Date:
April 15th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3577)
---------------------------------------
Vector Time (GMT): 2009/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3850409
08 A = 6729956
79 meter
Y = -3650863
70 meter E =
0008385
Z = 4143044
27 I = 51
30425
XDOT = 2103
010249 Wp = 162
87401
YDOT = 6415
598841 meter/sec RA = 277
80839 deg
ZDOT = 3689
176671 TA = 249
17432
MA = 249
26415
Ha = 192
789 n
mi
Hp = 188
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12632575
71 X = 3870821
07
Y = -11977899
29 feet Y = -3607692
11 meter
Z = 13592664
93 Z = 4161799
31
XDOT = 6899
639924 XDOT = 2013
192076
YDOT = 21048
552629 feet/sec YDOT = 6438
613676 meter/sec
ZDOT = 12103
598001 ZDOT = 3699
175138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7415002
61 X = 2260092
80
Y = -15686950
72 feet Y = -4781382
58 meter
Z = 13665646
48 Z = 4165289
05
XDOT = 12788
836368 XDOT = 3898
037325
YDOT = 16651
377595 feet/sec YDOT = 5075
339891 meter/sec
ZDOT = 12143
078432 ZDOT = 3701
210306
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 09103
55435772
00010596 00000-0 82463-4 0 9001
2 25544 51
6377 278
2280 0009166 234
8722 125
1582 15
72139484 35781
Satellite: ISS
Catalog Number: 25544
Epoch time: 09103
55435772 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 278
2280 deg
Eccentricity:
0009166
Arg of perigee: 234
8722 deg
Mean anomaly: 125
1582 deg
Mean motion: 15
72139484 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3578
Checksum: 322
Coasting Arc #2 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2009/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2717127
16 A = 6731555
57 meter
Y = -4948276
18 meter E =
0006295
Z = -3670425
99 I = 51
30760
XDOT = 3681
449991 Wp = 198
10719
YDOT = -5213
277808 meter/sec RA = 272
61150 deg
ZDOT = 4295
104344 TA = 117
59532
MA = 117
53138
Ha = 192
613 n
mi
Hp = 188
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8914459
17 X = -2643762
33
Y = -16234501
90 feet Y = -4978250
38 meter
Z = -12042080
02 Z = -3683447
83
XDOT = 12078
248001 XDOT = 3718
607096
YDOT = -17103
929815 feet/sec YDOT = -5171
902037 meter/sec
ZDOT = 14091
549686 ZDOT = 4313
079114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14288599
99 X = -4355165
28
Y = -11731455
77 feet Y = -3575747
72 meter
Z = -12093270
09 Z = -3686028
72
XDOT = 3849
247427 XDOT = 1173
250616
YDOT = -19312
940606 feet/sec YDOT = -5886
584297 meter/sec
ZDOT = 14161
379617 ZDOT = 4316
388507
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 09104
50783041
00010596 00000-0 82463-4 0 9013
2 25544 51
6383 273
3443 0009018 237
5316 122
4975 15
72150060 35936
Satellite: ISS
Catalog Number: 25544
Epoch time: 09104
50783041 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 273
3443 deg
Eccentricity:
0009018
Arg of perigee: 237
5316 deg
Mean anomaly: 122
4975 deg
Mean motion: 15
72150060 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3593
Checksum: 289
Coasting Arc #3 (Orbit 3608)
---------------------------------------
Vector Time (GMT): 2009/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2437443
21 A = 6732480
14 meter
Y = 5316036
75 meter E =
0005289
Z = -3328225
33 I = 51
31126
XDOT = -3930
640101 Wp = 215
54188
YDOT = -4712
391299 meter/sec RA = 267
51836 deg
ZDOT = -4648
825391 TA = 3
77966
MA = 3
77566
Ha = 192
219 n
mi
Hp = 189
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7996860
93 X = -2480538
86
Y = 17441065
44 feet Y = 5288538
96 meter
Z = -10919374
44 Z = -3340171
