Date:
December 15th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 95 ET - UTC (sec) : 66 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 3436)
---------------------------------------
Vector Time (GMT): 2009/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3008168
72 A = 6721842
22 meter
Y = -5381379
00 meter E =
0011486
Z = -2686022
32 I = 51
98486
XDOT = 3405
974762 Wp = 97
81670
YDOT = 4504
380548 meter/sec RA = 99
29292 deg
ZDOT = -5230
383602 TA = 112
64590
MA = 112
52439
Ha = 188
900 n
mi
Hp = 177
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9869319
96 X = 3081169
07
Y = -17655442
90 feet Y = -5347331
32 meter
Z = -8812409
17 Z = -2671231
88
XDOT = 11174
457881 XDOT = 3380
761466
YDOT = 14778
151403 feet/sec YDOT = 4542
327952 meter/sec
ZDOT = -17160
051187 ZDOT = -5213
897727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16214058
02 X = 4942044
88
Y = 12134570
87 feet Y = 3698617
20 meter
Z = -8754039
55 Z = -2668231
25
XDOT = -15234
756431 XDOT = -4643
553760
YDOT = 8072
833854 feet/sec YDOT = 2460
599759 meter/sec
ZDOT = -17094
706250 ZDOT = -5210
466465
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 09348
52640251
00016717 00000-0 10270-3 0 9006
2 25544 51
6439 99
9460 0007448 80
3331 279
8675 15
76542327 34371
Satellite: ISS
Catalog Number: 25544
Epoch time: 09348
52640251 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 99
9460 deg
Eccentricity:
0007448
Arg of perigee: 80
3331 deg
Mean anomaly: 279
8675 deg
Mean motion: 15
76542327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 331
Coasting Arc #2 (Orbit 3452)
---------------------------------------
Vector Time (GMT): 2009/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2856251
30 A = 6717801
21 meter
Y = -4516666
07 meter E =
0018279
Z = 4057635
52 I = 51
97547
XDOT = 3456
770626 Wp = 79
78410
YDOT = -5693
745961 meter/sec RA = 94
11465 deg
ZDOT = -3886
720683 TA = 50
07155
MA = 49
91107
Ha = 189
006 n
mi
Hp = 177
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9370903
22 X = -2825244
33
Y = -14818458
24 feet Y = -4548433
62 meter
Z = 13312452
48 Z = 4043834
31
XDOT = 11341
110978 XDOT = 3539
063355
YDOT = -18680
268901 feet/sec YDOT = -5654
629580 meter/sec
ZDOT = -12751
708276 ZDOT = -3869
728514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15791659
98 X = 4813297
96
Y = -7712195
43 feet Y = -2350677
17 meter
Z = 13257731
30 Z = 4040956
50
XDOT = 16707
298772 XDOT = 5092
384666
YDOT = 12303
484265 feet/sec YDOT = 3750
102004 meter/sec
ZDOT = -12684
620146 ZDOT = -3866
272221
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 09349
54058844
00016717 00000-0 10270-3 0 9011
2 25544 51
6445 94
7192 0007584 83
6846 276
5182 15
76546966 34539
Satellite: ISS
Catalog Number: 25544
Epoch time: 09349
54058844 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 94
7192 deg
Eccentricity:
0007584
Arg of perigee: 83
6846 deg
Mean anomaly: 276
5182 deg
Mean motion: 15
76546966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3453
Checksum: 354
Coasting Arc #3 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2009/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3048218
01 A = 6717816
45 meter
Y = 4446827
16 meter E =
0018278
Z = 3993684
85 I = 51
97788
XDOT = -3204
954827 Wp = 95
58366
YDOT = -5781
176272 meter/sec RA = 89
03481 deg
ZDOT = 3973
764452 TA = 313
49417
MA = 313
64597
Ha = 188
865 n
mi
Hp = 177
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10000715
25 X = -3117117
37
Y = 14589327
94 feet Y = 4412354
30 meter
Z = 13102640
58 Z = 3978709
87
XDOT = -10514
943657 XDOT = -3159
374441
YDOT = -18967
