Date:
June 6th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14262 18 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 411)
---------------------------------------
Vector Time (GMT): 2009/156/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6398908
92 A = 6732330
97 meter
Y = -833465
92 meter E =
0015039
Z = -1914776
79 I = 51
68916
XDOT = 2287
850413 Wp = 61
57657
YDOT = 4720
645955 meter/sec RA = 6
13714 deg
ZDOT = 5631
221707 TA = 277
16726
MA = 277
33822
Ha = 194
286 n
mi
Hp = 181
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20993795
66 X = 6417055
07
Y = -2734468
24 feet Y = -761807
80 meter
Z = -6282076
09 Z = -1883646
49
XDOT = 7506
070908 XDOT = 2207
537452
YDOT = 15487
683579 feet/sec YDOT = 4745
780041 meter/sec
ZDOT = 18475
136833 ZDOT = 5642
141956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2481326
87 X = -756308
43
Y = -21061261
26 feet Y = -6419472
43 meter
Z = -6160157
76 Z = -1877616
09
XDOT = 14040
089140 XDOT = 4279
419170
YDOT = -7030
946796 feet/sec YDOT = -2143
032583 meter/sec
ZDOT = 18518
102418 ZDOT = 5644
317617
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
54808070
00010596 00000-0 82463-4 0 9003
2 25544 51
6382 6
6355 0008933 80
4486 279
7685 15
73404695 4120
Satellite: ISS
Catalog Number: 25544
Epoch time: 09156
54808070 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 6
6355 deg
Eccentricity:
0008933
Arg of perigee: 80
4486 deg
Mean anomaly: 279
7685 deg
Mean motion: 15
73404695 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 412
Checksum: 323
Coasting Arc #2 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2009/157/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2547527
41 A = 6723457
09 meter
Y = -3900602
53 meter E =
0021200
Z = -4867134
36 I = 51
62934
XDOT = 7111
246898 Wp = 77
50494
YDOT = -1725
935096 meter/sec RA = 1
04296 deg
ZDOT = -2343
002693 TA = 169
62838
MA = 169
58457
Ha = 194
232 n
mi
Hp = 181
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8358029
56 X = -2480076
92
Y = -12797252
41 feet Y = -3928712
44 meter
Z = -15968288
58 Z = -4879347
28
XDOT = 23330
862527 XDOT = 7141
400093
YDOT = -5662
516718 feet/sec YDOT = -1646
243954 meter/sec
ZDOT = -7687
016710 ZDOT = -2308
382891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12754629
81 X = -3887611
17
Y = 8331305
99 feet Y = 2539382
07 meter
Z = -16016283
17 Z = -4881763
11
XDOT = -5175
870194 XDOT = -1577
605235
YDOT = -22415
393300 feet/sec YDOT = -6832
211878 meter/sec
ZDOT = -7551
459297 ZDOT = -2301
684794
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 09157
56428601
00010596 00000-0 82463-4 0 9015
2 25544 51
6375 1
4207 0009027 84
4022 275
8170 15
73440295 4285
Satellite: ISS
Catalog Number: 25544
Epoch time: 09157
56428601 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 1
4207 deg
Eccentricity:
0009027
Arg of perigee: 84
4022 deg
Mean anomaly: 275
8170 deg
Mean motion: 15
73440295 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 428
Checksum: 290
Coasting Arc #3 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2009/158/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5978826
84 A = 6731573
01 meter
Y = 2164565
75 meter E =
0022404
Z = 2183115
83 I = 51
62778
XDOT = -3509
000258 Wp = 100
41811
YDOT = -4107
836583 meter/sec RA = 355
87227 deg
ZDOT = -5493
500102 TA = 55
11322
MA = 54
90282
Ha = 194
075 n
mi
Hp = 181
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19615573
61 X = -6013192
29
Y = 7101593
68 feet Y = 2097514
45 meter
Z = 7162453
