: 25544
Epoch time: 06268
28459994 = yrday
fracday
Element set: 906
Inclination: 51
6356 deg
RA of node: 31
8291 deg
Eccentricity:
0012504
Arg of perigee: 21
8734 deg
Mean anomaly: 338
2961 deg
Mean motion: 15
76004880 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 895
Checksum: 311
Coasting Arc #8 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2006/269/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6172773
18 A = 6726297
93 meter
Y = 2582209
40 meter E =
0023436
Z = -552382
61 I = 51
79432
XDOT = -1398
273814 Wp = 32
04088
YDOT = 4603
138606 meter/sec RA = 26
42621 deg
ZDOT = 6027
881515 TA = 321
94909
MA = 322
11438
Ha = 190
823 n
mi
Hp = 177
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20251880
53 X = 6146123
21
Y = 8471815
61 feet Y = 2651087
73 meter
Z = -1812278
90 Z = -522459
58
XDOT = -4587
512513 XDOT = -1478
925727
YDOT = 15102
160782 feet/sec YDOT = 4587
051676 meter/sec
ZDOT = 19776
514156 ZDOT = 6020
892447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8941701
11 X = 2725430
50
Y = -20058640
47 feet Y = -6113873
61 meter
Z = -1700471
52 Z = -518303
72
XDOT = 13525
684841 XDOT = 4122
628739
YDOT = 4395
116214 feet/sec YDOT = 1339
631422 meter/sec
ZDOT = 19751
091397 ZDOT = 6020
132658
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 06269
23571835
00020000 00000-0 20000-3 0 9073
2 25544 51
6349 26
9291 0012541 24
7353 335
4410 15
76028311 9100
Satellite: ISS
Catalog Number: 25544
Epoch time: 06269
23571835 = yrday
fracday
Element set: 907
Inclination: 51
6349 deg
RA of node: 26
9291 deg
Eccentricity:
0012541
Arg of perigee: 24
7353 deg
Mean anomaly: 335
4410 deg
Mean motion: 15
76028311 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 910
Checksum: 275
Coasting Arc #9 (Orbit 925)
---------------------------------------
Vector Time (GMT): 2006/270/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1688235
08 A = 6714248
76 meter
Y = -3813082
53 meter E =
0023548
Z = -5279947
21 I = 51
72692
XDOT = 7110
968497 Wp = 62
98216
YDOT = 2919
707793 meter/sec RA = 21
28635 deg
ZDOT = 176
210861 TA = 208
62584
MA = 208
75532
Ha = 190
825 n
mi
Hp = 177
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5538828
99 X = 1756397
53
Y = -12510113
28 feet Y = -3793822
78 meter
Z = -17322661
44 Z = -5271579
94
XDOT = 23329
949137 XDOT = 7076
935400
YDOT = 9579
093808 feet/sec YDOT = 2999
036296 meter/sec
ZDOT = 578
119623 ZDOT = 210
673846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12475293
93 X = -3802469
59
Y = -5710524
61 feet Y = -1740567
90 meter
Z = -17291995
56 Z = -5270600
25
XDOT = 9304
860493 XDOT = 2836
121478
YDOT = -22357
793525 feet/sec YDOT = -6814
655467 meter/sec
ZDOT = 706
880874 ZDOT = 215
457290
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 06270
25023394
00020000 00000-0 20000-3 0 9080
2 25544 51
6338 21
7017 0012524 28
7386 331
4466 15
76063478 9265
Satellite: ISS
Catalog Number: 25544
Epoch time: 06270
25023394 = yrday
fracday
Element set: 908
Inclination: 51
6338 deg
RA of node: 21
7017 deg
Eccentricity:
0012524
Arg of perigee: 28
7386 deg
Mean anomaly: 331
4466 deg
Mean motion: 15
76063478 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 926
Checksum: 287
Coasting Arc #10 (Orbit 941)
---------------------------------------
Vector Time (GMT): 2006/271/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6182240
84 A = 6725938
56 meter
Y = -2509200
12 meter E =
0013286
Z = -875297
62 I = 51
73965
XDOT = 2522
790485 Wp = 77
95654
YDOT = -4162
339639 meter/sec RA = 16
15246 deg
ZDOT = -5959
525851 TA = 111
57883
MA = 111
43720
Ha = 190
891 n
mi
Hp = 177
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20282942
39 X = -6149471
03
Y = -8232283
85 feet Y = -2578150
14 meter
Z = -2871711
35 Z = -905251
84
XDOT = 8276
871669 XDOT = 2598
097636
YDOT = -13655
969943 feet/sec YDOT = -4133
707381 meter/sec
ZDOT = -19552
250167 ZDOT = -5947
086970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8006812
68 X = -2440476
51
Y = 20356913
30 feet Y = 6204787
17 meter
Z = -2983623
12 Z = -909408
33
XDOT = -12263
516016 XDOT = -3737
919682
YDOT = -7648
638342 feet/sec YDOT = -2331
304967 meter/sec
ZDOT = -19506
458447 ZDOT = -5945
568535
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 06271
26473808
00020000 00000-0 20000-3 0 9092
2 25544 51
6339 16
4755 0012521 32
4734 327
7198 15
76064860 9426
Satellite: ISS
Catalog Number: 25544
Epoch time: 06271
26473808 = yrday
fracday
Element set: 909
Inclination: 51
6339 deg
RA of node: 16
4755 deg
Eccentricity:
0012521
Arg of perigee: 32
4734 deg
Mean anomaly: 327
7198 deg
Mean motion: 15