04
XDOT = -12895
800856 XDOT = -3855
069936
YDOT = -15460
601376 feet/sec YDOT = -4755
923352 meter/sec
ZDOT = -15252
051809 ZDOT = -4667
737111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -482538
62 X = -147077
77
Y = 19154500
10 feet Y = 5838291
63 meter
Z = -10965654
06 Z = -3342331
36
XDOT = -16436
162647 XDOT = -5009
742375
YDOT = -9187
074683 feet/sec YDOT = -2800
220363 meter/sec
ZDOT = -15326
233090 ZDOT = -4671
435846
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 09105
52485090
00010596 00000-0 82463-4 0 9020
2 25544 51
6385 268
1360 0008887 242
3239 117
7022 15
72190276 36090
Satellite: ISS
Catalog Number: 25544
Epoch time: 09105
52485090 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 268
1360 deg
Eccentricity:
0008887
Arg of perigee: 242
3239 deg
Mean anomaly: 117
7022 deg
Mean motion: 15
72190276 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3609
Checksum: 310
Coasting Arc #4 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2009/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3986112
57 A = 6728876
51 meter
Y = 3160327
71 meter E =
0000588
Z = 4404062
31 I = 51
30084
XDOT = -1735
170857 Wp = 132
68303
YDOT = 6747
576442 meter/sec RA = 262
32319 deg
ZDOT = -3271
633728 TA = 350
31587
MA = 350
31701
Ha = 192
079 n
mi
Hp = 189
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13077797
16 X = 3929082
80
Y = 10368529
25 feet Y = 3204583
79 meter
Z = 14449023
31 Z = 4423288
43
XDOT = -5692
817772 XDOT = -1794
601374
YDOT = 22137
717984 feet/sec YDOT = 6727
840522 meter/sec
ZDOT = -10733
706458 ZDOT = -3280
207434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16088091
60 X = 4903650
32
Y = 4186469
02 feet Y = 1276035
76 meter
Z = 14524332
61 Z = 4427016
58
XDOT = 4166
575487 XDOT = 1269
972208
YDOT = 21340
555179 feet/sec YDOT = 6504
601219 meter/sec
ZDOT = -10766
714036 ZDOT = -3281
694438
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 09106
54185618
00010596 00000-0 82463-4 0 9037
2 25544 51
6378 262
9266 0008963 245
5807 114
4420 15
72171803 36259
Satellite: ISS
Catalog Number: 25544
Epoch time: 09106
54185618 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 262
9266 deg
Eccentricity:
0008963
Arg of perigee: 245
5807 deg
Mean anomaly: 114
4420 deg
Mean motion: 15
72171803 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3625
Checksum: 316
Coasting Arc #5 (Orbit 3640)
---------------------------------------
Vector Time (GMT): 2009/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 521143
92 A = 6734733
08 meter
Y = -6280143
23 meter E =
0004992
Z = 2370404
26 I = 51
32735
XDOT = 4952
932888 Wp = 81
74789
YDOT = 2438
000937 meter/sec RA = 257
22245 deg
ZDOT = 5361
379550 TA = 305
05664
MA = 305
10345
Ha = 191
880 n
mi
Hp = 189
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1709789
78 X = 579815
80
Y = -20604144
46 feet Y = -6273987
47 meter
Z = 7776916
88 Z = 2373078
44
XDOT = 16249
779817 XDOT = 4899
257996
YDOT = 7998
690738 feet/sec YDOT = 2493
087361 meter/sec
ZDOT = 17589
827921 ZDOT = 5385
310571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7194813
11 X = -2192979
04
Y = -19378680
87 feet Y = -5906621
93 meter
Z = 7786910
71 Z = 2373450
38
XDOT = 16602
083071 XDOT = 5060
314920
YDOT = 953
550853 feet/sec YDOT = 290
642300 meter/sec
ZDOT = 17683
469791 ZDOT = 5389
921592
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 09107
55884272
00010596 00000-0 82463-4 0 9042
2 25544 51
6388 257
7173 0009012 249
5134 110
5061 15
72244940 36411
