Date:
November 4th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 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 1045)
---------------------------------------
Vector Time (GMT): 2008/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1505496
45 A = 6724733
74 meter
Y = 3882650
08 meter E =
0001920
Z = 5281253
13 I = 51
74502
XDOT = -7162
221840 Wp = 320
02907
YDOT = -2821
473823 meter/sec RA = 21
70113 deg
ZDOT = 34
035604 TA = 129
65680
MA = 129
63986
Ha = 191
513 n
mi
Hp = 187
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4939292
80 X = -1574456
90
Y = 12738353
29 feet Y = 3865428
87 meter
Z = 17326945
97 Z = 5273771
99
XDOT = -23498
103151 XDOT = -7130
304687
YDOT = -9256
803882 feet/sec YDOT = -2901
387469 meter/sec
ZDOT = 111
665367 ZDOT = -
681851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4860280
34 X = -1481413
45
Y = -12807582
93 feet Y = -3903751
28 meter
Z = 17298231
38 Z = 5272500
93
XDOT = 22666
399548 XDOT = 6908
718582
YDOT = -8639
191817 feet/sec YDOT = -2633
225666 meter/sec
ZDOT = -23
107342 ZDOT = -7
043118
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 08308
54766940
00020000 00000-0 20000-3 0 9009
2 25544 51
6440 21
9692 0003884 292
3608 67
7142 15
72374941 10465
Satellite: ISS
Catalog Number: 25544
Epoch time: 08308
54766940 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 21
9692 deg
Eccentricity:
0003884
Arg of perigee: 292
3608 deg
Mean anomaly: 67
7142 deg
Mean motion: 15
72374941 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1046
Checksum: 296
Coasting Arc #2 (Orbit 1060)
---------------------------------------
Vector Time (GMT): 2008/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6540208
75 A = 6736834
07 meter
Y = 1484571
67 meter E =
0011072
Z = -562784
14 I = 51
75688
XDOT = -570
369054 Wp = 20
38377
YDOT = 4775
039285 meter/sec RA = 16
58108 deg
ZDOT = 6013
188686 TA = 333
50432
MA = 333
56088
Ha = 191
764 n
mi
Hp = 187
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21457377
80 X = 6525855
90
Y = 4870641
95 feet Y = 1557627
84 meter
Z = -1846404
64 Z = -531045
99
XDOT = -1871
289547 XDOT = -652
933458
YDOT = 15666
139385 feet/sec YDOT = 4768
199144 meter/sec
ZDOT = 19728
309336 ZDOT = 6010
217468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18954622
26 X = -5777368
87
Y = 11193928
87 feet Y = 3411909
52 meter
Z = -1723274
94 Z = -525254
20
XDOT = -8494
302548 XDOT = -2589
063417
YDOT = -11372
548357 feet/sec YDOT = -3466
352739 meter/sec
ZDOT = 19717
139092 ZDOT = 6009
783995
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 08309
50101109
00020000 00000-0 20000-3 0 9017
2 25544 51
6434 17
0860 0003901 300
6811 59
3967 15
72322379 10617
Satellite: ISS
Catalog Number: 25544
Epoch time: 08309
50101109 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 17
0860 deg
Eccentricity:
0003901
Arg of perigee: 300
6811 deg
Mean anomaly: 59
3967 deg
Mean motion: 15
72322379 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1061
Checksum: 256
Coasting Arc #3 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2008/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -525628
10 A = 6725226
61 meter
Y = -4277290
73 meter E =
0011753
Z = -5173178
22 I = 51
68914
XDOT = 7571
804284 Wp = 67
81861
YDOT = 551
519090 meter/sec RA = 11
47932 deg
ZDOT = -1223
210666 TA = 190
47279
MA = 190
49730
Ha = 191
723 n
mi
Hp = 187
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1724501
63 X = -452628
87
Y = -14033106
05 feet Y = -4282760
25 meter
Z = -16972369