51 Z = 2153987
37
XDOT = -11512
468038 XDOT = -3436
118269
YDOT = -13477
154143 feet/sec YDOT = -4146
667694 meter/sec
ZDOT = -18023
294299 ZDOT = -5510
370755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7539650
15 X = 2298085
37
Y = 19493012
67 feet Y = 5941470
26 meter
Z = 7048420
67 Z = 2148358
62
XDOT = -11797
455369 XDOT = -3595
864396
YDOT = 11156
550421 feet/sec YDOT = 3400
516568 meter/sec
ZDOT = -18089
542985 ZDOT = -5513
692702
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 09158
58046848
00010596 00000-0 82463-4 0 9028
2 25544 51
6379 356
2053 0008765 86
9896 273
2270 15
73509282 4446
Satellite: ISS
Catalog Number: 25544
Epoch time: 09158
58046848 = yrday
fracday
Element set: 902
Inclination: 51
6379 deg
RA of node: 356
2053 deg
Eccentricity:
0008765
Arg of perigee: 86
9896 deg
Mean anomaly: 273
2270 deg
Mean motion: 15
73509282 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 444
Checksum: 344
Coasting Arc #4 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2009/159/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3545321
82 A = 6723848
22 meter
Y = 3212439
18 meter E =
0015985
Z = 4712783
48 I = 51
57146
XDOT = -6479
342602 Wp = 103
62239
YDOT = 3204
920525 meter/sec RA = 350
77727 deg
ZDOT = 2678
375446 TA = 319
99068
MA = 320
10833
Ha = 194
028 n
mi
Hp = 181
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11631633
25 X = 3486242
32
Y = 10539498
62 feet Y = 3251753
77 meter
Z = 15461888
06 Z = 4729863
88
XDOT = -21257
685701 XDOT = -6527
710131
YDOT = 10514
831119 feet/sec YDOT = 3132
193761 meter/sec
ZDOT = 8787
321016 ZDOT = 2646
781789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10074887
75 X = 3070825
78
Y = -11949685
89 feet Y = -3642264
26 meter
Z = 15528926
23 Z = 4733216
71
XDOT = 10478
388556 XDOT = 3193
812832
YDOT = 20140
946021 feet/sec YDOT = 6138
960347 meter/sec
ZDOT = 8663
664576 ZDOT = 2640
684963
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 09159
59663394
00010596 00000-0 82463-4 0 9032
2 25544 51
6371 350
9899 0008891 91
7685 268
4496 15
73493782 4608
Satellite: ISS
Catalog Number: 25544
Epoch time: 09159
59663394 = yrday
fracday
Element set: 903
Inclination: 51
6371 deg
RA of node: 350
9899 deg
Eccentricity:
0008891
Arg of perigee: 91
7685 deg
Mean anomaly: 268
4496 deg
Mean motion: 15
73493782 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 460
Checksum: 370
Coasting Arc #5 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2009/160/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5272640
90 A = 6730909
99 meter
Y = -3379781
31 meter E =
0013262
Z = -2472643
53 I = 51
56682
XDOT = 4535
831536 Wp = 77
79576
YDOT = 3198
973960 meter/sec RA = 345
59787 deg
ZDOT = 5326
330141 TA = 254
24797
MA = 254
39427
Ha = 194
106 n
mi
Hp = 181
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17298690
61 X = 5322053
97
Y = -11088521
35 feet Y = -3320542
79 meter
Z = -8112347
55 Z = -2446909
65
XDOT = 14881
337060 XDOT = 4473
848581
YDOT = 10495
321392 feet/sec YDOT = 3249
348660 meter/sec
ZDOT = 17474
836421 ZDOT = 5348
215314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12055065
17 X = -3674383
86
Y = -16688290
01 feet Y = -5086590
79 meter
Z = -8011651
86 Z = -2441951
49
XDOT = 8423
107988 XDOT = 2567
363315
YDOT = -14472
390356 feet/sec YDOT = -4411
184581 meter/sec
ZDOT = 17560
701606 ZDOT = 5352
501849
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 09160
54926824
00010596 00000-0 82463-4 0 9040
2 25544 51
6376 346
1003 0008995 96
1254 264
0934 15
