Date:
August 21st 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 3358)
---------------------------------------
Vector Time (GMT): 2010/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3005188
23 A = 6731468
38 meter
Y = 3998615
24 meter E =
0003945
Z = -4507737
94 I = 51
30095
XDOT = -3504
160327 Wp = 18
40301
YDOT = -6114
316098 meter/sec RA = 260
71030 deg
ZDOT = -3084
655074 TA = 220
66590
MA = 220
69536
Ha = 191
816 n
mi
Hp = 191
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9859541
43 X = -3027780
75
Y = 13118816
41 feet Y = 3964883
31 meter
Z = -14789166
45 Z = -4522391
57
XDOT = -11496
589000 XDOT = -3420
544064
YDOT = -20060
092185 feet/sec YDOT = -6153
034052 meter/sec
ZDOT = -10120
259430 ZDOT = -3101
475155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15244977
73 X = 4646669
21
Y = -5930275
63 feet Y = -1807548
01 meter
Z = -14847755
07 Z = -4525595
75
XDOT = -1389
165135 XDOT = -423
417533
YDOT = 21959
873359 feet/sec YDOT = 6693
369400 meter/sec
ZDOT = -10187
568606 ZDOT = -3105
170911
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 10232
52138062
00016717 00000-0 10270-3 0 9002
2 25544 51
6460 261
3971 0008147 271
9263 88
0965 15
71135538 33598
Satellite: ISS
Catalog Number: 25544
Epoch time: 10232
52138062 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 261
3971 deg
Eccentricity:
0008147
Arg of perigee: 271
9263 deg
Mean anomaly: 88
0965 deg
Mean motion: 15
71135538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 304
Coasting Arc #2 (Orbit 3374)
---------------------------------------
Vector Time (GMT): 2010/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3941607
31 A = 6735019
75 meter
Y = 4236066
96 meter E =
0004479
Z = 3444271
98 I = 51
31782
XDOT = -2255
488163 Wp = 73
69714
YDOT = 5791
721580 meter/sec RA = 255
52469 deg
ZDOT = -4535
873436 TA = 65
36536
MA = 65
31871
Ha = 192
517 n
mi
Hp = 191
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12931782
51 X = 3877214
58
Y = 13897857
46 feet Y = 4279784
23 meter
Z = 11300104
93 Z = 3463263
63
XDOT = -7399
895549 XDOT = -2298
050621
YDOT = 19001
711220 feet/sec YDOT = 5766
261514 meter/sec
ZDOT = -14881
474526 ZDOT = -4546
933586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3844284
40 X = -1171737
88
Y = -18543990
44 feet Y = -5652208
29 meter
Z = 11376102
51 Z = 3467436
05
XDOT = 14718
021809 XDOT = 4486
053047
YDOT = -12219
767956 feet/sec YDOT = -3724
585273 meter/sec
ZDOT = -14925
673158 ZDOT = -4549
345178
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 10233
53906194
00016717 00000-0 10270-3 0 9014
2 25544 51
6444 256
1934 0008115 276
8876 83
1363 15
71174842 33757
Satellite: ISS
Catalog Number: 25544
Epoch time: 10233
53906194 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 256
1934 deg
Eccentricity:
0008115
Arg of perigee: 276
8876 deg
Mean anomaly: 83
1363 deg
Mean motion: 15
71174842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3375
Checksum: 315
Coasting Arc #3 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2010/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 747326
05 A = 6735509
95 meter
Y = -5813786
03 meter E =
0005095
Z = 3311884
74 I = 51
32740
XDOT = 5142
234893 Wp = 69
35873
YDOT = 3320
708409 meter/sec RA = 250
43888 deg
ZDOT = 4664
911022 TA = 329
69725
MA = 329
72670
Ha = 192
744 n
mi
Hp = 191
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2451857
13 X = 796193
13
Y = -19074101
15 feet Y = -5805155
78 meter
Z = 10865763
59 Z = 3315633
82
XDOT = 16870
849386 XDOT = 5082
059125
YDOT = 10894
712628 feet/sec YDOT = 3377
875455 meter/sec
ZDOT = 15304
826189 ZDOT = 4689
745338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11628695
16 X = -3544426
28
Y = 15306253
81 feet Y = 4665346
16 meter
Z = 10880707
69 Z = 3316439
70
XDOT = -7939
783964 XDOT = -2420
046152
YDOT = -16991
