Date:
February 5th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9526 06 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 2492)
---------------------------------------
Vector Time (GMT): 2009/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3769841
88 A = 6732045
11 meter
Y = -3058364
71 meter E =
0006456
Z = 4658302
08 I = 51
29933
XDOT = 2138
317633 Wp = 43
62364
YDOT = 6856
847021 meter/sec RA = 270
70191 deg
ZDOT = 2773
638277 TA = 18
89841
MA = 18
87446
Ha = 196
341 n
mi
Hp = 188
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12368247
63 X = 3781131
85
Y = -10034004
96 feet Y = -3016145
24 meter
Z = 15283143
30 Z = 4676643
08
XDOT = 7015
477799 XDOT = 2048
010601
YDOT = 22496
217259 feet/sec YDOT = 6880
253867 meter/sec
ZDOT = 9099
863112 ZDOT = 2783
807097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15714571
77 X = 4789801
47
Y = 2127351
99 feet Y = 648416
89 meter
Z = 15354344
06 Z = 4680004
07
XDOT = -11535
298225 XDOT = -3515
958899
YDOT = 19296
662703 feet/sec YDOT = 5881
622792 meter/sec
ZDOT = 9139
954170 ZDOT = 2785
858031
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 09034
55259493
00010596 00000-0 82463-4 0 9008
2 25544 51
6416 271
1653 0008687 342
9361 17
1507 15
70711658 24937
Satellite: ISS
Catalog Number: 25544
Epoch time: 09034
55259493 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 271
1653 deg
Eccentricity:
0008687
Arg of perigee: 342
9361 deg
Mean anomaly: 17
1507 deg
Mean motion: 15
70711658 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2493
Checksum: 315
Coasting Arc #2 (Orbit 2507)
---------------------------------------
Vector Time (GMT): 2009/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3055943
76 A = 6736637
05 meter
Y = -4999205
66 meter E =
0009070
Z = -3317280
26 I = 51
31544
XDOT = 3343
001982 Wp = 16
01297
YDOT = -5129
772470 meter/sec RA = 265
52068 deg
ZDOT = 4662
648081 TA = 304
85159
MA = 304
93685
Ha = 196
449 n
mi
Hp = 188
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10026062
22 X = -2983700
15
Y = -16401593
38 feet Y = -5032974
84 meter
Z = -10883465
44 Z = -3331950
72
XDOT = 10967
854271 XDOT = 3377
465465
YDOT = -16829
962172 feet/sec YDOT = -5092
196705 meter/sec
ZDOT = 15297
401839 ZDOT = 4678
971545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4869692
56 X = 1484282
29
Y = -18562476
08 feet Y = -5657842
71 meter
Z = -10940959
06 Z = -3334804
32
XDOT = 18308
609686 XDOT = 5580
464232
YDOT = -4228
286111 feet/sec YDOT = -1288
781607 meter/sec
ZDOT = 15360
600162 ZDOT = 4681
910929
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 09035
50691891
00010596 00000-0 82463-4 0 9017
2 25544 51
6411 266
2878 0008817 345
0593 15
0307 15
70742902 25080
Satellite: ISS
Catalog Number: 25544
Epoch time: 09035
50691891 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 266
2878 deg
Eccentricity:
0008817
Arg of perigee: 345
0593 deg
Mean anomaly: 15
0307 deg
Mean motion: 15
70742902 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2508
Checksum: 307
Coasting Arc #3 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2009/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1780578
71 A = 6736553
52 meter
Y = 5573876
87 meter E =
0008999
Z = -3349551
39 I = 51
31796
XDOT = -4465
643431 Wp = 19
79814
YDOT = -4209
713960 meter/sec RA = 260
43767 deg
ZDOT = -4626
662884 TA = 199
72661
MA = 199
76144
Ha = 196
613 n
mi
Hp = 188
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5841793
68 X = -1826503
16
Y = 18286997
60 feet Y = 5553708
90 meter