73532020 4757
Satellite: ISS
Catalog Number: 25544
Epoch time: 09160
54926824 = yrday
fracday
Element set: 904
Inclination: 51
6376 deg
RA of node: 346
1003 deg
Eccentricity:
0008995
Arg of perigee: 96
1254 deg
Mean anomaly: 264
0934 deg
Mean motion: 15
73532020 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 475
Checksum: 307
Coasting Arc #6 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2009/161/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4308514
39 A = 6724075
11 meter
Y = -2360806
68 meter E =
0019115
Z = -4608319
85 I = 51
51644
XDOT = 5552
610698 Wp = 83
12574
YDOT = -4434
889779 meter/sec RA = 340
50247 deg
ZDOT = -2927
541217 TA = 157
79813
MA = 157
71525
Ha = 194
012 n
mi
Hp = 181
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14135545
89 X = -4259408
89
Y = -7745428
74 feet Y = -2408711
57 meter
Z = -15119159
62 Z = -4629131
74
XDOT = 18217
226699 XDOT = 5616
011136
YDOT = -14550
163318 feet/sec YDOT = -4372
442202 meter/sec
ZDOT = -9604
794020 ZDOT = -2900
413523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6686243
72 X = -2037967
09
Y = 14581645
35 feet Y = 4444485
50 meter
Z = -15200791
94 Z = -4633201
38
XDOT = -14797
759832 XDOT = -4510
357197
YDOT = -16659
684070 feet/sec YDOT = -5077
871704 meter/sec
ZDOT = -9498
676097 ZDOT = -2895
196474
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 09161
56539122
00010596 00000-0 82463-4 0 9055
2 25544 51
6381 340
8854 0009065 99
2720 260
9468 15
73579278 4910
Satellite: ISS
Catalog Number: 25544
Epoch time: 09161
56539122 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 340
8854 deg
Eccentricity:
0009065
Arg of perigee: 99
2720 deg
Mean anomaly: 260
9468 deg
Mean motion: 15
73579278 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 491
Checksum: 335
Coasting Arc #7 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2009/162/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4392789
58 A = 6730357
56 meter
Y = 4339495
69 meter E =
0022612
Z = 2651550
53 I = 51
50917
XDOT = -5268
986560 Wp = 102
46569
YDOT = -2133
461101 meter/sec RA = 335
31560 deg
ZDOT = -5205
073492 TA = 47
26164
MA = 47
07154
Ha = 193
969 n
mi
Hp = 181
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14412039
31 X = -4453868
77
Y = 14237190
59 feet Y = 4290030
98 meter
Z = 8699312
78 Z = 2630062
84
XDOT = -17286
701311 XDOT = -5219
453035
YDOT = -6999
544294 feet/sec YDOT = -2192
104120 meter/sec
ZDOT = -17077
012770 ZDOT = -5230
550185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15495041
44 X = 4722888
63
Y = 13105837
55 feet Y = 3994659
28 meter
Z = 8615290
40 Z = 2625940
51
XDOT = -4450
099565 XDOT = -1356
390347
YDOT = 16623
363749 feet/sec YDOT = 5066
801271 meter/sec
ZDOT = -17176
917237 ZDOT = -5235
524374
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 09162
58149284
00010596 00000-0 82463-4 0 9065
2 25544 51
6375 335
6692 0008887 103
5794 256
6359 15
73586971 5073
Satellite: ISS
Catalog Number: 25544
Epoch time: 09162
58149284 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 335
6692 deg
Eccentricity:
0008887
Arg of perigee: 103
5794 deg
Mean anomaly: 256
6359 deg
Mean motion: 15
73586971 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 507
Checksum: 358
Coasting Arc #8 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2009/163/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4834056
33 A = 6724344
87 meter
Y = 1334271
26 meter E =
0017653
Z = 4468681
92 I = 51
46411
XDOT = -4442
779981 Wp = 109
85093
YDOT = 5445
986727 meter/sec RA = 330
