Date:
May 28th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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 238)
---------------------------------------
Vector Time (GMT): 2009/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1183241
88 A = 6732589
38 meter
Y = 6204093
42 meter E =
0022796
Z = 2294668
80 I = 51
94968
XDOT = -5339
901201 Wp = 59
64723
YDOT = -1014
164337 meter/sec RA = 62
68123 deg
ZDOT = 5466
819605 TA = 326
05139
MA = 326
19706
Ha = 194
701 n
mi
Hp = 182
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3882027
17 X = 1102631
47
Y = 20354637
19 feet Y = 6216873
97 meter
Z = 7528440
95 Z = 2300222
44
XDOT = -17519
360895 XDOT = -5354
720974
YDOT = -3327
310817 feet/sec YDOT = -1073
962117 meter/sec
ZDOT = 17935
759858 ZDOT = 5440
841790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19821079
04 X = 6041464
89
Y = 6014461
24 feet Y = 1833207
79 meter
Z = 7550489
73 Z = 2301389
27
XDOT = -10664
373592 XDOT = -3250
501071
YDOT = 12638
824960 feet/sec YDOT = 3852
313848 meter/sec
ZDOT = 17833
960879 ZDOT = 5435
791276
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 09145
55896977
00010596 00000-0 82463-4 0 9005
2 25544 51
6417 62
9997 0009680 41
3196 318
8698 15
73048772 2396
Satellite: ISS
Catalog Number: 25544
Epoch time: 09145
55896977 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 62
9997 deg
Eccentricity:
0009680
Arg of perigee: 41
3196 deg
Mean anomaly: 318
8698 deg
Mean motion: 15
73048772 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 239
Checksum: 361
Coasting Arc #2 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2009/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4624045
82 A = 6724503
18 meter
Y = 119409
62 meter E =
0018710
Z = -4895396
92 I = 51
90867
XDOT = 2271
012545 Wp = 79
61298
YDOT = 6965
858025 meter/sec RA = 57
53467 deg
ZDOT = 2325
818984 TA = 212
93760
MA = 213
05431
Ha = 194
694 n
mi
Hp = 182
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15170754
00 X = 4646148
02
Y = 391763
85 feet Y = 171242
92 meter
Z = -16061013
53 Z = -4872879
42
XDOT = 7450
828561 XDOT = 2181
651865
YDOT = 22853
864910 feet/sec YDOT = 6990
753722 meter/sec
ZDOT = 7630
639710 ZDOT = 2336
635932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7178158
56 X = 2187902
73
Y = -13476090
05 feet Y = -4107512
25 meter
Z = -15972803
39 Z = -4868510
47
XDOT = 22770
304890 XDOT = 6940
388930
YDOT = 3075
965549 feet/sec YDOT = 937
554299 meter/sec
ZDOT = 7673
335075 ZDOT = 2338
832531
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 09146
51187304
00010596 00000-0 82463-4 0 9010
2 25544 51
6423 58
1130 0009624 44
5962 315
5974 15
73088705 2541
Satellite: ISS
Catalog Number: 25544
Epoch time: 09146
51187304 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 58
1130 deg
Eccentricity:
0009624
Arg of perigee: 44
5962 deg
Mean anomaly: 315
5974 deg
Mean motion: 15
73088705 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 254
Checksum: 301
Coasting Arc #3 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2009/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2746808
63 A = 6733295
09 meter
Y = -5883010
39 meter E =
0011663
Z = -1795298
05 I = 51
92190
XDOT = 5121
950507 Wp = 87
15597
YDOT = -661
957554 meter/sec RA = 52
46000 deg
ZDOT = -5698
500463 TA = 112
63367
MA = 112
51028
Ha = 194
641 n
mi
Hp = 182
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9011839
32 X = -2672098
42
Y = -19301215
18 feet Y = -5913308
75 meter
Z = -5890085