Z = -10989341
84 Z = -3358312
39
XDOT = -14651
061124 XDOT = -4395
762723
YDOT = -13811
397508 feet/sec YDOT = -4259
260278 meter/sec
ZDOT = -15179
340171 ZDOT = -4648
187204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17015171
25 X = -5186224
20
Y = 8847747
78 feet Y = 2696793
52 meter
Z = -11023056
54 Z = -3359827
63
XDOT = 110
328653 XDOT = 33
628174
YDOT = -18823
151430 feet/sec YDOT = -5737
296556 meter/sec
ZDOT = -15263
479581 ZDOT = -4652
308576
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 09036
52485242
00010596 00000-0 82463-4 0 9022
2 25544 51
6403 261
0854 0008771 348
4408 11
6551 15
70752457 25246
Satellite: ISS
Catalog Number: 25544
Epoch time: 09036
52485242 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 261
0854 deg
Eccentricity:
0008771
Arg of perigee: 348
4408 deg
Mean anomaly: 11
6551 deg
Mean motion: 15
70752457 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2524
Checksum: 298
Coasting Arc #4 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2009/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4395605
73 A = 6731869
47 meter
Y = 2145386
51 meter E =
0013770
Z = 4625911
95 I = 51
30900
XDOT = -475
632728 Wp = 25
92951
YDOT = 7134
693407 meter/sec RA = 255
25589 deg
ZDOT = -2841
538769 TA = 92
38750
MA = 92
22983
Ha = 196
596 n
mi
Hp = 188
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14421278
65 X = 4348817
68
Y = 7038669
64 feet Y = 2194278
75 meter
Z = 15176876
46 Z = 4647151
81
XDOT = -1560
474829 XDOT = -541
575352
YDOT = 23407
786769 feet/sec YDOT = 7129
006128 meter/sec
ZDOT = -9322
633755 ZDOT = -2844
008938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5419779
19 X = 1651948
70
Y = 15020624
70 feet Y = 4578286
41 meter
Z = 15259769
15 Z = 4651177
64
XDOT = -16250
155195 XDOT = -4953
047304
YDOT = 15394
793083 feet/sec YDOT = 4692
332932 meter/sec
ZDOT = -9331
725793 ZDOT = -2844
310022
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 09037
54277101
00010596 00000-0 82463-4 0 9039
2 25544 51
6402 255
8823 0008882 352
1090 7
9930 15
70820797 25404
Satellite: ISS
Catalog Number: 25544
Epoch time: 09037
54277101 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 255
8823 deg
Eccentricity:
0008882
Arg of perigee: 352
1090 deg
Mean anomaly: 7
9930 deg
Mean motion: 15
70820797 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2540
Checksum: 303
Coasting Arc #5 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2009/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1041665
20 A = 6740229
24 meter
Y = -6470577
02 meter E =
0019332
Z = 1520867
74 I = 51
34429
XDOT = 5090
509815 Wp = 37
51305
YDOT = 539
209594 meter/sec RA = 250
15758 deg
ZDOT = 5757
417639 TA = 339
31304
MA = 339
39119
Ha = 196
703 n
mi
Hp = 188
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3417536
75 X = -976620
60
Y = -21228927
23 feet Y = -6481861
94 meter
Z = 4989723
54 Z = 1515965
06
XDOT = 16701
147686 XDOT = 5056
134297
YDOT = 1769
060349 feet/sec YDOT = 595
942069 meter/sec
ZDOT = 18889
165483 ZDOT = 5782
063132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11963610
50 X = 3646508
48
Y = -17872158
44 feet Y = -5447433
89 meter
Z = 4970133
43 Z = 1514896
67
XDOT = 9620
399534 XDOT = 2932
297778
YDOT = 11740
836815 feet/sec YDOT = 3578
607061 meter/sec
ZDOT = 18985
216085 ZDOT = 5786
693863
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 09038
56067720
00010596 00000-0 82463-4 0 9047
2 25544 51
6387 250
6788 0008800 355
9079 4
2009 15
70829067 25560
Satellite: ISS