Satellite: ISS
Catalog Number: 25544
Epoch time: 09107
55884272 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 257
7173 deg
Eccentricity:
0009012
Arg of perigee: 249
5134 deg
Mean anomaly: 110
5061 deg
Mean motion: 15
72244940 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3641
Checksum: 303
Coasting Arc #6 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2009/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4478156
74 A = 6726582
73 meter
Y = -1057632
11 meter E =
0006975
Z = -4911659
40 I = 51
30820
XDOT = -597
699976 Wp = 148
44221
YDOT = -7369
489470 meter/sec RA = 252
04013 deg
ZDOT = 2127
330042 TA = 142
33015
MA = 142
28129
Ha = 191
562 n
mi
Hp = 189
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14692115
28 X = -4442137
32
Y = -3469921
62 feet Y = -1107508
10 meter
Z = -16114368
10 Z = -4933326
80
XDOT = -1960
957926 XDOT = -525
582877
YDOT = -24178
115059 feet/sec YDOT = -7375
770061 meter/sec
ZDOT = 6979
429273 ZDOT = 2124
601623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14643855
77 X = -4463447
24
Y = 3273969
78 feet Y = 997905
99 meter
Z = -16199076
42 Z = -4937478
49
XDOT = -12149
381875 XDOT = -3703
131595
YDOT = -19791
614997 feet/sec YDOT = -6032
484251 meter/sec
ZDOT = 6968
233990 ZDOT = 2123
917720
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 09108
51225470
00010596 00000-0 82463-4 0 9059
2 25544 51
6391 252
8347 0008904 253
6448 106
3735 15
72251775 36568
Satellite: ISS
Catalog Number: 25544
Epoch time: 09108
51225470 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 252
8347 deg
Eccentricity:
0008904
Arg of perigee: 253
6448 deg
Mean anomaly: 106
3735 deg
Mean motion: 15
72251775 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3656
Checksum: 317
Coasting Arc #7 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2009/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1567602
88 A = 6736287
46 meter
Y = 6406890
44 meter E =
0009444
Z = -1336698
50 I = 51
35116
XDOT = -5046
184497 Wp = 200
85513
YDOT = 20
563843 meter/sec RA = 246
92471 deg
ZDOT = -5815
409431 TA = 353
87802
MA = 353
88956
Ha = 191
277 n
mi
Hp = 190
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5143054
08 X = 1502336
90
Y = 21019981
76 feet Y = 6424055
34 meter
Z = -4385493
76 Z = -1329241
73
XDOT = -16555
723414 XDOT = -5017
789149
YDOT = 67
466678 feet/sec YDOT = -35
706885 meter/sec
ZDOT = -19079
427268 ZDOT = -5839
854859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14136223
63 X = 4308720
96
Y = 16392577
38 feet Y = 4996457
58 meter
Z = -4355890
56 Z = -1327675
44
XDOT = -13432
086969 XDOT = -4094
100108
YDOT = 6484
583823 feet/sec YDOT = 1976
501149 meter/sec
ZDOT = -19174
912379 ZDOT = -5844
513293
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 09109
52921011
00010596 00000-0 82463-4 0 9066
2 25544 51
6388 247
6245 0008891 258
5398 101
4766 15
72288390 36727
Satellite: ISS
Catalog Number: 25544
Epoch time: 09109
52921011 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 247
6245 deg
Eccentricity:
0008891
Arg of perigee: 258
5398 deg
Mean anomaly: 101
4766 deg
Mean motion: 15
72288390 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3672
Checksum: 333
Coasting Arc #8 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2009/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4148229
77 A = 6725272
42 meter
Y = -1058349
07 meter E =
0005873
Z = 5191769
21 I = 51
32777
XDOT = 2948
943686 Wp = 276
42129
YDOT = 7046
769739 meter/sec RA = 241
76042 deg
ZDOT = -919