47 Z = -1808461
67
XDOT = 16804
299565 XDOT = 5156
654277
YDOT = -2171
776751 feet/sec YDOT = -604
485841 meter/sec
ZDOT = -18695
867662 ZDOT = -5673
533808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21285669
57 X = -6487872
08
Y = -238936
31 feet Y = -72827
79 meter
Z = -5941922
48 Z = -1811097
97
XDOT = 5327
801912 XDOT = 1623
914023
YDOT = -14639
677383 feet/sec YDOT = -4462
173666 meter/sec
ZDOT = -18598
092107 ZDOT = -5668
698474
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 09147
52828463
00010596 00000-0 82463-4 0 9021
2 25544 51
6426 52
9000 0009491 48
4804 311
7172 15
73103996 2708
Satellite: ISS
Catalog Number: 25544
Epoch time: 09147
52828463 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 52
9000 deg
Eccentricity:
0009491
Arg of perigee: 48
4804 deg
Mean anomaly: 311
7172 deg
Mean motion: 15
73103996 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 270
Checksum: 299
Coasting Arc #4 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2009/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4238671
48 A = 6723444
60 meter
Y = 1259209
33 meter E =
0014855
Z = 5057181
95 I = 51
86994
XDOT = -3991
520430 Wp = 52
13846
YDOT = -6355
327299 meter/sec RA = 47
31813 deg
ZDOT = -1750
646054 TA = 54
71688
MA = 54
57801
Ha = 194
675 n
mi
Hp = 182
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13906402
48 X = -4277003
96
Y = 4131264
20 feet Y = 1211594
90 meter
Z = 16591804
29 Z = 5036497
61
XDOT = -13095
539467 XDOT = -3911
653124
YDOT = -20850
811350 feet/sec YDOT = -6399
515970 meter/sec
ZDOT = -5743
589417 ZDOT = -1769
843840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2072855
60 X = -631806
39
Y = 14451269
95 feet Y = 4404747
08 meter
Z = 16510827
05 Z = 5032500
09
XDOT = -23342
163567 XDOT = -7114
691455
YDOT = 3346
982978 feet/sec YDOT = 1020
160412 meter/sec
ZDOT = -5819
088783 ZDOT = -1773
658261
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 09148
54467477
00010596 00000-0 82463-4 0 9039
2 25544 51
6422 47
6871 0009495 51
2221 308
9789 15
73190921 2863
Satellite: ISS
Catalog Number: 25544
Epoch time: 09148
54467477 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 47
6871 deg
Eccentricity:
0009495
Arg of perigee: 51
2221 deg
Mean anomaly: 308
9789 deg
Mean motion: 15
73190921 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 286
Checksum: 332
Coasting Arc #5 (Orbit 301)
---------------------------------------
Vector Time (GMT): 2009/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4172198
99 A = 6733840
85 meter
Y = 5118895
25 meter E =
0023486
Z = 1256672
67 I = 51
88414
XDOT = -4469
424697 Wp = 57
06899
YDOT = 2181
185865 meter/sec RA = 42
23185 deg
ZDOT = 5887
550786 TA = 316
67633
MA = 316
86075
Ha = 194
650 n
mi
Hp = 181
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13688316
88 X = 4108543
88
Y = 16794275
77 feet Y = 5165195
14 meter
Z = 4122941
84 Z = 1276787
23
XDOT = -14663
466854 XDOT = -4522
083482
YDOT = 7156
121605 feet/sec YDOT = 2130
910933 meter/sec
ZDOT = 19316
111504 ZDOT = 5865
710762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20861795
44 X = 6358675
25
Y = -5791824
98 feet Y = -1765348
25 meter
Z = 4201978
28 Z = 1280762
98
XDOT = 215
632981 XDOT = 65
724933
YDOT = 14883
451068 feet/sec YDOT = 4536
475886 meter/sec
ZDOT = 19230
645738 ZDOT = 5861
500821
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 09149
56104824
00010596 00000-0 82463-4 0 9047
2 25544 51
6426 42
4738 0009555 55
0923 305
1136 15
73168613 3027
Satellite: ISS
