Date:
April 19th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 3639)
---------------------------------------
Vector Time (GMT): 2009/107/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4071545
43 A = 6725180
58 meter
Y = 1069829
98 meter E =
0007370
Z = -5250412
24 I = 51
29521
XDOT = -1794
825500 Wp = 112
98075
YDOT = -7480
012739 meter/sec RA = 257
31447 deg
ZDOT = -135
287252 TA = 155
74543
MA = 155
71072
Ha = 191
802 n
mi
Hp = 189
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13358088
68 X = -4057700
26
Y = 3509940
88 feet Y = 1024377
05 meter
Z = -17225761
95 Z = -5270158
19
XDOT = -5888
535104 XDOT = -1710
392145
YDOT = -24540
724209 feet/sec YDOT = -7499
611432 meter/sec
ZDOT = -443
855815 ZDOT = -143
801506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11593320
95 X = -3533644
22
Y = 7327543
14 feet Y = 2233435
15 meter
Z = -17302806
54 Z = -5273895
43
XDOT = -12446
380345 XDOT = -3793
656729
YDOT = -20796
966079 feet/sec YDOT = -6338
915261 meter/sec
ZDOT = -477
646309 ZDOT = -145
586595
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
49530836
00010596 00000-0 82463-4 0 9005
2 25544 51
6392 258
0475 0008825 249
0667 110
9551 15
72220749 36400
Satellite: ISS
Catalog Number: 25544
Epoch time: 09107
49530836 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 258
0475 deg
Eccentricity:
0008825
Arg of perigee: 249
0667 deg
Mean anomaly: 110
9551 deg
Mean motion: 15
72220749 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3640
Checksum: 315
Coasting Arc #2 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2009/108/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2564617
47 A = 6736963
99 meter
Y = 6184212
02 meter E =
0010788
Z = 683521
79 I = 51
34210
XDOT = -4232
950221 Wp = 169
56130
YDOT = 2414
841220 meter/sec RA = 252
16065 deg
ZDOT = -5961
921476 TA = 2
96525
MA = 2
95886
Ha = 191
555 n
mi
Hp = 189
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8414099
30 X = 2491953
53
Y = 20289409
50 feet Y = 6212484
78 meter
Z = 2242525
57 Z = 695804
18
XDOT = -13887
631958 XDOT = -4230
676823
YDOT = 7922
707414 feet/sec YDOT = 2367
518585 meter/sec
ZDOT = -19560
109829 ZDOT = -5982
479649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14391209
42 X = 4386440
63
Y = 16587066
06 feet Y = 5055737
73 meter
Z = 2290951
04 Z = 698281
88
XDOT = -9348
746287 XDOT = -2849
497868
YDOT = 10825
643840 feet/sec YDOT = 3299
656243 meter/sec
ZDOT = -19640
231861 ZDOT = -5986
342671
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
51229229
00010596 00000-0 82463-4 0 9011
2 25544 51
6384 252
8375 0008950 254
3541 105
6633 15
72245658 36566
Satellite: ISS
Catalog Number: 25544
Epoch time: 09108
51229229 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 252
8375 deg
Eccentricity:
0008950
Arg of perigee: 254
3541 deg
Mean anomaly: 105
6633 deg
Mean motion: 15
72245658 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3656
Checksum: 317
Coasting Arc #3 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2009/109/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3147181
31 A = 6725752
83 meter
Y = -3051761
47 meter E =
0006768
Z = 5106049
81 I = 51
31547
XDOT = 3957
437759 Wp = 228
24919
YDOT = 6445
546460 meter/sec RA = 247
03480 deg
ZDOT = 1409
886592 TA = 208
15526
MA = 208
19187
Ha = 191
338 n
mi
Hp = 189
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10325398
00 X = 3156268
41
Y = -10012340
79 feet Y = -3016516
95 meter
Z = 16752131
93 Z = 5121360
97
XDOT = 12983