960138 TA = 182
38662
MA = 182
38942
Ha = 190
959 n
mi
Hp = 190
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13609677
74 X = 4134535
33
Y = -3472273
84 feet Y = -1012037
54 meter
Z = 17033363
53 Z = 5211888
16
XDOT = 9675
012094 XDOT = 2874
395370
YDOT = 23119
323292 feet/sec YDOT = 7079
329696 meter/sec
ZDOT = -3018
241924 ZDOT = -905
815428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10308403
24 X = 3142001
31
Y = -9398727
50 feet Y = -2864732
14 meter
Z = 17111873
98 Z = 5215699
19
XDOT = 18711
015408 XDOT = 5703
117496
YDOT = 15129
829196 feet/sec YDOT = 4611
571939 meter/sec
ZDOT = -2962
456765 ZDOT = -902
956822
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 09110
54615058
00010596 00000-0 82463-4 0 9072
2 25544 51
6397 242
4153 0008824 262
7876 97
2283 15
72281091 36886
Satellite: ISS
Catalog Number: 25544
Epoch time: 09110
54615058 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 242
4153 deg
Eccentricity:
0008824
Arg of perigee: 262
7876 deg
Mean anomaly: 97
2283 deg
Mean motion: 15
72281091 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3688
Checksum: 328
Coasting Arc #9 (Orbit 3703)
---------------------------------------
Vector Time (GMT): 2009/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514584
97 A = 6736924
28 meter
Y = -5734556
36 meter E =
0008078
Z = 274638
93 I = 51
38343
XDOT = 4228
009267 Wp = 4
27369
YDOT = -2303
419772 meter/sec RA = 236
62768 deg
ZDOT = 6006
696162 TA = 358
71948
MA = 358
72154
Ha = 190
705 n
mi
Hp = 190
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11530790
59 X = -3451533
14
Y = -18814161
28 feet Y = -5773505
95 meter
Z = 901046
36 Z = 257718
34
XDOT = 13871
421480 XDOT = 4224
272579
YDOT = -7557
151482 feet/sec YDOT = -2256
160344 meter/sec
ZDOT = 19707
008407 ZDOT = 6027
227014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19197534
25 X = -5851408
44
Y = -10885860
25 feet Y = -3318010
21 meter
Z = 834509
37 Z = 254358
46
XDOT = 7590
894839 XDOT = 2313
704747
YDOT = -11868
968884 feet/sec YDOT = -3617
661716 meter/sec
ZDOT = 19787
034587 ZDOT = 6031
088142
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 09111
56307248
00010596 00000-0 82463-4 0 9085
2 25544 51
6407 237
2057 0008857 267
0435 92
9714 15
72323898 37040
Satellite: ISS
Catalog Number: 25544
Epoch time: 09111
56307248 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 237
2057 deg
Eccentricity:
0008857
Arg of perigee: 267
0435 deg
Mean anomaly: 92
9714 deg
Mean motion: 15
72323898 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3704
Checksum: 325
Coasting Arc #10 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2009/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3082884
90 A = 6724793
88 meter
Y = 2865875
16 meter E =
0006155
Z = -5249848
11 I = 51
36058
XDOT = -4965
755607 Wp = 82
23636
YDOT = -5870
180362 meter/sec RA = 231
48661 deg
ZDOT = -287
925281 TA = 185
01453
MA = 185
02070
Ha = 190
561 n
mi
Hp = 190
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10114451
78 X = -3089199
33
Y = 9402477
55 feet Y = 2831365
01 meter
Z = -17223911
11 Z = -5264840
41
XDOT = -16291
849103 XDOT = -4898
346488
YDOT = -19259
121922 feet/sec YDOT = -5925
333448 meter/sec
ZDOT = -944
636750 ZDOT = -311
885245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3991016
84 X = -1216461
93
Y = 13144091
53 feet Y = 4006319
10 meter
Z = -17282258
97 Z = -5267632
53
XDOT = -22762
741807 XDOT = -6938
083703
YDOT = -8279
566435 feet/sec YDOT = -2523
611849 meter/sec
