Date:
May 31st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 303)
---------------------------------------
Vector Time (GMT): 2009/149/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2882645
29 A = 6731175
29 meter
Y = -5429083
90 meter E =
0012091
Z = -2757261
52 I = 51
86773
XDOT = 5679
293072 Wp = 75
66601
YDOT = -399
250867 meter/sec RA = 41
41604 deg
ZDOT = -5167
304279 TA = 135
68725
MA = 135
59040
Ha = 194
553 n
mi
Hp = 182
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9457497
66 X = -2808327
87
Y = -17811955
05 feet Y = -5460903
44 meter
Z = -9046133
59 Z = -2771085
56
XDOT = 18632
851286 XDOT = 5708
437225
YDOT = -1309
878173 feet/sec YDOT = -335
578074 meter/sec
ZDOT = -16953
098028 ZDOT = -5139
643603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9251795
97 X = -2819947
41
Y = 17892093
09 feet Y = 5453509
97 meter
Z = -9100539
23 Z = -2773844
36
XDOT = -10466
866215 XDOT = -3190
300822
YDOT = -13953
776076 feet/sec YDOT = -4253
110948 meter/sec
ZDOT = -16844
747238 ZDOT = -5134
278958
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
68811709
00010596 00000-0 82463-4 0 9003
2 25544 51
6385 41
8232 0009332 55
1592 305
0448 15
73177262 3046
Satellite: ISS
Catalog Number: 25544
Epoch time: 09149
68811709 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 41
8232 deg
Eccentricity:
0009332
Arg of perigee: 55
1592 deg
Mean anomaly: 305
0448 deg
Mean motion: 15
73177262 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 304
Checksum: 299
Coasting Arc #2 (Orbit 319)
---------------------------------------
Vector Time (GMT): 2009/150/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4753727
74 A = 6725215
36 meter
Y = 1032459
36 meter E =
0017432
Z = 4634605
35 I = 51
82461
XDOT = -4109
441793 Wp = 61
23877
YDOT = -5839
182540 meter/sec RA = 36
25545 deg
ZDOT = -2897
865708 TA = 57
42430
MA = 57
25608
Ha = 194
627 n
mi
Hp = 182
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15596219
62 X = -4787433
63
Y = 3387333
87 feet Y = 979111
44 meter
Z = 15205398
13 Z = 4611429
99
XDOT = -13482
420581 XDOT = -4029
764343
YDOT = -19157
423032 feet/sec YDOT = -5884
690905 meter/sec
ZDOT = -9507
433425 ZDOT = -2917
636465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11923656
10 X = 3634330
38
Y = 10737507
01 feet Y = 3272792
14 meter
Z = 15114648
45 Z = 4606944
85
XDOT = -6897
539520 XDOT = -2102
370046
YDOT = 21228
207094 feet/sec YDOT = 6470
357522 meter/sec
ZDOT = -9585
154407 ZDOT = -2921
555063
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
70447378
00010596 00000-0 82463-4 0 9016
2 25544 51
6386 36
6088 0009167 59
2125 300
9939 15
73198879 3205
Satellite: ISS
Catalog Number: 25544
Epoch time: 09150
70447378 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 36
6088 deg
Eccentricity:
0009167
Arg of perigee: 59
2125 deg
Mean anomaly: 300
9939 deg
Mean motion: 15
73198879 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 320
Checksum: 331
Coasting Arc #3 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2009/151/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4244982
44 A = 6732003
06 meter
Y = 4677782
05 meter E =
0023069
Z = 2294696
13 I = 51
82281
XDOT = -5093
611128 Wp = 68
86725
YDOT = 1929
642974 meter/sec RA = 31
18034 deg
ZDOT = 5453
571394 TA = 316
87635
MA = 317
05683
Ha = 194
462 n
mi
Hp = 181
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13927107
74 X = 4181211
94
Y = 15347053
96 feet Y = 4724895
14 meter
Z = 7528530
62 Z = 2315163
88
XDOT = -16711