Catalog Number: 25544
Epoch time: 09038
56067720 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 250
6788 deg
Eccentricity:
0008800
Arg of perigee: 355
9079 deg
Mean anomaly: 4
2009 deg
Mean motion: 15
70829067 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2556
Checksum: 327
Coasting Arc #6 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2009/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4075728
44 A = 6729235
95 meter
Y = 1178158
56 meter E =
0016688
Z = -5235445
69 I = 51
31708
XDOT = -2805
227583 Wp = 62
66346
YDOT = -7131
157371 meter/sec RA = 245
00392 deg
ZDOT = 588
055887 TA = 212
90952
MA = 213
01353
Ha = 196
825 n
mi
Hp = 187
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13371812
47 X = -4063167
90
Y = 3865349
60 feet Y = 1132651
80 meter
Z = -17176659
08 Z = -5255214
36
XDOT = -9203
502570 XDOT = -2728
133885
YDOT = -23396
185600 feet/sec YDOT = -7162
096021 meter/sec
ZDOT = 1929
317215 ZDOT = 574
615571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12446138
66 X = -3793583
06
Y = -6015920
73 feet Y = -1833652
64 meter
Z = -17253586
40 Z = -5258893
14
XDOT = 8382
523429 XDOT = 2554
993141
YDOT = -22639
676057 feet/sec YDOT = -6900
573262 meter/sec
ZDOT = 1876
398168 ZDOT = 571
926161
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 09039
51495230
00010596 00000-0 82463-4 0 9055
2 25544 51
6371 245
8000 0008850 359
9693
1466 15
70838839 25713
Satellite: ISS
Catalog Number: 25544
Epoch time: 09039
51495230 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 245
8000 deg
Eccentricity:
0008850
Arg of perigee: 359
9693 deg
Mean anomaly:
1466 deg
Mean motion: 15
70838839 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2571
Checksum: 318
Coasting Arc #7 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2009/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3707360
89 A = 6740967
58 meter
Y = 5608230
83 meter E =
0010637
Z = 489926
95 I = 51
37081
XDOT = -3770
503635 Wp = 86
87576
YDOT = 3024
815734 meter/sec RA = 239
87159 deg
ZDOT = -5980
790784 TA = 87
78579
MA = 87
66399
Ha = 196
964 n
mi
Hp = 187
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12163257
51 X = 3641993
29
Y = 18399707
46 feet Y = 5649323
21 meter
Z = 1607371
89 Z = 507777
92
XDOT = -12370
418749 XDOT = -3774
994782
YDOT = 9923
936135 feet/sec YDOT = 2982
626655 meter/sec
ZDOT = -19622
017008 ZDOT = -5999
118178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2917045
55 X = -889115
48
Y = 21857606
84 feet Y = 6662198
56 meter
Z = 1677373
24 Z = 511263
36
XDOT = -14166
658712 XDOT = -4317
997575
YDOT = -352
230393 feet/sec YDOT = -107
359824 meter/sec
ZDOT = -19693
184564 ZDOT = -6002
482655
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 09040
53283102
00010596 00000-0 82463-4 0 9063
2 25544 51
6374 240
5971 0008998 3
4327 356
6895 15
70874413 25873
Satellite: ISS
Catalog Number: 25544
Epoch time: 09040
53283102 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 240
5971 deg
Eccentricity:
0008998
Arg of perigee: 3
4327 deg
Mean anomaly: 356
6895 deg
Mean motion: 15
70874413 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2587
Checksum: 326
Coasting Arc #8 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2009/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2190552
40 A = 6730140
90 meter
Y = -3880847
69 meter E =
0007996
Z = 5037118
09 I = 51
34875
XDOT = 5375
817945 Wp = 43
56535
YDOT = 5243
788561 meter/sec RA = 234
75746 deg
ZDOT = 1706
335146 TA = 29
97570
MA = 29
92994
Ha = 197
049 n
mi
Hp = 187