828822 feet/sec YDOT = -5179
109425 meter/sec
ZDOT = 15404
200449 ZDOT = 4695
200297
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 10234
55673258
00016717 00000-0 10270-3 0 9020
2 25544 51
6438 250
9892 0008063 281
2013 78
8242 15
71158337 33916
Satellite: ISS
Catalog Number: 25544
Epoch time: 10234
55673258 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 250
9892 deg
Eccentricity:
0008063
Arg of perigee: 281
2013 deg
Mean anomaly: 78
8242 deg
Mean motion: 15
71158337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 310
Coasting Arc #4 (Orbit 3405)
---------------------------------------
Vector Time (GMT): 2010/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4709685
04 A = 6730997
24 meter
Y = -1439384
57 meter E =
0002505
Z = -4590846
34 I = 51
32423
XDOT = -686
587419 Wp = 126
60838
YDOT = -7082
674358 meter/sec RA = 245
25558 deg
ZDOT = 2924
649421 TA = 172
53283
MA = 172
52910
Ha = 192
907 n
mi
Hp = 191
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15451722
59 X = -4670938
50
Y = -4722390
31 feet Y = -1491834
49 meter
Z = -15061831
82 Z = -4613631
40
XDOT = -2252
583396 XDOT = -621
543757
YDOT = -23237
120596 feet/sec YDOT = -7089
988480 meter/sec
ZDOT = 9595
306499 ZDOT = 2921
472110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11125113
95 X = 3390934
73
Y = 11598876
50 feet Y = 3535337
56 meter
Z = -15152999
13 Z = -4618634
13
XDOT = -8439
097417 XDOT = -2572
236893
YDOT = 20614
751168 feet/sec YDOT = 6283
376156 meter/sec
ZDOT = 9582
517432 ZDOT = 2920
751313
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 10235
51078582
00016717 00000-0 10270-3 0 9037
2 25544 51
6443 246
1108 0008217 284
8186 75
2065 15
71170115 34069
Satellite: ISS
Catalog Number: 25544
Epoch time: 10235
51078582 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 246
1108 deg
Eccentricity:
0008217
Arg of perigee: 284
8186 deg
Mean anomaly: 75
2065 deg
Mean motion: 15
71170115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3406
Checksum: 290
Coasting Arc #5 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2010/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1957047
46 A = 6738869
59 meter
Y = 6206187
99 meter E =
0004584
Z = -1739840
34 I = 51
36329
XDOT = -5199
043511 Wp = 221
60277
YDOT = 48
024058 meter/sec RA = 240
15794 deg
ZDOT = -5671
623998 TA = 337
70638
MA = 337
72630
Ha = 193
200 n
mi
Hp = 191
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6420759
40 X = 1895954
96
Y = 20361509
16 feet Y = 6227731
23 meter
Z = -5708137
59 Z = -1730481
74
XDOT = -17057
229366 XDOT = -5171
642889
YDOT = 157
559245 feet/sec YDOT = -9
961719 meter/sec
ZDOT = -18607
690282 ZDOT = -5696
813944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3903910
89 X = 1189912
04
Y = -21000086
20 feet Y = -6400826
27 meter
Z = -5670617
32 Z = -1728404
16
XDOT = 13489
003307 XDOT = 4111
448208
YDOT = 7564
034968 feet/sec YDOT = 2305
517858 meter/sec
ZDOT = -18708
466494 ZDOT = -5702
340587
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 10236
52843164
00016717 00000-0 10270-3 0 9046
2 25544 51
6430 240
9062 0008119 288
5832 71
4447 15
71196945 34225
Satellite: ISS
Catalog Number: 25544
Epoch time: 10236
52843164 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 240
9062 deg
Eccentricity:
0008119
Arg of perigee: 288
5832 deg
Mean anomaly: 71
4447 deg
Mean motion: 15
71196945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 305
Coasting Arc #6 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2010/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4039424
16 A = 6728332
06 meter
Y = -1460108
46 meter E =
0006841
Z = 5183616
81 I = 51
34384
XDOT = 3697
514982 Wp = 318
34205
YDOT = 6671
712199 meter/sec RA = 234
99829 deg
ZDOT = -997
801157 TA = 141
24343
MA = 141
19434
Ha = 193
340 n
mi
Hp = 190