113754 feet/sec YDOT = -5816
761755 meter/sec
ZDOT = 13037
284948 ZDOT = 3958
304470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13554991
56 X = -4131561
43
Y = -11431165
80 feet Y = -3484219
34 meter
Z = 13043490
24 Z = 3975655
83
XDOT = 19062
252843 XDOT = 5810
174667
YDOT = -7733
165665 feet/sec YDOT = -2357
068895 meter/sec
ZDOT = 12975
971001 ZDOT = 3955
075961
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 09350
55475479
00016717 00000-0 10270-3 0 9022
2 25544 51
6452 89
4915 0007478 87
0252 273
1768 15
76622198 34694
Satellite: ISS
Catalog Number: 25544
Epoch time: 09350
55475479 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 89
4915 deg
Eccentricity:
0007478
Arg of perigee: 87
0252 deg
Mean anomaly: 273
1768 deg
Mean motion: 15
76622198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 350
Coasting Arc #4 (Orbit 3483)
---------------------------------------
Vector Time (GMT): 2009/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2757202
48 A = 6721524
51 meter
Y = 5477885
82 meter E =
0011783
Z = -2757251
12 I = 51
98860
XDOT = -3599
385092 Wp = 76
72083
YDOT = 4409
667126 meter/sec RA = 83
85604 deg
ZDOT = 5182
486514 TA = 251
91619
MA = 252
04457
Ha = 188
822 n
mi
Hp = 177
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9045939
91 X = 2709137
13
Y = 17972066
33 feet Y = 5508450
17 meter
Z = -9046099
48 Z = -2743972
49
XDOT = -11809
006206 XDOT = -3673
602867
YDOT = 14467
411830 feet/sec YDOT = 4369
000884 meter/sec
ZDOT = 17002
908509 ZDOT = 5164
821093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18633336
15 X = -5679440
86
Y = 7653312
03 feet Y = 2332729
51 meter
Z = -8993426
03 Z = -2741196
25
XDOT = -12925
704230 XDOT = -3939
754649
YDOT = -11653
345447 feet/sec YDOT = -3551
939692 meter/sec
ZDOT = 16933
099774 ZDOT = 5161
208811
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 09351
50552362
00016717 00000-0 10270-3 0 9036
2 25544 51
6454 84
5916 0007400 88
7226 271
4786 15
76592790 34849
Satellite: ISS
Catalog Number: 25544
Epoch time: 09351
50552362 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 84
5916 deg
Eccentricity:
0007400
Arg of perigee: 88
7226 deg
Mean anomaly: 271
4786 deg
Mean motion: 15
76592790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3484
Checksum: 329
Coasting Arc #5 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2009/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3303628
47 A = 6714238
95 meter
Y = -3167657
03 meter E =
0019681
Z = -4930157
92 I = 51
95955
XDOT = 3097
782462 Wp = 80
90525
YDOT = 6679
319819 meter/sec RA = 78
76536 deg
ZDOT = -2220
162413 TA = 167
61477
MA = 167
56633
Ha = 188
760 n
mi
Hp = 177
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10838676
08 X = 3362754
00
Y = -10392575
55 feet Y = -3130382
58 meter
Z = -16175058
80 Z = -4913965
78
XDOT = 10163
328288 XDOT = 3033
648026
YDOT = 21913
778933 feet/sec YDOT = 6713
602787 meter/sec
ZDOT = -7283
997417 ZDOT = -2205
268200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9698686
71 X = 2956159
71
Y = 11553561
08 feet Y = 3521525
42 meter
Z = -16111044
52 Z = -4910646
37
XDOT = -21658
979521 XDOT = -6601
656958
YDOT = 8127
226786 feet/sec YDOT = 2477
178724 meter/sec
ZDOT = -7224
904146 ZDOT = -2202
150784
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 09352
51966014
00016717 00000-0 10270-3 0 9042
2 25544 51
6451 79
3639 0007407 93
2418 266
9594 15
76623648 35003
Satellite: ISS
Catalog Number: 25544
Epoch time: 09352
51966014 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 79
3639 deg
Eccentricity:
0007407
Arg of perigee: 93
2418 deg
Mean anomaly: 266
9594 deg