48 Z = -5175554
60
XDOT = 24841
877572 XDOT = 7571
016589
YDOT = 1809
445832 feet/sec YDOT = 636
187022 meter/sec
ZDOT = -4013
158352 ZDOT = -1186
428100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10970662
04 X = 3343857
79
Y = 8900743
32 feet Y = 2712946
57 meter
Z = -16981891
52 Z = -5176080
54
XDOT = -18400
694688 XDOT = -5608
531741
YDOT = 15281
811796 feet/sec YDOT = 4657
896235 meter/sec
ZDOT = -3870
541818 ZDOT = -1179
741146
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 08310
51789464
00020000 00000-0 20000-3 0 9027
2 25544 51
6428 11
8765 0003844 303
2346 56
8447 15
72365711 10773
Satellite: ISS
Catalog Number: 25544
Epoch time: 08310
51789464 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 11
8765 deg
Eccentricity:
0003844
Arg of perigee: 303
2346 deg
Mean anomaly: 56
8447 deg
Mean motion: 15
72365711 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1077
Checksum: 292
Coasting Arc #4 (Orbit 1092)
---------------------------------------
Vector Time (GMT): 2008/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6527692
85 A = 6735632
66 meter
Y = 514837
06 meter E =
0010300
Z = 1559787
88 I = 51
69630
XDOT = -1762
081161 Wp = 112
71603
YDOT = -4781
088458 meter/sec RA = 6
33537 deg
ZDOT = -5769
963707 TA = 50
10896
MA = 50
01844
Ha = 191
821 n
mi
Hp = 187
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21416315
11 X = -6540541
98
Y = 1689097
97 feet Y = 441768
75 meter
Z = 5117414
30 Z = 1528044
60
XDOT = -5781
106171 XDOT = -1680
457370
YDOT = -15685
985754 feet/sec YDOT = -4800
336567 meter/sec
ZDOT = -18930
327122 ZDOT = -5778
325874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13878497
84 X = 4230166
14
Y = -16436018
72 feet Y = -5009698
51 meter
Z = 4994408
92 Z = 1522295
84
XDOT = 13943
361458 XDOT = 4249
936573
YDOT = 5984
599846 feet/sec YDOT = 1824
106033 meter/sec
ZDOT = -18963
088583 ZDOT = -5779
949400
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 08311
53476325
00020000 00000-0 20000-3 0 9030
2 25544 51
6434 6
6670 0003883 310
8148 49
2677 15
72434850 10934
Satellite: ISS
Catalog Number: 25544
Epoch time: 08311
53476325 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 6
6670 deg
Eccentricity:
0003883
Arg of perigee: 310
8148 deg
Mean anomaly: 49
2677 deg
Mean motion: 15
72434850 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1093
Checksum: 286
Coasting Arc #5 (Orbit 1108)
---------------------------------------
Vector Time (GMT): 2008/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2514907
04 A = 6726282
27 meter
Y = 3905022
66 meter E =
0003023
Z = 4862888
86 I = 51
63544
XDOT = -7140
481363 Wp = 106
36822
YDOT = 1691
423200 meter/sec RA = 1
24666 deg
ZDOT = 2332
508646 TA = 320
89329
MA = 320
91513
Ha = 191
843 n
mi
Hp = 187
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8251007
34 X = 2447430
05
Y = 12811754
14 feet Y = 3932768
50 meter
Z = 15954359
77 Z = 4874942
62
XDOT = -23426
776126 XDOT = -7170
195550
YDOT = 5549
288714 feet/sec YDOT = 1611
408059 meter/sec
ZDOT = 7652
587421 ZDOT = 2297
747368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14899903
25 X = -4541490
51
Y = -2951423
91 feet Y = -899594
01 meter
Z = 16001366
88 Z = 4877216
63
XDOT = 11986
400882 XDOT = 3653
454989
YDOT = -19716
631998 feet/sec YDOT = -6009
629433 meter/sec
ZDOT = 7517
971994 ZDOT = 2291
477864
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 08312
55161848
00020000 00000-0 20000-3 0 9045
2 25544 51
6431 1
4574 0003820 314
2907 45
7941 15
72441511 11094
Satellite: ISS