719682 XDOT = 3878
219466
YDOT = 21146
805972 feet/sec YDOT = 6489
357933 meter/sec
ZDOT = 4625
612177 ZDOT = 1428
919304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6313223
46 X = 1924270
51
Y = -12845398
96 feet Y = -3915277
60 meter
Z = 16811712
33 Z = 5124209
92
XDOT = 18319
113562 XDOT = 5583
665814
YDOT = 15169
097380 feet/sec YDOT = 4623
540882 meter/sec
ZDOT = 4700
434987 ZDOT = 1432
692584
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
52926423
00010596 00000-0 82463-4 0 9024
2 25544 51
6392 247
6281 0008944 258
0865 101
9294 15
72257429 36725
Satellite: ISS
Catalog Number: 25544
Epoch time: 09109
52926423 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 247
6281 deg
Eccentricity:
0008944
Arg of perigee: 258
0865 deg
Mean anomaly: 101
9294 deg
Mean motion: 15
72257429 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3672
Checksum: 329
Coasting Arc #4 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2009/110/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4232981
36 A = 6735725
35 meter
Y = -4929161
06 meter E =
0006167
Z = -1761718
89 I = 51
36307
XDOT = 2775
783605 Wp = 317
63889
YDOT = -4410
731874 meter/sec RA = 241
86286 deg
ZDOT = 5664
353409 TA = 22
78680
MA = 22
75944
Ha = 191
160 n
mi
Hp = 190
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13887734
12 X = -4168989
90
Y = -16171788
27 feet Y = -4976139
00 meter
Z = -5779917
62 Z = -1782127
19
XDOT = 9106
901592 XDOT = 2797
382332
YDOT = -14470
905099 feet/sec YDOT = -4379
570490 meter/sec
ZDOT = 18583
836644 ZDOT = 5677
890828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18626594
15 X = -5677385
90
Y = -10320543
31 feet Y = -3145701
60 meter
Z = -5860010
12 Z = -1786131
08
XDOT = 2631
036500 XDOT = 801
939925
YDOT = -15343
164381 feet/sec YDOT = -4676
596503 meter/sec
ZDOT = 18636
384695 ZDOT = 5680
370055
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
48266277
00010596 00000-0 82463-4 0 9036
2 25544 51
6403 242
7447 0008854 261
5376 98
4783 15
72267239 36873
Satellite: ISS
Catalog Number: 25544
Epoch time: 09110
48266277 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 242
7447 deg
Eccentricity:
0008854
Arg of perigee: 261
5376 deg
Mean anomaly: 98
4783 deg
Mean motion: 15
72267239 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3687
Checksum: 339
Coasting Arc #5 (Orbit 3702)
---------------------------------------
Vector Time (GMT): 2009/111/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1581357
91 A = 6727251
76 meter
Y = 4505208
90 meter E =
0003621
Z = -4741981
89 I = 51
34993
XDOT = -5538
761804 Wp = 33
39748
YDOT = -4672
233689 meter/sec RA = 236
75750 deg
ZDOT = -2589
833882 TA = 211
06442
MA = 211
08584
Ha = 190
779 n
mi
Hp = 190
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5188182
13 X = -1608582
51
Y = 14780869
09 feet Y = 4487372
81 meter
Z = -15557683
35 Z = -4749730
50
XDOT = -18171
790697 XDOT = -5473
523403
YDOT = -15328
850686 feet/sec YDOT = -4733
806698 meter/sec
ZDOT = -8496
830321 ZDOT = -2616
582735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 649261
12 X = 197894
79
Y = 15621707
72 feet Y = 4761496
51 meter
Z = -15587608
67 Z = -4751103
12
XDOT = -21328
238704 XDOT = -6500
847157
YDOT = -7703
139575 feet/sec YDOT = -2347
916942 meter/sec
ZDOT = -8601
679328 ZDOT = -2621
791859
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
49960782
00010596 00000-0 82463-4 0 9041
2 25544 51
6405 237
5360 0008896 266
1939 93
8206 15
72290102 37036
Satellite: ISS