Catalog Number: 25544
Epoch time: 09149
56104824 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 42
4738 deg
Eccentricity:
0009555
Arg of perigee: 55
0923 deg
Mean anomaly: 305
1136 deg
Mean motion: 15
73168613 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 302
Checksum: 294
Coasting Arc #6 (Orbit 316)
---------------------------------------
Vector Time (GMT): 2009/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3501438
89 A = 6722799
67 meter
Y = -2474525
44 meter E =
0022291
Z = -5196549
68 I = 51
82487
XDOT = 5457
904268 Wp = 82
81042
YDOT = 5280
409212 meter/sec RA = 37
09530 deg
ZDOT = 1170
075702 TA = 198
31860
MA = 198
39901
Ha = 194
566 n
mi
Hp = 181
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11487660
42 X = 3554093
09
Y = -8118521
78 feet Y = -2435075
32 meter
Z = -17049047
51 Z = -5179412
08
XDOT = 17906
510066 XDOT = 5392
768185
YDOT = 17324
177206 feet/sec YDOT = 5341
078360 meter/sec
ZDOT = 3838
831044 ZDOT = 1196
432550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3035384
84 X = -925185
30
Y = -13818258
83 feet Y = -4211805
29 meter
Z = -16982017
57 Z = -5176118
95
XDOT = 21864
256733 XDOT = 6664
225452
YDOT = -9619
441884 feet/sec YDOT = -2932
005886 meter/sec
ZDOT = 3942
330175 ZDOT = 1201
622237
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 09150
51387804
00010596 00000-0 82463-4 0 9056
2 25544 51
6430 37
5862 0009423 58
3901 301
8180 15
73222070 3177
Satellite: ISS
Catalog Number: 25544
Epoch time: 09150
51387804 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 37
5862 deg
Eccentricity:
0009423
Arg of perigee: 58
3901 deg
Mean anomaly: 301
8180 deg
Mean motion: 15
73222070 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 317
Checksum: 283
Coasting Arc #7 (Orbit 332)
---------------------------------------
Vector Time (GMT): 2009/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5305488
15 A = 6734126
20 meter
Y = -4065830
69 meter E =
0015186
Z = -810471
25 I = 51
83874
XDOT = 3479
328030 Wp = 103
88824
YDOT = -3367
364829 meter/sec RA = 31
99697 deg
ZDOT = -5980
173477 TA = 84
91768
MA = 84
74436
Ha = 194
560 n
mi
Hp = 181
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17406457
18 X = -5255691
89
Y = -13339339
54 feet Y = -4124881
25 meter
Z = -2659026
41 Z = -836124
83
XDOT = 11415
118208 XDOT = 3545
774559
YDOT = -11047
784871 feet/sec YDOT = -3328
084844 meter/sec
ZDOT = -19619
991721 ZDOT = -5963
109783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18813449
18 X = -5734339
31
Y = 11244166
07 feet Y = 3427221
82 meter
Z = -2759712
26 Z = -841160
30
XDOT = -5196
695843 XDOT = -1583
952893
YDOT = -13419
026940 feet/sec YDOT = -4090
119411 meter/sec
ZDOT = -19553
291294 ZDOT = -5959
843186
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 09151
53021280
00010596 00000-0 82463-4 0 9063
2 25544 51
6432 32
3727 0009268 62
8699 297
3408 15
73204769 3338
Satellite: ISS
Catalog Number: 25544
Epoch time: 09151
53021280 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 32
3727 deg
Eccentricity:
0009268
Arg of perigee: 62
8699 deg
Mean anomaly: 297
3408 deg
Mean motion: 15
73204769 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 333
Checksum: 311
Coasting Arc #8 (Orbit 348)
---------------------------------------
Vector Time (GMT): 2009/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2514765
60 A = 6722251
03 meter
Y = 3356649
19 meter E =
0012289
Z = 5244355
55 I = 51
77386
XDOT = -6604
787155 Wp = 64
28390
YDOT = -3920