Catalog Number: 25544
Epoch time: 08312
55161848 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 1
4574 deg
Eccentricity:
0003820
Arg of perigee: 314
2907 deg
Mean anomaly: 45
7941 deg
Mean motion: 15
72441511 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1109
Checksum: 261
Coasting Arc #6 (Orbit 1123)
---------------------------------------
Vector Time (GMT): 2008/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5782636
14 A = 6733917
16 meter
Y = -2375092
03 meter E =
0006676
Z = -2494073
80 I = 51
63184
XDOT = 3914
295298 Wp = 13
37507
YDOT = 3953
470907 meter/sec RA = 356
08298 deg
ZDOT = 5319
822511 TA = 318
41979
MA = 318
47054
Ha = 192
058 n
mi
Hp = 187
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18971903
35 X = 5820881
05
Y = -7792296
69 feet Y = -2310213
43 meter
Z = -8182656
82 Z = -2465888
21
XDOT = 12842
176173 XDOT = 3843
952715
YDOT = 12970
705075 feet/sec YDOT = 3996
849561 meter/sec
ZDOT = 17453
485929 ZDOT = 5338
667676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7174247
83 X = -2186710
74
Y = 19260225
91 feet Y = 5870516
86 meter
Z = -8073583
04 Z = -2460828
11
XDOT = -16769
035547 XDOT = -5111
202035
YDOT = 1087
841363 feet/sec YDOT = 331
574047 meter/sec
ZDOT = 17526
819150 ZDOT = 5342
174477
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 08313
50490861
00020000 00000-0 20000-3 0 9052
2 25544 51
6432 356
5734 0003784 319
8227 40
2655 15
72464530 11247
Satellite: ISS
Catalog Number: 25544
Epoch time: 08313
50490861 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 356
5734 deg
Eccentricity:
0003784
Arg of perigee: 319
8227 deg
Mean anomaly: 40
2655 deg
Mean motion: 15
72464530 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1124
Checksum: 281
Coasting Arc #7 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2008/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213100
38 A = 6728051
93 meter
Y = -2867327
76 meter E =
0009242
Z = -4401940
23 I = 51
58382
XDOT = 5925
541116 Wp = 45
57409
YDOT = -3604
907021 meter/sec RA = 351
00217 deg
ZDOT = -3321
111906 TA = 190
96688
MA = 190
98704
Ha = 192
125 n
mi
Hp = 186
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13822507
81 X = -4159339
92
Y = -9407243
30 feet Y = -2914140
55 meter
Z = -14442061
11 Z = -4422277
39
XDOT = 19440
751694 XDOT = 5981
545161
YDOT = -11827
122773 feet/sec YDOT = -3538
331102 meter/sec
ZDOT = -10896
036437 ZDOT = -3292
188777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16165436
16 X = 4927224
94
Y = -3993439
91 feet Y = -1217200
49 meter
Z = -14521094
63 Z = -4426029
64
XDOT = -4444
063052 XDOT = -1354
550418
YDOT = 21248
906815 feet/sec YDOT = 6476
666797 meter/sec
ZDOT = -10784
197574 ZDOT = -3287
023421
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 08314
52173754
00020000 00000-0 20000-3 0 9065
2 25544 51
6438 351
3636 0003775 325
1740 34
9175 15
72468597 11409
Satellite: ISS
Catalog Number: 25544
Epoch time: 08314
52173754 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 351
3636 deg
Eccentricity:
0003775
Arg of perigee: 325
1740 deg
Mean anomaly: 34
9175 deg
Mean motion: 15
72468597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1140
Checksum: 296
Coasting Arc #8 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2008/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4459137
43 A = 6731788
05 meter
Y = 3817973
72 meter E =
0011251
Z = 3288765
01 I = 51
56671
XDOT = -5578
136544 Wp = 74
53687
YDOT = -2444
904468 meter/sec RA = 345
82504 deg
ZDOT = -4708