Catalog Number: 25544
Epoch time: 09111
49960782 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 237
5360 deg
Eccentricity:
0008896
Arg of perigee: 266
1939 deg
Mean anomaly: 93
8206 deg
Mean motion: 15
72290102 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3703
Checksum: 317
Coasting Arc #6 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2009/112/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5284995
48 A = 6733701
73 meter
Y = 3140384
88 meter E =
0005122
Z = 2740269
32 I = 51
38946
XDOT = -717
590955 Wp = 119
21122
YDOT = 5690
793175 meter/sec RA = 231
57187 deg
ZDOT = -5132
999081 TA = 29
38790
MA = 29
35911
Ha = 189
712 n
mi
Hp = 189
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17339224
01 X = 5236174
47
Y = 10303099
99 feet Y = 3199211
93 meter
Z = 8990384
92 Z = 2765825
44
XDOT = -2354
301035 XDOT = -756
237523
YDOT = 18670
581283 feet/sec YDOT = 5682
552352 meter/sec
ZDOT = -16840
548167 ZDOT = -5136
579298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19908556
80 X = 6068128
11
Y = 2939801
76 feet Y = 896051
58 meter
Z = 9090462
66 Z = 2770773
02
XDOT = 5241
180044 XDOT = 1597
511677
YDOT = 16670
277018 feet/sec YDOT = 5081
100435 meter/sec
ZDOT = -16854
096812 ZDOT = -5137
128708
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
51654020
00010596 00000-0 82463-4 0 9051
2 25544 51
6408 232
3263 0008859 269
7524 90
2623 15
72294819 37192
Satellite: ISS
Catalog Number: 25544
Epoch time: 09112
51654020 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 232
3263 deg
Eccentricity:
0008859
Arg of perigee: 269
7524 deg
Mean anomaly: 90
2623 deg
Mean motion: 15
72294819 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3719
Checksum: 313
Coasting Arc #7 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2009/113/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -378285
60 A = 6729242
33 meter
Y = -5254113
65 meter E =
0002342
Z = 4187965
99 I = 51
39553
XDOT = 6326
357011 Wp = 156
89275
YDOT = 2445
397173 meter/sec RA = 226
47959 deg
ZDOT = 3636
562291 TA = 255
88932
MA = 255
91535
Ha = 190
649 n
mi
Hp = 190
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1241094
48 X = -339849
85
Y = -17237905
67 feet Y = -5258128
82 meter
Z = 13740045
89 Z = 4186221
77
XDOT = 20755
764471 XDOT = 6280
875894
YDOT = 8022
956605 feet/sec YDOT = 2515
888008 meter/sec
ZDOT = 11930
978646 ZDOT = 3667
185732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8052882
89 X = -2454518
70
Y = -15298205
79 feet Y = -4662893
13 meter
Z = 13732827
28 Z = 4185765
76
XDOT = 21056
083629 XDOT = 6417
894290
YDOT = -257
803645 feet/sec YDOT = -78
578551 meter/sec
ZDOT = 12050
803463 ZDOT = 3673
084895
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
53345718
00010596 00000-0 82463-4 0 9066
2 25544 51
6420 227
1168 0008928 274
2331 85
7811 15
72361083 37350
Satellite: ISS
Catalog Number: 25544
Epoch time: 09113
53345718 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 227
1168 deg
Eccentricity:
0008928
Arg of perigee: 274
2331 deg
Mean anomaly: 85
7811 deg
Mean motion: 15
72361083 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3735
Checksum: 306
Coasting Arc #8 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2009/114/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5587722
01 A = 6731249
65 meter
Y = -1102395
53 meter E =
0003454
Z = -3584288
85 I = 51
42366
XDOT = -1623
355731 Wp = 279
09835
YDOT = -6100
672120 meter/sec RA = 221
29025 deg
ZDOT = 4404
001194 TA = 37
95588