Mean motion: 15
76623648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 329
Coasting Arc #6 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2009/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2654632
96 A = 6724147
00 meter
Y = -6076656
75 meter E =
0020828
Z = 1063846
41 I = 51
98559
XDOT = 4018
794615 Wp = 113
89508
YDOT = -2811
250660 meter/sec RA = 73
60579 deg
ZDOT = -5947
187479 TA = 54
50608
MA = 54
31193
Ha = 188
778 n
mi
Hp = 176
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8709425
73 X = -2591653
37
Y = -19936537
90 feet Y = -6105990
43 meter
Z = 3490309
73 Z = 1051102
41
XDOT = 13185
021704 XDOT = 4078
822056
YDOT = -9223
263321 feet/sec YDOT = -2765
973693 meter/sec
ZDOT = -19511
769944 ZDOT = -5927
518832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20305291
23 X = 6189052
77
Y = -7833596
68 feet Y = -2387680
27 meter
Z = 3439740
29 Z = 1048432
84
XDOT = 8051
366107 XDOT = 2454
056389
YDOT = 12215
797594 feet/sec YDOT = 3723
375107 meter/sec
ZDOT = -19433
982109 ZDOT = -5923
477747
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 09353
53378075
00016717 00000-0 10270-3 0 9050
2 25544 51
6445 74
1363 0007588 96
3540 263
8489 15
76658852 35164
Satellite: ISS
Catalog Number: 25544
Epoch time: 09353
53378075 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 74
1363 deg
Eccentricity:
0007588
Arg of perigee: 96
3540 deg
Mean anomaly: 263
8489 deg
Mean motion: 15
76658852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 348
Coasting Arc #7 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2009/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3760224
85 A = 6712338
81 meter
Y = 1727942
38 meter E =
0009822
Z = 5276708
16 I = 51
93722
XDOT = -2977
209370 Wp = 99
28802
YDOT = -7112
783837 meter/sec RA = 68
48438 deg
ZDOT = 205
736359 TA = 348
75966
MA = 348
78159
Ha = 188
723 n
mi
Hp = 176
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12336695
71 X = -3804900
69
Y = 5669102
29 feet Y = 1685642
91 meter
Z = 17312034
65 Z = 5258332
77
XDOT = -9767
747277 XDOT = -2898
451124
YDOT = -23335
904978 feet/sec YDOT = -7145
636414 meter/sec
ZDOT = 674
988056 ZDOT = 191
463617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5327562
67 X = -1623841
10
Y = -12588153
78 feet Y = -3836869
27 meter
Z = 17239338
32 Z = 5254550
32
XDOT = 22676
231197 XDOT = 6911
715269
YDOT = -8741
763393 feet/sec YDOT = -2664
489482 meter/sec
ZDOT = 618
346879 ZDOT = 188
472129
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 09354
54788286
00016717 00000-0 10270-3 0 9062
2 25544 51
6449 68
9078 0007404 99
6998 260
5004 15
76725099 35325
Satellite: ISS
Catalog Number: 25544
Epoch time: 09354
54788286 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 68
9078 deg
Eccentricity:
0007404
Arg of perigee: 99
6998 deg
Mean anomaly: 260
5004 deg
Mean motion: 15
76725099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 361
Coasting Arc #8 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2009/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2481246
25 A = 6724297
75 meter
Y = 6201492
32 meter E =
0019306
Z = 719998
45 I = 51
96444
XDOT = -4679
592130 Wp = 69
63298
YDOT = 1160
159671 meter/sec RA = 63
35621 deg
ZDOT = 6011
793835 TA = 298
18749
MA = 298
38235
Ha = 188
696 n
mi
Hp = 176
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8140571
69 X = 2408218
06
Y = 20346103
40 feet Y = 6228830
68 meter
Z = 2362199
64 Z = 731875
53
XDOT = -15352
992553 XDOT = -4721
421503
YDOT = 3806
298132 feet/sec YDOT = 1107
595222 meter/sec
ZDOT = 19723
733055 ZDOT = 5988
958999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20427402