614849 TA = 66
85807
MA = 66
73955
Ha = 192
240 n
mi
Hp = 186
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14629715
99 X = -4517475
95
Y = 12526160
49 feet Y = 3767782
89 meter
Z = 10789911
44 Z = 3266960
10
XDOT = -18300
972913 XDOT = -5527
508312
YDOT = -8021
340117 feet/sec YDOT = -2506
999359 meter/sec
ZDOT = -15448
211447 ZDOT = -4735
591308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 96720
49 X = 29480
40
Y = -19306334
78 feet Y = -5884570
84 meter
Z = 10705678
77 Z = 3263090
89
XDOT = 16555
305368 XDOT = 5046
057076
YDOT = -8571
288950 feet/sec YDOT = -2612
528872 meter/sec
ZDOT = -15552
942117 ZDOT = -4740
536757
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 08315
53855156
00020000 00000-0 20000-3 0 9071
2 25544 51
6428 346
1539 0003903 330
7237 29
3706 15
72515409 11568
Satellite: ISS
Catalog Number: 25544
Epoch time: 08315
53855156 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 346
1539 deg
Eccentricity:
0003903
Arg of perigee: 330
7237 deg
Mean anomaly: 29
3706 deg
Mean motion: 15
72515409 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1156
Checksum: 291
Coasting Arc #9 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2008/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5396201
61 A = 6730093
59 meter
Y = 1307491
74 meter E =
0009989
Z = 3793332
70 I = 51
53249
XDOT = -4146
627711 Wp = 78
65659
YDOT = 4966
056979 meter/sec RA = 340
74537 deg
ZDOT = 4179
738330 TA = 327
43804
MA = 327
49961
Ha = 192
271 n
mi
Hp = 186
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17704073
52 X = 5362751
97
Y = 4289671
05 feet Y = 1367648
08 meter
Z = 12445317
25 Z = 3819467
17
XDOT = -13604
421623 XDOT = -4222
155925
YDOT = 16292
837859 feet/sec YDOT = 4919
264613 meter/sec
ZDOT = 13713
052265 ZDOT = 4159
409913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14573545
85 X = -4442016
78
Y = 10812656
33 feet Y = 3295697
65 meter
Z = 12546698
48 Z = 3824233
70
XDOT = -2987
699112 XDOT = -910
650689
YDOT = -19875
815055 feet/sec YDOT = -6058
148429 meter/sec
ZDOT = 13634
623307 ZDOT = 4155
833184
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 08316
55535385
00020000 00000-0 20000-3 0 9084
2 25544 51
6423 340
9435 0003853 337
3143 22
7848 15
72501547 11723
Satellite: ISS
Catalog Number: 25544
Epoch time: 08316
55535385 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 340
9435 deg
Eccentricity:
0003853
Arg of perigee: 337
3143 deg
Mean anomaly: 22
7848 deg
Mean motion: 15
72501547 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1172
Checksum: 289
Coasting Arc #10 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2008/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2709441
61 A = 6729547
04 meter
Y = -4706220
59 meter E =
0005490
Z = -3977843
85 I = 51
50442
XDOT = 6586
440168 Wp = 72
55436
YDOT = 457
973182 meter/sec RA = 335
56135 deg
ZDOT = 3950
501905 TA = 238
41735
MA = 238
47095
Ha = 192
430 n
mi
Hp = 186
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8889244
11 X = 2781190
34
Y = -15440356
27 feet Y = -4675520
67 meter
Z = -13050668
81 Z = -3964506
85
XDOT = 21609
055668 XDOT = 6561
637957
YDOT = 1502
536685 feet/sec YDOT = 531
487678 meter/sec
ZDOT = 12960
964254 ZDOT = 3982
439828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6425901
46 X = 1958614
76
Y = 16657397
13 feet Y = 5077174
65 meter
Z = -12999312
68 Z = -3962190
50
XDOT = -13440
872034 XDOT = -4096
777796
YDOT = 15380
675823 feet/sec YDOT = 4688
029991 meter/sec
ZDOT = 13084
775559 ZDOT = 3988
239590