747336 meter/sec RA = 26
86505 deg
ZDOT = -651
235726 TA = 31
92705
MA = 31
85264
Ha = 194
549 n
mi
Hp = 181
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8250543
30 X = -2577589
63
Y = 11012628
58 feet Y = 3328175
84 meter
Z = 17205890
92 Z = 5231986
45
XDOT = -21669
249195 XDOT = -6557
290202
YDOT = -12863
344277 feet/sec YDOT = -3994
340292 meter/sec
ZDOT = -2136
600150 ZDOT = -683
207022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7358657
50 X = 2242918
81
Y = 11698705
14 feet Y = 3565765
33 meter
Z = 17157581
21 Z = 5229630
75
XDOT = -18823
783811 XDOT = -5737
489305
YDOT = 15188
893504 feet/sec YDOT = 4629
574740 meter/sec
ZDOT = -2262
024656 ZDOT = -689
465115
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 09152
54652585
00010596 00000-0 82463-4 0 9074
2 25544 51
6433 27
1592 0009274 65
4375 294
7754 15
73295891 3496
Satellite: ISS
Catalog Number: 25544
Epoch time: 09152
54652585 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 27
1592 deg
Eccentricity:
0009274
Arg of perigee: 65
4375 deg
Mean anomaly: 294
7754 deg
Mean motion: 15
73295891 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 349
Checksum: 340
Coasting Arc #9 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2009/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6138197
98 A = 6734066
81 meter
Y = 2728216
46 meter E =
0021814
Z = 328950
78 I = 51
78651
XDOT = -2220
432248 Wp = 56
73361
YDOT = 4234
303761 meter/sec RA = 21
75388 deg
ZDOT = 6040
480330 TA = 306
83553
MA = 307
03540
Ha = 194
441 n
mi
Hp = 181
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20138444
83 X = 6105636
40
Y = 8950841
39 feet Y = 2796675
28 meter
Z = 1079234
86 Z = 358691
69
XDOT = -7284
882705 XDOT = -2296
959818
YDOT = 13892
072708 feet/sec YDOT = 4209
045070 meter/sec
ZDOT = 19817
848851 ZDOT = 6029
507901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15206036
66 X = 4634799
98
Y = -15943200
12 feet Y = -4859487
40 meter
Z = 1195863
16 Z = 364499
09
XDOT = 9427
600731 XDOT = 2873
532703
YDOT = 10535
968094 feet/sec YDOT = 3211
363075 meter/sec
ZDOT = 19775
046407 ZDOT = 6027
434145
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 09153
56282128
00010596 00000-0 82463-4 0 9080
2 25544 51
6430 21
9454 0009221 68
9879 291
2270 15
73318092 3653
Satellite: ISS
Catalog Number: 25544
Epoch time: 09153
56282128 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 21
9454 deg
Eccentricity:
0009221
Arg of perigee: 68
9879 deg
Mean anomaly: 291
2270 deg
Mean motion: 15
73318092 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 365
Checksum: 313
Coasting Arc #10 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2009/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1358437
19 A = 6721996
79 meter
Y = -3949502
20 meter E =
0023871
Z = -5287279
89 I = 51
71720
XDOT = 7323
578664 Wp = 83
72588
YDOT = 2314
974202 meter/sec RA = 16
62598 deg
ZDOT = 155
522840 TA = 187
73350
MA = 187
77037
Ha = 194
392 n
mi
Hp = 181
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4456814
92 X = 1428185
25
Y = -12957684
40 feet Y = -3933920
74 meter
Z = -17346718
80 Z = -5280511
57
XDOT = 24027
489054 XDOT = 7296
392409
YDOT = 7595
059719 feet/sec YDOT = 2396
718711 meter/sec
ZDOT = 510
245537 ZDOT = 191
035553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10814518
67 X = -3296265
29
Y = -8469026
79 feet Y = -2581359
37 meter
Z = -17320369
76 Z = -5279248
70
XDOT = 14274
819274 XDOT = 4350
964915
YDOT = -19535
280731 feet/sec YDOT = -5954