MA = 37
93154
Ha = 190
988 n
mi
Hp = 190
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18332421
31 X = -5557567
33
Y = -3616783
24 feet Y = -1164712
13 meter
Z = -11759477
85 Z = -3611361
35
XDOT = -5325
970245 XDOT = -1576
410656
YDOT = -20015
328478 feet/sec YDOT = -6118
562900 meter/sec
ZDOT = 14448
822815 ZDOT = 4396
228855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18129409
19 X = -5525843
92
Y = 4240581
54 feet Y = 1292529
25 meter
Z = -11865331
95 Z = -3616553
18
XDOT = -12876
189653 XDOT = -3924
662606
YDOT = -14678
424935 feet/sec YDOT = -4473
983920 meter/sec
ZDOT = 14417
989394 ZDOT = 4394
603167
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
48680754
00010596 00000-0 82463-4 0 9074
2 25544 51
6421 222
2339 0008979 279
1041 80
9105 15
72331450 37500
Satellite: ISS
Catalog Number: 25544
Epoch time: 09114
48680754 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 222
2339 deg
Eccentricity:
0008979
Arg of perigee: 279
1041 deg
Mean anomaly: 80
9105 deg
Mean motion: 15
72331450 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3750
Checksum: 304
Coasting Arc #9 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2009/115/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2439249
20 A = 6731628
62 meter
Y = 5220972
27 meter E =
0004260
Z = -3478521
34 I = 51
44835
XDOT = -6230
739441 Wp = 302
10680
YDOT = -101
582142 meter/sec RA = 216
20475 deg
ZDOT = -4515
396814 TA = 279
25431
MA = 279
30249
Ha = 191
252 n
mi
Hp = 189
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8002786
10 X = 2397584
56
Y = 17129174
12 feet Y = 5248016
48 meter
Z = -11412471
59 Z = -3466772
29
XDOT = -20442
058535 XDOT = -6207
204933
YDOT = -333
274744 feet/sec YDOT = -171
126235 meter/sec
ZDOT = -14814
294008 ZDOT = -4545
609314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14626000
74 X = 4458005
02
Y = 12024475
11 feet Y = 3665060
01 meter
Z = -11366169
09 Z = -3464408
34
XDOT = -17661
465675 XDOT = -5383
214738
YDOT = 7348
228359 feet/sec YDOT = 2239
740004 meter/sec
ZDOT = -14932
347580 ZDOT = -4551
379542
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 09115
50370101
00010596 00000-0 82463-4 0 9081
2 25544 51
6424 217
0248 0008889 282
6663 77
3505 15
72363988 37665
Satellite: ISS
Catalog Number: 25544
Epoch time: 09115
50370101 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 217
0248 deg
Eccentricity:
0008889
Arg of perigee: 282
6663 deg
Mean anomaly: 77
3505 deg
Mean motion: 15
72363988 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3766
Checksum: 326
Coasting Arc #10 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2009/116/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5128337
20 A = 6728784
28 meter
Y = -883263
30 meter E =
0005777
Z = 4268449
52 I = 51
46367
XDOT = 3903
422865 Wp = 9
57377
YDOT = 5619
234915 meter/sec RA = 211
01899 deg
ZDOT = -3520
708381 TA = 116
25502
MA = 116
19564
Ha = 191
441 n
mi
Hp = 189
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16825253
27 X = 5117097
01
Y = -2897845
46 feet Y = -825978
30 meter
Z = 14004099
48 Z = 4293336
22
XDOT = 12806
505462 XDOT = 3857
400884
YDOT = 18435
810089 feet/sec YDOT = 5662
628117 meter/sec
ZDOT = -11550
880515 ZDOT = -3501
856625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13720176
13 X = 4181909
68
Y = -10025574
17 feet Y = -3055795
01 meter
Z = 14101279
65 Z = 4298070
04
XDOT = 18985
010115 XDOT = 5786
631083
YDOT = 9810
044015 feet/sec YDOT = 2990
101416 meter/sec
ZDOT = -11476