322600 XDOT = -5141
302705
YDOT = 6330
849652 feet/sec YDOT = 1872
416055 meter/sec
ZDOT = 17892
294600 ZDOT = 5428
710887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3974728
86 X = 1211497
36
Y = -20309626
72 feet Y = -6190374
23 meter
Z = 7608926
43 Z = 2319200
78
XDOT = 13659
976271 XDOT = 4163
560768
YDOT = 9383
394461 feet/sec YDOT = 2860
058632 meter/sec
ZDOT = 17794
984201 ZDOT = 5423
911185
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
72080978
00010596 00000-0 82463-4 0 9029
2 25544 51
6381 31
3944 0009171 63
7781 296
4323 15
73242137 3366
Satellite: ISS
Catalog Number: 25544
Epoch time: 09151
72080978 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 31
3944 deg
Eccentricity:
0009171
Arg of perigee: 63
7781 deg
Mean anomaly: 296
4323 deg
Mean motion: 15
73242137 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 336
Checksum: 305
Coasting Arc #4 (Orbit 350)
---------------------------------------
Vector Time (GMT): 2009/152/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4074792
57 A = 6724137
69 meter
Y = -2270966
05 meter E =
0019986
Z = -4859917
15 I = 51
77061
XDOT = 5513
315257 Wp = 89
93127
YDOT = 4789
428195 meter/sec RA = 26
02179 deg
ZDOT = 2393
068767 TA = 203
37648
MA = 203
46747
Ha = 194
522 n
mi
Hp = 181
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13368742
01 X = 4123492
83
Y = -7450676
02 feet Y = -2225126
57 meter
Z = -15944610
06 Z = -4840003
57
XDOT = 18088
304650 XDOT = 5447
724110
YDOT = 15713
347098 feet/sec YDOT = 4850
714337 meter/sec
ZDOT = 7851
275481 ZDOT = 2419
693809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14135554
66 X = -4308517
06
Y = -6074576
19 feet Y = -1851530
82 meter
Z = -15866696
09 Z = -4836168
97
XDOT = 923
271559 XDOT = 281
413171
YDOT = -22855
979699 feet/sec YDOT = -6966
502612 meter/sec
ZDOT = 7955
792433 ZDOT = 2424
925533
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
67360641
00010596 00000-0 82463-4 0 9033
2 25544 51
6384 26
5061 0009246 67
8998 292
3146 15
73266570 3515
Satellite: ISS
Catalog Number: 25544
Epoch time: 09152
67360641 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 26
5061 deg
Eccentricity:
0009246
Arg of perigee: 67
8998 deg
Mean anomaly: 292
3146 deg
Mean motion: 15
73266570 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 351
Checksum: 318
Coasting Arc #5 (Orbit 366)
---------------------------------------
Vector Time (GMT): 2009/153/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5324902
53 A = 6732437
44 meter
Y = -3651466
02 meter E =
0013346
Z = -1913795
50 I = 51
77252
XDOT = 4176
925663 Wp = 99
35978
YDOT = -3155
554385 meter/sec RA = 20
93765 deg
ZDOT = -5636
445924 TA = 101
84880
MA = 101
69909
Ha = 194
432 n
mi
Hp = 181
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17470152
67 X = -5274378
48
Y = -11979875
38 feet Y = -3710729
49 meter
Z = -6278856
64 Z = -1939541
86
XDOT = 13703
824354 XDOT = 4239
282330
YDOT = -10352
868718 feet/sec YDOT = -3108
496304 meter/sec
ZDOT = -18492
276653 ZDOT = -5616
003043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1574596
93 X = 479937
14
Y = 21094206
07 feet Y = 6429514
01 meter
Z = -6379874
93 Z = -1944585
88
XDOT = -15181
721680 XDOT = -4627
388768
YDOT = -4400
958338 feet/sec YDOT = -1341
412101 meter/sec
ZDOT = -18412
326752 ZDOT = -5612
077194
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
68990138
00010596 00000-0 82463-4 0 9046
2 25544 51
6387 21
2923 0009300 70
5837 289
6330 15
73328635 3673
Satellite: ISS
Catalog Number: 25544