ZDOT = -1038
689059 ZDOT = -316
592425
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 09112
51642251
00010596 00000-0 82463-4 0 9098
2 25544 51
6409 232
3228 0008887 271
4490 88
5654 15
72365068 37196
Satellite: ISS
Catalog Number: 25544
Epoch time: 09112
51642251 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 232
3228 deg
Eccentricity:
0008887
Arg of perigee: 271
4490 deg
Mean anomaly: 88
5654 deg
Mean motion: 15
72365068 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3719
Checksum: 324
Coasting Arc #11 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2009/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5041161
45 A = 6736546
24 meter
Y = 4394285
64 meter E =
0007537
Z = 768153
37 I = 51
42000
XDOT = -2659
116740 Wp = 165
08918
YDOT = 4092
241437 meter/sec RA = 226
33536 deg
ZDOT = -5953
253129 TA = 6
51715
MA = 6
50736
Ha = 190
791 n
mi
Hp = 190
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16539243
61 X = 4987917
52
Y = 14416947
65 feet Y = 4450361
18 meter
Z = 2520188
21 Z = 792514
30
XDOT = -8724
136287 XDOT = -2675
758884
YDOT = 13425
988967 feet/sec YDOT = 4062
412402 meter/sec
ZDOT = -19531
670372 ZDOT = -5966
211907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21582819
81 X = 6578443
48
Y = 3884111
63 feet Y = 1183877
23 meter
Z = 2615697
45 Z = 797264
58
XDOT = -210
370333 XDOT = -64
120877
YDOT = 14368
434361 feet/sec YDOT = 4379
498793 meter/sec
ZDOT = -19581
981371 ZDOT = -5968
587922
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 09113
53331416
00010596 00000-0 82463-4 0 9101
2 25544 51
6412 227
1130 0008899 275
0695 84
9451 15
72368831 37358
Satellite: ISS
Catalog Number: 25544
Epoch time: 09113
53331416 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 227
1130 deg
Eccentricity:
0008899
Arg of perigee: 275
0695 deg
Mean anomaly: 84
9451 deg
Mean motion: 15
72368831 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3735
Checksum: 309
Coasting Arc #12 (Orbit 3750)
---------------------------------------
Vector Time (GMT): 2009/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1463931
70 A = 6725302
02 meter
Y = -4133190
62 meter E =
0005170
Z = 5103930
36 I = 51
40486
XDOT = 6379
915455 Wp = 256
54419
YDOT = 4049
970807 meter/sec RA = 221
21572 deg
ZDOT = 1449
818335 TA = 179
50596
MA = 179
50545
Ha = 190
907 n
mi
Hp = 189
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4802925
53 X = 1485246
40
Y = -13560336
69 feet Y = -4116700
86 meter
Z = 16745178
33 Z = 5111094
11
XDOT = 20931
481153 XDOT = 6327
110715
YDOT = 13287
305796 feet/sec YDOT = 4121
019513 meter/sec
ZDOT = 4756
621835 ZDOT = 1480
684348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3167390
13 X = -965420
51
Y = -13999677
66 feet Y = -4267101
75 meter
Z = 16772849
71 Z = 5112364
59
XDOT = 23747
193704 XDOT = 7238
144641
YDOT = 470
785471 feet/sec YDOT = 143
495412 meter/sec
ZDOT = 4877
522841 ZDOT = 1486
668962
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 09114
55018810
00010596 00000-0 82463-4 0 9115
2 25544 51
6421 221
9032 0008950 279
7808 80
2344 15
72432146 37515
Satellite: ISS
Catalog Number: 25544
Epoch time: 09114
55018810 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 221
9032 deg
Eccentricity:
0008950
Arg of perigee: 279
7808 deg
Mean anomaly: 80
2344 deg
Mean motion: 15
72432146 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3751
Checksum: 290
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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