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7186851
72 X = 2209317
23
Y = -12732439
94 feet Y = -3856246
59 meter
Z = 16525978
00 Z = 5047805
16
XDOT = 17637
197982 XDOT = 5308
492682
YDOT = 17204
030711 feet/sec YDOT = 5303
527698 meter/sec
ZDOT = 5598
212420 ZDOT = 1732
286372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13622089
74 X = 4152012
95
Y = -5180438
88 feet Y = -1578997
77 meter
Z = 16567303
26 Z = 5049714
03
XDOT = 2022
889798 XDOT = 616
576810
YDOT = 23504
395954 feet/sec YDOT = 7164
139887 meter/sec
ZDOT = 5699
761330 ZDOT = 1737
287253
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 09041
55069813
00010596 00000-0 82463-4 0 9078
2 25544 51
6363 235
3922 0008935 7
8437 352
2863 15
70828459 26035
Satellite: ISS
Catalog Number: 25544
Epoch time: 09041
55069813 = yrday
fracday
Element set: 907
Inclination: 51
6363 deg
RA of node: 235
3922 deg
Eccentricity:
0008935
Arg of perigee: 7
8437 deg
Mean anomaly: 352
2863 deg
Mean motion: 15
70828459 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2603
Checksum: 323
Coasting Arc #9 (Orbit 2617)
---------------------------------------
Vector Time (GMT): 2009/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5350586
56 A = 6738384
79 meter
Y = -3277663
95 meter E =
0013470
Z = -2441413
06 I = 51
39489
XDOT = 930
677179 Wp = 25
48001
YDOT = -5473
468002 meter/sec RA = 229
58995 deg
ZDOT = 5331
469019 TA = 306
87379
MA = 306
99719
Ha = 197
001 n
mi
Hp = 187
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17554417
85 X = -5301677
88
Y = -10753490
64 feet Y = -3337223
97 meter
Z = -8009885
36 Z = -2467286
57
XDOT = 3053
402819 XDOT = 965
914594
YDOT = -17957
572184 feet/sec YDOT = -5462
863345 meter/sec
ZDOT = 17491
696257 ZDOT = 5336
075988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6812780
73 X = -2076535
57
Y = -19384309
00 feet Y = -5908337
38 meter
Z = -8110979
82 Z = -2472226
65
XDOT = 12198
075292 XDOT = 3717
973349
YDOT = -11582
508049 feet/sec YDOT = -3530
348453 meter/sec
ZDOT = 17509
192737 ZDOT = 5336
801946
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 09042
50493243
00010596 00000-0 82463-4 0 9083
2 25544 51
6360 230
5130 0008804 11
1707 348
9648 15
70890852 26188
Satellite: ISS
Catalog Number: 25544
Epoch time: 09042
50493243 = yrday
fracday
Element set: 908
Inclination: 51
6360 deg
RA of node: 230
5130 deg
Eccentricity:
0008804
Arg of perigee: 11
1707 deg
Mean anomaly: 348
9648 deg
Mean motion: 15
70890852 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2618
Checksum: 301
Coasting Arc #10 (Orbit 2633)
---------------------------------------
Vector Time (GMT): 2009/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 678231
69 A = 6733583
79 meter
Y = 5288371
93 meter E =
0014790
Z = -4128715
83 I = 51
39903
XDOT = -6380
817510 Wp = 41
20683
YDOT = -2096
456180 meter/sec RA = 224
50725 deg
ZDOT = -3730
143091 TA = 190
36932
MA = 190
39986
Ha = 197
190 n
mi
Hp = 186
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2225169
57 X = 639101
97
Y = 17350301
59 feet Y = 5295737
30 meter
Z = -13545655
60 Z = -4125516
38
XDOT = -20934
440650 XDOT = -6338
780367
YDOT = -6878
137074 feet/sec YDOT = -2167
575354 meter/sec
ZDOT = -12238
002268 ZDOT = -3761
038240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8890795
19 X = -2709914
38
Y = 15076066
04 feet Y = 4595184
93 meter
Z = -13532742
67 Z = -4124779
97
XDOT = -11077
510529 XDOT = -3376
425209
YDOT = -17636
028865 feet/sec YDOT = -5375
461598 meter/sec
ZDOT = -12358
573081 ZDOT = -3766