Epoch time: 09153
68990138 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 21
2923 deg
Eccentricity:
0009300
Arg of perigee: 70
5837 deg
Mean anomaly: 289
6330 deg
Mean motion: 15
73328635 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 367
Checksum: 319
Coasting Arc #6 (Orbit 382)
---------------------------------------
Vector Time (GMT): 2009/154/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3162565
22 A = 6723409
60 meter
Y = 3197611
64 meter E =
0014911
Z = 4987633
43 I = 51
71288
XDOT = -6601
644897 Wp = 67
52458
YDOT = -3467
512404 meter/sec RA = 15
78081 deg
ZDOT = -1952
714678 TA = 41
36063
MA = 41
24782
Ha = 194
597 n
mi
Hp = 181
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10375870
14 X = -3222315
78
Y = 10490851
84 feet Y = 3161911
28 meter
Z = 16363626
74 Z = 4972124
72
XDOT = -21658
939950 XDOT = -6552
893860
YDOT = -11376
353032 feet/sec YDOT = -3541
063026 meter/sec
ZDOT = -6406
544220 ZDOT = -1984
667967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14761336
52 X = 4499255
37
Y = 1341597
25 feet Y = 408918
84 meter
Z = 16303005
69 Z = 4969156
13
XDOT = 5177
047596 XDOT = 1577
964107
YDOT = 22821
519485 feet/sec YDOT = 6955
999139 meter/sec
ZDOT = -6531
863855 ZDOT = -1990
912103
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
70617785
00010596 00000-0 82463-4 0 9055
2 25544 51
6382 16
0780 0009225 75
7852 284
4335 15
73297317 3839
Satellite: ISS
Catalog Number: 25544
Epoch time: 09154
70617785 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 16
0780 deg
Eccentricity:
0009225
Arg of perigee: 75
7852 deg
Mean anomaly: 284
4335 deg
Mean motion: 15
73297317 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 383
Checksum: 324
Coasting Arc #7 (Orbit 398)
---------------------------------------
Vector Time (GMT): 2009/155/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6117746
82 A = 6732948
81 meter
Y = 2354716
52 meter E =
0022968
Z = 1494428
29 I = 51
71782
XDOT = -3005
570764 Wp = 68
67344
YDOT = 4089
357455 meter/sec RA = 10
68613 deg
ZDOT = 5797
620702 TA = 307
77539
MA = 307
98320
Ha = 194
354 n
mi
Hp = 181
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20071347
84 X = 6083701
52
Y = 7725447
90 feet Y = 2422938
16 meter
Z = 4902979
94 Z = 1524066
42
XDOT = -9860
796470 XDOT = -3079
239499
YDOT = 13416
527082 feet/sec YDOT = 4055
334646 meter/sec
ZDOT = 19021
065296 ZDOT = 5782
841069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7225597
95 X = -2202362
25
Y = -20228181
49 feet Y = -6165549
72 meter
Z = 5019180
13 Z = 1529846
10
XDOT = 15197
985904 XDOT = 4632
346104
YDOT = -673
479208 feet/sec YDOT = -205
276463 meter/sec
ZDOT = 18963
332707 ZDOT = 5780
023809
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
72243098
00010596 00000-0 82463-4 0 9061
2 25544 51
6391 10
8641 0009155 79
9303 280
2893 15
73374451 3991
Satellite: ISS
Catalog Number: 25544
Epoch time: 09155
72243098 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 10
8641 deg
Eccentricity:
0009155
Arg of perigee: 79
9303 deg
Mean anomaly: 280
2893 deg
Mean motion: 15
73374451 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 399
Checksum: 322
Coasting Arc #8 (Orbit 413)
---------------------------------------
Vector Time (GMT): 2009/156/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2076002
61 A = 6722641
46 meter
Y = -3863670
41 meter E =
0022681
Z = -5114480
28 I = 51
65420
XDOT = 7285
091192 Wp = 93
98625
YDOT = 1911
487199 meter/sec RA = 5
53233 deg
ZDOT = 1517
281323 TA = 190