21804 deg
ZDOT = 3163
952096 TA = 308
41618
MA = 308
57455
Ha = 193
684 n
mi
Hp = 181
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15859764
87 X = 4797069
06
Y = 4377530
37 feet Y = 1388120
99 meter
Z = 14661029
91 Z = 4492076
03
XDOT = -14576
049807 XDOT = -4518
717563
YDOT = 17867
410521 feet/sec YDOT = 5395
879878 meter/sec
ZDOT = 10380
420264 ZDOT = 3142
185575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2645773
60 X = 806431
79
Y = -16155404
14 feet Y = -4924167
18 meter
Z = 14752745
89 Z = 4496636
95
XDOT = 18167
859066 XDOT = 5537
563443
YDOT = 12424
492739 feet/sec YDOT = 3786
985387 meter/sec
ZDOT = 10295
352613 ZDOT = 3138
023477
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 09163
59757269
00010596 00000-0 82463-4 0 9076
2 25544 51
6383 330
4540 0008829 107
6159 252
5968 15
73655924 5237
Satellite: ISS
Catalog Number: 25544
Epoch time: 09163
59757269 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 330
4540 deg
Eccentricity:
0008829
Arg of perigee: 107
6159 deg
Mean anomaly: 252
5968 deg
Mean motion: 15
73655924 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 523
Checksum: 343
Coasting Arc #9 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2009/164/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3339370
45 A = 6729647
97 meter
Y = -5106947
27 meter E =
0012517
Z = -2850190
68 I = 51
45785
XDOT = 5715
747734 Wp = 93
96932
YDOT = 922
695352 meter/sec RA = 325
02617 deg
ZDOT = 5061
710375 TA = 233
27302
MA = 233
38805
Ha = 193
805 n
mi
Hp = 181
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10955939
80 X = 3410074
67
Y = -16755076
36 feet Y = -5069208
75 meter
Z = -9351019
29 Z = -2833797
05
XDOT = 18752
453196 XDOT = 5680
416409
YDOT = 3027
215721 feet/sec YDOT = 986
413922 meter/sec
ZDOT = 16606
661336 ZDOT = 5089
391692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18002335
99 X = -5487112
01
Y = -8824646
25 feet Y = -2689752
18 meter
Z = -9286995
20 Z = -2830676
14
XDOT = 23
433563 XDOT = 7
142550
YDOT = -17575
296867 feet/sec YDOT = -5356
950485 meter/sec
ZDOT = 16715
160092 ZDOT = 5094
780796
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 09164
55012988
00010596 00000-0 82463-4 0 9086
2 25544 51
6395 325
5651 0008932 110
5710 249
6412 15
73663613 5380
Satellite: ISS
Catalog Number: 25544
Epoch time: 09164
55012988 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 325
5651 deg
Eccentricity:
0008932
Arg of perigee: 110
5710 deg
Mean anomaly: 249
6412 deg
Mean motion: 15
73663613 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 538
Checksum: 316
Coasting Arc #10 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2009/165/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5093754
37 A = 6724557
29 meter
Y = -296263
22 meter E =
0016853
Z = -4394556
48 I = 51
41760
XDOT = 3206
752262 Wp = 90
46748
YDOT = -6152
125531 meter/sec RA = 319
92638 deg
ZDOT = -3313
293077 TA = 146
13058
MA = 146
02284
Ha = 193
645 n
mi
Hp = 181
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16711792
54 X = -5068714
99
Y = -971992
18 feet Y = -353083
99 meter
Z = -14417836
22 Z = -4419241
13
XDOT = 10520
840753 XDOT = 3291
403397
YDOT = -20184
138881 feet/sec YDOT = -6115
792022 meter/sec
ZDOT = -10870
384110 ZDOT = -3297
509856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1403829
82 X = 427887
33
Y = 16596968
82 feet Y = 5058756
10 meter
Z = -14514567
43 Z = -4424040
15
XDOT = -20274
729340 XDOT = -6179
737503
YDOT = -7706
146005 feet/sec YDOT = -2348
833302 meter/sec