893075
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 09043
52277012
00010596 00000-0 82463-4 0 9091
2 25544 51
6360 225
3094 0008935 15
8372 344
3067 15
70928661 26346
Satellite: ISS
Catalog Number: 25544
Epoch time: 09043
52277012 = yrday
fracday
Element set: 909
Inclination: 51
6360 deg
RA of node: 225
3094 deg
Eccentricity:
0008935
Arg of perigee: 15
8372 deg
Mean anomaly: 344
3067 deg
Mean motion: 15
70928661 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2634
Checksum: 307
Coasting Arc #11 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2009/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5421129
60 A = 6733987
64 meter
Y = 341176
81 meter E =
0017114
Z = 3976330
63 I = 51
42249
XDOT = 2516
285046 Wp = 52
10084
YDOT = 6117
752897 meter/sec RA = 219
32709 deg
ZDOT = -3933
623154 TA = 78
82329
MA = 78
63094
Ha = 197
156 n
mi
Hp = 186
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17785858
26 X = 5397595
61
Y = 1119346
50 feet Y = 401667
64 meter
Z = 13045704
16 Z = 4002608
87
XDOT = 8255
528366 XDOT = 2466
796826
YDOT = 20071
367772 feet/sec YDOT = 6145
614566 meter/sec
ZDOT = -12905
587775 ZDOT = -3921
519742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13449025
40 X = 4099262
94
Y = 11577141
23 feet Y = 3528712
65 meter
Z = 13148140
72 Z = 4007553
29
XDOT = -4621
176547 XDOT = -1408
534612
YDOT = 20051
912334 feet/sec YDOT = 6111
822879 meter/sec
ZDOT = -12857
902225 ZDOT = -3919
088598
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 09044
54059290
00010596 00000-0 82463-4 0 9102
2 25544 51
6361 220
1048 0008814 18
8512 341
2974 15
70924274 26501
Satellite: ISS
Catalog Number: 25544
Epoch time: 09044
54059290 = yrday
fracday
Element set: 910
Inclination: 51
6361 deg
RA of node: 220
1048 deg
Eccentricity:
0008814
Arg of perigee: 18
8512 deg
Mean anomaly: 341
2974 deg
Mean motion: 15
70924274 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2650
Checksum: 293
Coasting Arc #12 (Orbit 2665)
---------------------------------------
Vector Time (GMT): 2009/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3643068
47 A = 6737903
43 meter
Y = -5008247
45 meter E =
0020223
Z = 2623213
42 I = 51
45948
XDOT = 5521
812031 Wp = 56
86448
YDOT = -1272
344117 meter/sec RA = 214
24804 deg
ZDOT = 5221
346375 TA = 333
04602
MA = 333
15092
Ha = 197
288 n
mi
Hp = 186
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11952324
37 X = -3599537
58
Y = -16431258
03 feet Y = -5048742
87 meter
Z = 8606343
24 Z = 2605621
54
XDOT = 18116
181203 XDOT = 5510
265182
YDOT = -4174
357338 feet/sec YDOT = -1210
660388 meter/sec
ZDOT = 17130
401493 ZDOT = 5248
142973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9063
70 X = -2762
61
Y = -20347650
45 feet Y = -6201963
86 meter
Z = 8537357
97 Z = 2602186
71
XDOT = 15530
677895 XDOT = 4733
750622
YDOT = 7249
421246 feet/sec YDOT = 2209
623596 meter/sec
ZDOT = 17234
727533 ZDOT = 5253
144952
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 09045
55840124
00010596 00000-0 82463-4 0 9119
2 25544 51
6361 214
9007 0008817 23
4744 336
6819 15
70962043 26668
Satellite: ISS
Catalog Number: 25544
Epoch time: 09045
55840124 = yrday
fracday
Element set: 911
Inclination: 51
6361 deg
RA of node: 214
9007 deg
Eccentricity:
0008817
Arg of perigee: 23
4744 deg
Mean anomaly: 336
6819 deg
Mean motion: 15
70962043 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2666
Checksum: 307
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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