24 X = -6226272
20
Y = 7920173
43 feet Y = 2414068
86 meter
Z = 2409337
83 Z = 734366
17
XDOT = -3072
424927 XDOT = -936
475118
YDOT = -14016
421450 feet/sec YDOT = -4272
205258 meter/sec
ZDOT = 19633
370732 ZDOT = 5984
251399
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 09355
56197299
00016717 00000-0 10270-3 0 9074
2 25544 51
6444 63
6799 0007550 101
6512 258
5500 15
76691842 35483
Satellite: ISS
Catalog Number: 25544
Epoch time: 09355
56197299 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 63
6799 deg
Eccentricity:
0007550
Arg of perigee: 101
6512 deg
Mean anomaly: 258
5500 deg
Mean motion: 15
76691842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 341
Coasting Arc #9 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2009/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4450074
71 A = 6713506
65 meter
Y = -312216
47 meter E =
0020723
Z = -5035583
10 I = 51
91300
XDOT = 2606
728739 Wp = 104
14558
YDOT = 6987
790244 meter/sec RA = 58
19854 deg
ZDOT = 1871
813027 TA = 183
86218
MA = 183
87820
Ha = 188
596 n
mi
Hp = 177
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14599982
64 X = 4477697
10
Y = -1024332
27 feet Y = -262298
23 meter
Z = -16520941
92 Z = -5013897
63
XDOT = 8552
259642 XDOT = 2519
303402
YDOT = 22925
821010 feet/sec YDOT = 7016
451242 meter/sec
ZDOT = 6141
118856 ZDOT = 1884
264725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1128718
26 X = 344033
33
Y = 14688886
91 feet Y = 4477172
73 meter
Z = -16435110
83 Z = -5009421
78
XDOT = -21794
001176 XDOT = -6642
811559
YDOT = 8595
864561 feet/sec YDOT = 2620
019518 meter/sec
ZDOT = 6190
544147 ZDOT = 1886
877856
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 09356
51266506
00016717 00000-0 10270-3 0 9089
2 25544 51
6436 58
7781 0007513 104
8562 255
3436 15
76732408 35633
Satellite: ISS
Catalog Number: 25544
Epoch time: 09356
51266506 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 58
7781 deg
Eccentricity:
0007513
Arg of perigee: 104
8562 deg
Mean anomaly: 255
3436 deg
Mean motion: 15
76732408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 326
Coasting Arc #10 (Orbit 3578)
---------------------------------------
Vector Time (GMT): 2009/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1980627
10 A = 6721538
70 meter
Y = -5912654
17 meter E =
0012662
Z = -2509911
54 I = 51
92387
XDOT = 5533
543792 Wp = 116
77350
YDOT = 402
136213 meter/sec RA = 53
09870 deg
ZDOT = -5340
067242 TA = 91
54326
MA = 91
39821
Ha = 188
564 n
mi
Hp = 176
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6498120
39 X = -1902170
86
Y = -19398471
70 feet Y = -5934363
85 meter
Z = -8234617
92 Z = -2519343
31
XDOT = 18154
671232 XDOT = 5554
576842
YDOT = 1319
344532 feet/sec YDOT = 464
133580 meter/sec
ZDOT = -17519
905648 ZDOT = -5313
134169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19236378
64 X = 5863248
21
Y = -6918807
62 feet Y = -2108852
56 meter
Z = -8272064
02 Z = -2521325
11
XDOT = -1379
833486 XDOT = -420
573247
YDOT = 16880
888895 feet/sec YDOT = 5145
294935 meter/sec
ZDOT = -17413
289353 ZDOT = -5307
570595
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 09357
52672292
00016717 00000-0 10270-3 0 9095
2 25544 51
6438 53
5491 0007636 108
3287 251
8708 15
76765540 35798
Satellite: ISS
Catalog Number: 25544
Epoch time: 09357
52672292 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 53
5491 deg
Eccentricity:
0007636
Arg of perigee: 108
3287 deg
Mean anomaly: 251
8708 deg
Mean motion: 15
76765540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 347
Coasting Arc #11 (Orbit 3594)
---------------------------------------