793119 ZDOT = -3498
126543
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 09116
52058200
00010596 00000-0 82463-4 0 9098
2 25544 51
6423 211
8160 0008769 287
7135 72
3069 15
72377811 37824
Satellite: ISS
Catalog Number: 25544
Epoch time: 09116
52058200 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 211
8160 deg
Eccentricity:
0008769
Arg of perigee: 287
7135 deg
Mean anomaly: 72
3069 deg
Mean motion: 15
72377811 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3782
Checksum: 312
Coasting Arc #11 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2009/117/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4302954
41 A = 6733675
03 meter
Y = -4439521
91 meter E =
0008087
Z = 2654312
02 I = 51
50616
XDOT = 5301
137310 Wp = 40
09032
YDOT = -2024
707829 meter/sec RA = 205
93154 deg
ZDOT = 5204
616208 TA = 350
17730
MA = 350
19310
Ha = 191
665 n
mi
Hp = 189
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14117304
48 X = -4265885
54
Y = -14565360
59 feet Y = -4487432
99 meter
Z = 8708372
76 Z = 2633497
57
XDOT = 17392
182774 XDOT = 5298
100364
YDOT = -6642
742222 feet/sec YDOT = -1965
444794 meter/sec
ZDOT = 17075
512495 ZDOT = 5230
362104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19272461
27 X = -5874246
20
Y = -6437087
51 feet Y = -1962024
27 meter
Z = 8626697
63 Z = 2629417
44
XDOT = 11845
214696 XDOT = 3610
421439
YDOT = -12433
821617 feet/sec YDOT = -3789
828829 meter/sec
ZDOT = 17175
977858 ZDOT = 5235
238051
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 09117
53744834
00010596 00000-0 82463-4 0 9107
2 25544 51
6421 206
6061 0008849 291
8648 68
1573 15
72420359 37984
Satellite: ISS
Catalog Number: 25544
Epoch time: 09117
53744834 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 206
6061 deg
Eccentricity:
0008849
Arg of perigee: 291
8648 deg
Mean anomaly: 68
1573 deg
Mean motion: 15
72420359 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3798
Checksum: 331
Coasting Arc #12 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2009/118/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3983429
95 A = 6726545
87 meter
Y = 2556703
08 meter E =
0003305
Z = -4782053
62 I = 51
50933
XDOT = -5822
371033 Wp = 85
37621
YDOT = -4353
373406 meter/sec RA = 200
75792 deg
ZDOT = 2524
255601 TA = 209
39028
MA = 209
40887
Ha = 191
716 n
mi
Hp = 188
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13068995
91 X = -3988492
71
Y = 8388133
47 feet Y = 2512130
17 meter
Z = -15689152
29 Z = -4801417
45
XDOT = -19102
267169 XDOT = -5785
520690
YDOT = -14282
721147 feet/sec YDOT = -4418
276742 meter/sec
ZDOT = 8281
678482 ZDOT = 2496
059248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7447999
75 X = -2270150
32
Y = 13539280
16 feet Y = 4126772
59 meter
Z = -15764648
09 Z = -4805064
74
XDOT = -22645
524210 XDOT = -6902
355779
YDOT = -2949
864214 feet/sec YDOT = -899
118613 meter/sec
ZDOT = 8171
146903 ZDOT = 2490
565576
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 09118
49075048
00010596 00000-0 82463-4 0 9118
2 25544 51
6415 201
7233 0008853 296
1814 63
8438 15
72457549 38133
Satellite: ISS
Catalog Number: 25544
Epoch time: 09118
49075048 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 201
7233 deg
Eccentricity:
0008853
Arg of perigee: 296
1814 deg
Mean anomaly: 63
8438 deg
Mean motion: 15
72457549 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3813
Checksum: 321
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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