ZDOT = -10808
800895 ZDOT = -3294
522513
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 09165
56616879
00010596 00000-0 82463-4 0 9098
2 25544 51
6396 320
3498 0008802 113
9419 246
2667 15
73694783 5547
Satellite: ISS
Catalog Number: 25544
Epoch time: 09165
56616879 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 320
3498 deg
Eccentricity:
0008802
Arg of perigee: 113
9419 deg
Mean anomaly: 246
2667 deg
Mean motion: 15
73694783 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 554
Checksum: 355
Coasting Arc #11 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2009/166/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2239146
29 A = 6729246
56 meter
Y = 5605144
81 meter E =
0021825
Z = 2949759
57 I = 51
41119
XDOT = -5877
452335 Wp = 105
27604
YDOT = 286
162236 meter/sec RA = 314
72859 deg
ZDOT = -4980
438503 TA = 40
54788
MA = 40
38550
Ha = 193
631 n
mi
Hp = 181
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7346280
50 X = -2315986
99
Y = 18389582
72 feet Y = 5579675
38 meter
Z = 9677688
87 Z = 2938695
80
XDOT = -19282
980102 XDOT = -5856
021296
YDOT = 938
852479 feet/sec YDOT = 220
557555 meter/sec
ZDOT = -16340
021336 ZDOT = -5008
939150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19334133
89 X = 5893044
01
Y = 4378172
91 feet Y = 1334467
10 meter
Z = 9634579
41 Z = 2936619
80
XDOT = 4302
607021 XDOT = 1311
434620
YDOT = 17383
384331 feet/sec YDOT = 5298
455544 meter/sec
ZDOT = -16451
678137 ZDOT = -5014
471496
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 09166
58218684
00010596 00000-0 82463-4 0 9105
2 25544 51
6394 315
1337 0008811 117
9272 242
2784 15
73711698 5709
Satellite: ISS
Catalog Number: 25544
Epoch time: 09166
58218684 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 315
1337 deg
Eccentricity:
0008811
Arg of perigee: 117
9272 deg
Mean anomaly: 242
2784 deg
Mean motion: 15
73711698 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 570
Checksum: 324
Coasting Arc #12 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2009/167/13:03:56
106
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5107675
88 A = 6724633
27 meter
Y = -791643
73 meter E =
0018194
Z = 4292146
17 I = 51
37753
XDOT = -1895
520435 Wp = 114
59085
YDOT = 6620
722096 meter/sec RA = 309
62649 deg
ZDOT = 3457
867662 TA = 300
26568
MA = 300
44563
Ha = 193
307 n
mi
Hp = 181
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16757466
81 X = 5095297
96
Y = -2597256
34 feet Y = -734596
44 meter
Z = 14081844
39 Z = 4316929
26
XDOT = -6218
899064 XDOT = -1986
211396
YDOT = 21721
529185 feet/sec YDOT = 6599
017781 meter/sec
ZDOT = 11344
710176 ZDOT = 3448
439672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5495656
94 X = -1675076
23
Y = -15956596
82 feet Y = -4863570
71 meter
Z = 14178912
11 Z = 4321732
41
XDOT = 21325
806838 XDOT = 6500
105924
YDOT = 2758
205055 feet/sec YDOT = 840
700901 meter/sec
ZDOT = 11308
057503 ZDOT = 3446
695927
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 09167
59818107
00010596 00000-0 82463-4 0 9114
2 25544 51
6403 309
9183 0008654 121
6787 238
5221 15
73792634 5868
Satellite: ISS
Catalog Number: 25544
Epoch time: 09167
59818107 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 309
9183 deg
Eccentricity:
0008654
Arg of perigee: 121
6787 deg
Mean anomaly: 238
5221 deg
Mean motion: 15
73792634 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 586
Checksum: 332
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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