Vector Time (GMT): 2009/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5202066
01 A = 6716797
22 meter
Y = -923364
58 meter E =
0017114
Z = 4132813
76 I = 51
88941
XDOT = -1857
374937 Wp = 90
11108
YDOT = -6468
524933 meter/sec RA = 47
91394 deg
ZDOT = -3769
859682 TA = 38
34790
MA = 38
22635
Ha = 188
525 n
mi
Hp = 176
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17067145
70 X = -5211430
68
Y = -3029411
35 feet Y = -981589
82 meter
Z = 13559100
27 Z = 4107519
23
XDOT = -6093
749793 XDOT = -1766
591356
YDOT = -21222
194662 feet/sec YDOT = -6488
787322 meter/sec
ZDOT = -12368
306044 ZDOT = -3778
662800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2315426
97 X = 705742
14
Y = -17257147
55 feet Y = -5259978
57 meter
Z = 13458961
77 Z = 4102291
55
XDOT = 19696
137934 XDOT = 6003
382842
YDOT = -7064
940014 feet/sec YDOT = -2153
393716 meter/sec
ZDOT = -12403
268017 ZDOT = -3780
516091
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 09358
54076321
00016717 00000-0 10270-3 0 9101
2 25544 51
6441 48
3205 0007445 111
4580 248
7380 15
76821172 35959
Satellite: ISS
Catalog Number: 25544
Epoch time: 09358
54076321 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 48
3205 deg
Eccentricity:
0007445
Arg of perigee: 111
4580 deg
Mean anomaly: 248
7380 deg
Mean motion: 15
76821172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 304
Coasting Arc #12 (Orbit 3610)
---------------------------------------
Vector Time (GMT): 2009/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1152245
45 A = 6717324
13 meter
Y = 5298846
45 meter E =
0018562
Z = 3953203
71 I = 51
86995
XDOT = -6382
040427 Wp = 106
39992
YDOT = -1620
946314 meter/sec RA = 42
82554 deg
ZDOT = 4012
324264 TA = 302
09503
MA = 302
27509
Ha = 188
461 n
mi
Hp = 176
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3780332
85 X = 1073703
11
Y = 17384666
84 feet Y = 5311292
08 meter
Z = 12969828
44 Z = 3958610
99
XDOT = -20938
452845 XDOT = -6382
931663
YDOT = -5318
065336 feet/sec YDOT = -1692
319358 meter/sec
ZDOT = 13163
793517 ZDOT = 3981
317815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17137806
56 X = -5223603
44
Y = 4717537
67 feet Y = 1437905
48 meter
Z = 12991321
41 Z = 3959754
76
XDOT = 4420
058040 XDOT = 1347
233691
YDOT = -20041
211315 feet/sec YDOT = -6108
561209 meter/sec
ZDOT = 13041
036549 ZDOT = 3974
907940
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 09359
55479059
00016717 00000-0 10270-3 0 9119
2 25544 51
6439 43
0917 0007680 114
8033 245
3931 15
76816375 36112
Satellite: ISS
Catalog Number: 25544
Epoch time: 09359
55479059 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 43
0917 deg
Eccentricity:
0007680
Arg of perigee: 114
8033 deg
Mean anomaly: 245
3931 deg
Mean motion: 15
76816375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3611
Checksum: 325
Coasting Arc #13 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2009/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5870322
10 A = 6720862
17 meter
Y = 1818172
05 meter E =
0010914
Z = -2731462
24 I = 51
85992
XDOT = 655
937413 Wp = 94
49771
YDOT = 5648
397419 meter/sec RA = 37
63579 deg
ZDOT = 5186
339181 TA = 234
41056
MA = 234
51232
Ha = 188
403 n
mi
Hp = 176
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19259586
95 X = 5862823
75
Y = 5965131
39 feet Y = 1883775
78 meter
Z = -8961490
29 Z = -2702962
00
XDOT = 2152
025633 XDOT = 567
532764
YDOT = 18531
487596 feet/sec YDOT = 5655
237729 meter/sec
ZDOT = 17015
548494 ZDOT = 5189
311533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4483664
02 X = -1366620
79
Y = 19708396
21 feet Y = 6007119
16 meter
Z = -8848653