76064860 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 942
Checksum: 300
Coasting Arc #11 (Orbit 957)
---------------------------------------
Vector Time (GMT): 2006/272/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2713183
26 A = 6715276
54 meter
Y = 3521111
99 meter E =
0017775
Z = 5026879
62 I = 51
67563
XDOT = -6961
954428 Wp = 41
43629
YDOT = -2789
668847 meter/sec RA = 10
98115 deg
ZDOT = -1786
889284 TA = 65
83944
MA = 65
65370
Ha = 191
004 n
mi
Hp = 177
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8901519
87 X = -2776775
18
Y = 11552204
70 feet Y = 3490416
08 meter
Z = 16492387
22 Z = 5013544
35
XDOT = -22841
057835 XDOT = -6921
562032
YDOT = -9152
456846 feet/sec YDOT = -2867
295420 meter/sec
ZDOT = -5862
497652 ZDOT = -1820
612827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11801853
52 X = 3597204
95
Y = 8661858
35 feet Y = 2640134
42 meter
Z = 16443168
46 Z = 5011877
75
XDOT = -7871
681549 XDOT = -2399
288536
YDOT = 22197
623822 feet/sec YDOT = 6765
835741 meter/sec
ZDOT = -5988
489818 ZDOT = -1825
291697
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
27922975
00020000 00000-0 20000-3 0 9100
2 25544 51
6334 11
2478 0012483 36
2206 323
9801 15
76084120 9586
Satellite: ISS
Catalog Number: 25544
Epoch time: 06272
27922975 = yrday
fracday
Element set: 910
Inclination: 51
6334 deg
RA of node: 11
2478 deg
Eccentricity:
0012483
Arg of perigee: 36
2206 deg
Mean anomaly: 323
9801 deg
Mean motion: 15
76084120 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 958
Checksum: 278
Coasting Arc #12 (Orbit 973)
---------------------------------------
Vector Time (GMT): 2006/273/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5883141
22 A = 6723978
44 meter
Y = 2355482
50 meter E =
0025495
Z = 2203709
32 I = 51
67643
XDOT = -3666
712018 Wp = 56
53873
YDOT = 3988
683554 meter/sec RA = 5
86619 deg
ZDOT = 5493
978692 TA = 328
21158
MA = 328
36523
Ha = 190
883 n
mi
Hp = 176
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19301644
44 X = 5845659
32
Y = 7727960
96 feet Y = 2421061
45 meter
Z = 7230017
44 Z = 2232198
87
XDOT = -12029
895072 XDOT = -3737
730521
YDOT = 13086
232131 feet/sec YDOT = 3947
283208 meter/sec
ZDOT = 18024
864474 ZDOT = 5475
993171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6843727
23 X = 2085968
06
Y = -19593054
32 feet Y = -5971962
96 meter
Z = 7336459
01 Z = 2236152
71
XDOT = 12195
462561 XDOT = 3717
176989
YDOT = 11022
279186 feet/sec YDOT = 3359
590696 meter/sec
ZDOT = 17958
379308 ZDOT = 5473
714013
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
29370935
00020000 00000-0 20000-3 0 9117
2 25544 51
6325 6
0201 0012454 40
3742 319
8345 15
76121398 9745
Satellite: ISS
Catalog Number: 25544
Epoch time: 06273
29370935 = yrday
fracday
Element set: 911
Inclination: 51
6325 deg
RA of node: 6
0201 deg
Eccentricity:
0012454
Arg of perigee: 40
3742 deg
Mean anomaly: 319
8345 deg
Mean motion: 15
76121398 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 974
Checksum: 274
Coasting Arc #13 (Orbit 988)
---------------------------------------
Vector Time (GMT): 2006/274/05:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 480828
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3659905
40 A = 6717618
23 meter
Y = -3476543
31 meter E =
0018496
Z = -4444200
14 I = 51
62609
XDOT = 6448
621923 Wp = 71
93027
YDOT = 2651
561904 meter/sec RA =
67053 deg
ZDOT = 3253
036973 TA = 230
62398
MA = 230
78796
Ha = 191
056 n
mi
Hp = 176
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12007563
64 X = 3720097
81
Y = -11405981
98 feet Y = -3435279
65 meter
Z = -14580709
13 Z = -4426274
04
XDOT = 21156
896072 XDOT = 6402
689765
YDOT = 8699
350080 feet/sec YDOT = 2723
417131 meter/sec
ZDOT = 10672
693482 ZDOT = 3284
252988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12140876
93 X = -3700539
29
Y = -11349320
19 feet Y = -3459272
79 meter
Z = -14514376
56 Z = -4423981
98
XDOT = 6532
458019 XDOT = 1991
093204
YDOT = -20716
039395 feet/sec YDOT = -6314
248808 meter/sec
ZDOT = 10789
336224 ZDOT = 3288
589681
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
24477441
00020000 00000-0 20000-3 0 9124
2 25544 51
6321 1
1189 0012541 44
4813 315
7356 15
76124132 9895
Satellite: ISS
Catalog Number: 25544
Epoch time: 06274
24477441 = yrday
fracday
Element set: 912
Inclination: 51
6321 deg
RA of node: 1
1189 deg
Eccentricity:
0012541
Arg of perigee: 44
4813 deg
Mean anomaly: 315
7356 deg
Mean motion: 15
76124132 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 989
Checksum: 271
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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