57418
MA = 190
62195
Ha = 194
368 n
mi
Hp = 181
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6811032
18 X = 2143898
11
Y = -12676084
02 feet Y = -3840074
85 meter
Z = -16779790
94 Z = -5104230
64
XDOT = 23901
217820 XDOT = 7255
804385
YDOT = 6271
283460 feet/sec YDOT = 1992
789334 meter/sec
ZDOT = 4977
957097 ZDOT = 1552
602007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14058971
59 X = -4285174
54
Y = 3280150
01 feet Y = 999789
72 meter
Z = -16739790
42 Z = -5102288
12
XDOT = -10967
160129 XDOT = -3342
790407
YDOT = -20966
106206 feet/sec YDOT = -6390
469172 meter/sec
ZDOT = 5116
399232 ZDOT = 1559
478486
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
67515114
00010596 00000-0 82463-4 0 9078
2 25544 51
6396 5
9765 0009196 83
3013 276
9196 15
73393443 4148
Satellite: ISS
Catalog Number: 25544
Epoch time: 09156
67515114 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 5
9765 deg
Eccentricity:
0009196
Arg of perigee: 83
3013 deg
Mean anomaly: 276
9196 deg
Mean motion: 15
73393443 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 414
Checksum: 326
Coasting Arc #9 (Orbit 429)
---------------------------------------
Vector Time (GMT): 2009/157/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6553873
07 A = 6733103
34 meter
Y = -981275
59 meter E =
0016158
Z = -1179136
05 I = 51
65992
XDOT = 1741
628741 Wp = 113
90010
YDOT = -4642
657822 meter/sec RA =
42560 deg
ZDOT = -5886
373309 TA = 79
00552
MA = 78
82380
Ha = 194
240 n
mi
Hp = 181
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21502208
22 X = -6536685
08
Y = -3219408
11 feet Y = -1054468
50 meter
Z = -3868556
58 Z = -1210933
59
XDOT = 5714
005057 XDOT = 1822
009564
YDOT = -15231
817002 feet/sec YDOT = -4622
731386 meter/sec
ZDOT = -19312
248390 ZDOT = -5877
717988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12202823
03 X = 3719420
46
Y = 17967221
34 feet Y = 5476409
06 meter
Z = -3993162
22 Z = -1217115
85
XDOT = -13834
240911 XDOT = -4216
676630
YDOT = 5160
440327 feet/sec YDOT = 1572
902212 meter/sec
ZDOT = -19278
519127 ZDOT = -5876
092630
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
69136452
00010596 00000-0 82463-4 0 9086
2 25544 51
6391
7609 0009136 86
0575 274
1632 15
73446100 4302
Satellite: ISS
Catalog Number: 25544
Epoch time: 09157
69136452 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node:
7609 deg
Eccentricity:
0009136
Arg of perigee: 86
0575 deg
Mean anomaly: 274
1632 deg
Mean motion: 15
73446100 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 430
Checksum: 298
Coasting Arc #10 (Orbit 445)
---------------------------------------
Vector Time (GMT): 2009/158/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -935456
41 A = 6722195
31 meter
Y = 4186298
72 meter E =
0012688
Z = 5165385
50 I = 51
59371
XDOT = -7618
545346 Wp = 79
30085
YDOT = -281
970617 meter/sec RA = 355
27241 deg
ZDOT = -1146
513530 TA = 21
66576
MA = 21
61213
Ha = 194
358 n
mi
Hp = 181
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3069082
72 X = -1007291
51
Y = 13734575
85 feet Y = 4175435
24 meter
Z = 16946802
82 Z = 5160667
34
XDOT = -24995
227512 XDOT = -7609
256470
YDOT = -925
100449 feet/sec YDOT = -367
113477 meter/sec
ZDOT = -3761
527328 ZDOT = -1183
502242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12118965
67 X = 3693860
74
Y = -7197867
95 feet Y = -2193910
15 meter
Z = 16928477
09 Z = 5159799
82
XDOT = 16057
452338 XDOT = 4894
311473
YDOT = 17812
054775 feet/sec YDOT = 5429
114295 meter/sec
ZDOT = -3906