35 Z = -2697069
54
XDOT = -16885
828792 XDOT = -5146
800616
YDOT = 3778
308596 feet/sec YDOT = 1151
628460 meter/sec
ZDOT = 17027
401705 ZDOT = 5189
952040
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 09360
50542677
00016717 00000-0 10270-3 0 9124
2 25544 51
6446 38
1897 0007725 117
9882 242
2065 15
76863156 36267
Satellite: ISS
Catalog Number: 25544
Epoch time: 09360
50542677 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 38
1897 deg
Eccentricity:
0007725
Arg of perigee: 117
9882 deg
Mean anomaly: 242
2065 deg
Mean motion: 15
76863156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 335
Coasting Arc #14 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2009/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 118470
03 A = 6713416
37 meter
Y = -4546627
84 meter E =
0018914
Z = -4954028
80 I = 51
81083
XDOT = 6969
820202 Wp = 91
47581
YDOT = 2475
055397 meter/sec RA = 32
53229 deg
ZDOT = -2112
215258 TA = 158
11541
MA = 158
03451
Ha = 188
354 n
mi
Hp = 176
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 388681
19 X = 193368
43
Y = -14916758
02 feet Y = -4544883
71 meter
Z = -16253375
33 Z = -4953271
85
XDOT = 22866
864181 XDOT = 6951
886545
YDOT = 8120
260489 feet/sec YDOT = 2552
896009 meter/sec
ZDOT = -6929
840086 ZDOT = -2078
398808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14897562
86 X = 4540777
16
Y = -904798
21 feet Y = -275782
49 meter
Z = -16250443
48 Z = -4953135
17
XDOT = -6021
619608 XDOT = -1835
389657
YDOT = 22476
338139 feet/sec YDOT = 6850
787865 meter/sec
ZDOT = -6795
953500 ZDOT = -2071
406627
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 09361
51942361
00016717 00000-0 10270-3 0 9131
2 25544 51
6453 32
9605 0007653 121
5994 238
5918 15
76846322 36428
Satellite: ISS
Catalog Number: 25544
Epoch time: 09361
51942361 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 32
9605 deg
Eccentricity:
0007653
Arg of perigee: 121
5994 deg
Mean anomaly: 238
5918 deg
Mean motion: 15
76846322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 323
Coasting Arc #15 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2009/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 736597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6199873
75 A = 6723656
17 meter
Y = -2414419
24 meter E =
0021300
Z = 896793
12 I = 51
81873
XDOT = 984
373859 Wp = 124
86995
YDOT = -4778
237283 meter/sec RA = 27
36198 deg
ZDOT = -5971
667257 TA = 45
34600
MA = 45
17256
Ha = 188
285 n
mi
Hp = 176
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20340793
15 X = -6176771
00
Y = -7921322
96 feet Y = -2483620
84 meter
Z = 2942234
65 Z = 866729
64
XDOT = 3229
573028 XDOT = 1066
741324
YDOT = -15676
631506 feet/sec YDOT = -4766
768067 meter/sec
ZDOT = -19592
084178 ZDOT = -5966
685713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5632422
46 X = 1716762
37
Y = -21105859
37 feet Y = -6433065
93 meter
Z = 2823204
88 Z = 860512
85
XDOT = 14410
911865 XDOT = 4392
445937
YDOT = 1187
741195 feet/sec YDOT = 362
023516 meter/sec
ZDOT = -19572
426434 ZDOT = -5965
675577
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 09362
53340481
00016717 00000-0 10270-3 0 9140
2 25544 51
6445 27
7314 0007687 124
3066 235
8827 15
76887487 36589
Satellite: ISS
Catalog Number: 25544
Epoch time: 09362
53340481 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 27
7314 deg
Eccentricity:
0007687
Arg of perigee: 124
3066 deg
Mean anomaly: 235
8827 deg
Mean motion: 15
76887487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 343
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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