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 08317
50859163
00020000 00000-0 20000-3 0 9094
2 25544 51
6433 336
0594 0003958 339
8194 20
2811 15
72530819 11878
Satellite: ISS
Catalog Number: 25544
Epoch time: 08317
50859163 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 336
0594 deg
Eccentricity:
0003958
Arg of perigee: 339
8194 deg
Mean anomaly: 20
2811 deg
Mean motion: 15
72530819 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1187
Checksum: 304
Coasting Arc #11 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2008/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5953597
03 A = 6732035
84 meter
Y = 533678
35 meter E =
0004312
Z = -3102935
04 I = 51
48594
XDOT = 2032
543918 Wp = 49
48780
YDOT = -5600
287251 meter/sec RA = 330
47655 deg
ZDOT = -4864
711636 TA = 166
58571
MA = 166
57424
Ha = 192
457 n
mi
Hp = 186
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19532798
64 X = -5944048
17
Y = 1750913
23 feet Y = 467155
46 meter
Z = -10180233
07 Z = -3131835
43
XDOT = 6668
451174 XDOT = 2118
648924
YDOT = -18373
645835 feet/sec YDOT = -5577
076300 meter/sec
ZDOT = -15960
340013 ZDOT = -4854
628518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10547141
93 X = 3214768
86
Y = -16463941
62 feet Y = -5018209
41 meter
Z = -10292205
25 Z = -3137064
16
XDOT = 9179
581070 XDOT = 2797
936310
YDOT = 15830
439956 feet/sec YDOT = 4825
118098 meter/sec
ZDOT = -15921
651241 ZDOT = -4852
919298
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 08318
52536588
00020000 00000-0 20000-3 0 9102
2 25544 51
6422 330
8486 0003930 343
3346 16
7687 15
72550988 12036
Satellite: ISS
Catalog Number: 25544
Epoch time: 08318
52536588 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 330
8486 deg
Eccentricity:
0003930
Arg of perigee: 343
3346 deg
Mean anomaly: 16
7687 deg
Mean motion: 15
72550988 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1203
Checksum: 300
Coasting Arc #12 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2008/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 626690
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -823307
80 A = 6727410
76 meter
Y = 4931725
11 meter E =
0010397
Z = 4498515
65 I = 51
44476
XDOT = -6830
080418 Wp = 44
46075
YDOT = 1711
308290 meter/sec RA = 325
29132 deg
ZDOT = -3114
486857 TA = 76
74727
MA = 76
63132
Ha = 192
528 n
mi
Hp = 186
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2701141
08 X = -900247
62
Y = 16180200
50 feet Y = 4922087
69 meter
Z = 14758909
60 Z = 4494329
58
XDOT = -22408
400322 XDOT = -6833
578829
YDOT = 5614
528512 feet/sec YDOT = 1634
911189 meter/sec
ZDOT = -10218
132733 ZDOT = -3147
676724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11288092
58 X = -3440610
62
Y = -11922358
84 feet Y = -3633934
98 meter
Z = 14743025
11 Z = 4493674
05
XDOT = 8021
363715 XDOT = 2444
911660
YDOT = -20436
463117 feet/sec YDOT = -6229
033958 meter/sec
ZDOT = -10346
655378 ZDOT = -3153
660559
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 08319
54212584
00020000 00000-0 20000-3 0 9113
2 25544 51
6414 325
6377 0004028 347
7825 12
3239 15
72594880 12198
Satellite: ISS
Catalog Number: 25544
Epoch time: 08319
54212584 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 325
6377 deg
Eccentricity:
0004028
Arg of perigee: 347
7825 deg
Mean anomaly: 12
3239 deg
Mean motion: 15
72594880 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1219
Checksum: 293
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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