353567 meter/sec
ZDOT = 649
461728 ZDOT = 197
955935
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 09154
51558135
00010596 00000-0 82463-4 0 9091
2 25544 51
6423 17
0570 0009175 72
0184 288
1978 15
73342486 3804
Satellite: ISS
Catalog Number: 25544
Epoch time: 09154
51558135 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 17
0570 deg
Eccentricity:
0009175
Arg of perigee: 72
0184 deg
Mean anomaly: 288
1978 deg
Mean motion: 15
73342486 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 380
Checksum: 315
Coasting Arc #11 (Orbit 395)
---------------------------------------
Vector Time (GMT): 2009/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6601020
22 A = 6734084
50 meter
Y = -1309006
50 meter E =
0018751
Z = 42710
29 I = 51
72909
XDOT = 876
639664 Wp = 109
77989
YDOT = -4687
476793 meter/sec RA = 11
50333 deg
ZDOT = -6043
823138 TA = 69
75693
MA = 69
55543
Ha = 194
405 n
mi
Hp = 181
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21656890
48 X = -6586099
56
Y = -4294640
74 feet Y = -1382739
54 meter
Z = 140125
62 Z = 10678
08
XDOT = 2876
114382 XDOT = 958
350924
YDOT = -15378
860871 feet/sec YDOT = -4677
215953 meter/sec
ZDOT = -19828
816068 ZDOT = -6039
366551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10676758
87 X = -3254276
10
Y = 19325917
49 feet Y = 5890539
65 meter
Z = 14588
90 Z = 4446
70
XDOT = -12332
167477 XDOT = -3758
844647
YDOT = -6747
316746 feet/sec YDOT = -2056
582144 meter/sec
ZDOT = -19811
548271 ZDOT = -6038
559913
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 09155
53184086
00010596 00000-0 82463-4 0 9106
2 25544 51
6423 11
8438 0009119 76
5228 283
6950 15
73329247 3962
Satellite: ISS
Catalog Number: 25544
Epoch time: 09155
53184086 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 11
8438 deg
Eccentricity:
0009119
Arg of perigee: 76
5228 deg
Mean anomaly: 283
6950 deg
Mean motion: 15
73329247 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 396
Checksum: 318
Coasting Arc #12 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2009/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -147037
40 A = 6721894
89 meter
Y = 4170001
96 meter E =
0011401
Z = 5260282
31 I = 51
65841
XDOT = -7678
175912 Wp = 83
66434
YDOT = -630
669854 meter/sec RA = 6
37841 deg
ZDOT = 286
039021 TA = 3
62838
MA = 3
62012
Ha = 194
371 n
mi
Hp = 181
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -482406
17 X = -219210
02
Y = 13681108
80 feet Y = 4167953
29 meter
Z = 17258144
07 Z = 5259393
38
XDOT = -25190
865853 XDOT = -7671
942538
YDOT = -2069
126817 feet/sec YDOT = -716
496895 meter/sec
ZDOT = 938
448232 ZDOT = 248
752914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12935633
36 X = 3942781
05
Y = 4493255
65 feet Y = 1369544
32 meter
Z = 17254826
39 Z = 5259271
08
XDOT = -8901
466810 XDOT = -2713
167084
YDOT = 22592
589300 feet/sec YDOT = 6886
221219 meter/sec
ZDOT = 792
357218 ZDOT = 241
510480
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 09156
54807995
00010596 00000-0 82463-4 0 9110
2 25544 51
6416 6
6292 0009087 79
6179 280
6007 15
73371468 4128
Satellite: ISS
Catalog Number: 25544
Epoch time: 09156
54807995 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 6
6292 deg
Eccentricity:
0009087
Arg of perigee: 79
6179 deg
Mean anomaly: 280
6007 deg
Mean motion: 15
73371468 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 412
Checksum: 328
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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