447030 ZDOT = -1190
685055
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
70755965
00010596 00000-0 82463-4 0 9096
2 25544 51
6397 355
5467 0009190 90
2057 270
0159 15
73424908 4461
Satellite: ISS
Catalog Number: 25544
Epoch time: 09158
70755965 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 355
5467 deg
Eccentricity:
0009190
Arg of perigee: 90
2057 deg
Mean anomaly: 270
0159 deg
Mean motion: 15
73424908 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 446
Checksum: 337
Coasting Arc #11 (Orbit 461)
---------------------------------------
Vector Time (GMT): 2009/159/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6657026
26 A = 6733281
28 meter
Y = -488525
77 meter E =
0021384
Z = 828707
42 I = 51
60342
XDOT = -399
502002 Wp = 69
57174
YDOT = 4862
835670 meter/sec RA = 350
15642 deg
ZDOT = 5959
606658 TA = 299
47296
MA = 299
68613
Ha = 194
165 n
mi
Hp = 181
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21840637
33 X = 6657968
54
Y = -1602774
84 feet Y = -414077
91 meter
Z = 2718856
37 Z = 861049
60
XDOT = -1310
702107 XDOT = -482
800180
YDOT = 15954
185268 feet/sec YDOT = 4857
901270 meter/sec
ZDOT = 19552
515281 ZDOT = 5957
464507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16485143
71 X = -5024671
80
Y = -14391573
89 feet Y = -4386551
72 meter
Z = 2845548
10 Z = 867323
06
XDOT = 11296
497599 XDOT = 3443
172468
YDOT = -9003
398105 feet/sec YDOT = -2744
235742 meter/sec
ZDOT = 19544
305682 ZDOT = 5957
104372
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
72373036
00010596 00000-0 82463-4 0 9106
2 25544 51
6408 350
3324 0009082 94
1853 266
0348 15
73499149 4628
Satellite: ISS
Catalog Number: 25544
Epoch time: 09159
72373036 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 350
3324 deg
Eccentricity:
0009082
Arg of perigee: 94
1853 deg
Mean anomaly: 266
0348 deg
Mean motion: 15
73499149 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 462
Checksum: 314
Coasting Arc #12 (Orbit 476)
---------------------------------------
Vector Time (GMT): 2009/160/15:53:07
067
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -204607
21 A = 6721661
62 meter
Y = -4244964
60 meter E =
0023699
Z = -5228143
53 I = 51
53555
XDOT = 7519
581494 Wp = 96
29377
YDOT = -1352
523206 meter/sec RA = 345
00521 deg
ZDOT = 804
459902 TA = 181
38840
MA = 181
39499
Ha = 194
081 n
mi
Hp = 181
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -671283
50 X = -131726
70
Y = -13927049
20 feet Y = -4246844
11 meter
Z = -17152701
89 Z = -5228961
33
XDOT = 24670
542959 XDOT = 7530
238841
YDOT = -4437
412092 feet/sec YDOT = -1268
375425 meter/sec
ZDOT = 2639
304139 ZDOT = 841
015682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9324299
25 X = -2842046
41
Y = 10361241
72 feet Y = 3158106
48 meter
Z = -17156066
46 Z = -5229169
06
XDOT = -19980
129554 XDOT = -6089
943488
YDOT = -13376
430346 feet/sec YDOT = -4077
135970 meter/sec
ZDOT = 2782
476275 ZDOT = 848
098769
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
67637324
00010596 00000-0 82463-4 0 9116
2 25544 51
6409 345
4445 0009028 96
9973 263
2217 15
73539207 4771
Satellite: ISS
Catalog Number: 25544
Epoch time: 09160
67637324 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 345
4445 deg
Eccentricity:
0009028
Arg of perigee: 96
9973 deg
Mean anomaly: 263
2217 deg
Mean motion: 15
73539207 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 477
Checksum: 327
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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