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13252703
94 X = 4030270
43
Y = -4790382
07 feet Y = -1414988
15 meter
Z = 17006616
85 Z = 5203217
88
XDOT = 12130
954666 XDOT = 3627
482933
YDOT = 21888
819550 feet/sec YDOT = 6712
668414 meter/sec
ZDOT = -3273
625843 ZDOT = -980
009284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13888754
60 X = -4233292
40
Y = -1735407
23 feet Y = -528952
12 meter
Z = 17085016
72 Z = 5207513
10
XDOT = -956
664751 XDOT = -291
591416
YDOT = -24008
266863 feet/sec YDOT = -7317
719740 meter/sec
ZDOT = -3202
347478 ZDOT = -976
075511
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 10237
54606403
00016717 00000-0 10270-3 0 9053
2 25544 51
6425 235
7014 0008217 293
0002 67
0292 15
71226901 34389
Satellite: ISS
Catalog Number: 25544
Epoch time: 10237
54606403 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 235
7014 deg
Eccentricity:
0008217
Arg of perigee: 293
0002 deg
Mean anomaly: 67
0292 deg
Mean motion: 15
71226901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 276
Coasting Arc #7 (Orbit 3452)
---------------------------------------
Vector Time (GMT): 2010/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4348280
46 A = 6739883
75 meter
Y = -5138895
31 meter E =
0012192
Z = -16164
35 I = 51
40186
XDOT = 3658
250034 Wp = 6
36991
YDOT = -3112
959141 meter/sec RA = 229
87356 deg
ZDOT = 6017
534572 TA = 353
45406
MA = 353
46997
Ha = 193
375 n
mi
Hp = 190
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14266012
00 X = -4290414
69
Y = -16859892
75 feet Y = -5187196
85 meter
Z = -53032
65 Z = -37147
25
XDOT = 12002
132656 XDOT = 3663
556025
YDOT = -10213
120541 feet/sec YDOT = -3072
020408 meter/sec
ZDOT = 19742
567494 ZDOT = 6035
319222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5375385
65 X = 1638417
55
Y = 21421118
94 feet Y = 6529157
05 meter
Z = -137065
51 Z = -41777
57
XDOT = -13607
118784 XDOT = -4147
449805
YDOT = 3537
715777 feet/sec YDOT = 1078
295769 meter/sec
ZDOT = 19813
675201 ZDOT = 6039
208201
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 10238
50008296
00016717 00000-0 10270-3 0 9067
2 25544 51
6427 230
8229 0008105 295
7541 64
2784 15
71295690 34531
Satellite: ISS
Catalog Number: 25544
Epoch time: 10238
50008296 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 230
8229 deg
Eccentricity:
0008105
Arg of perigee: 295
7541 deg
Mean anomaly: 64
2784 deg
Mean motion: 15
71295690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3453
Checksum: 312
Coasting Arc #8 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2010/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2097670
50 A = 6728305
10 meter
Y = 3751208
81 meter E =
0009608
Z = -5183911
56 I = 51
38255
XDOT = -5957
827177 Wp = 49
23408
YDOT = -4753
936670 meter/sec RA = 224
74980 deg
ZDOT = -1024
295852 TA = 210
92282
MA = 210
97943
Ha = 193
737 n
mi
Hp = 190
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6882121
07 X = -2114278
94
Y = 12307115
51 feet Y = 3727658
24 meter
Z = -17007583
86 Z = -5194142
54
XDOT = -19546
677091 XDOT = -5899
249169
YDOT = -15596
905085 feet/sec YDOT = -4820
233196 meter/sec
ZDOT = -3360
550696 ZDOT = -1053
096249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11370321
66 X = 3465674
04
Y = -8255450
76 feet Y = -2516261
39 meter
Z = -17048457
68 Z = -5196369
90
XDOT = 10439
755205 XDOT = 3182
037386
YDOT = 21590
216513 feet/sec YDOT = 6580
697993 meter/sec
ZDOT = -3475
864452 ZDOT = -1059
443485
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 10239
51769080
00016717 00000-0 10270-3 0 9075
2 25544 51
6423 225
6177 0008241 301
2022 58
8331 15
71256289 34694
Satellite: ISS
Catalog Number: 25544
Epoch time: 10239
51769080 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 225
6177 deg
Eccentricity:
0008241
Arg of perigee: 301
2022 deg
Mean anomaly: 58
8331 deg
Mean motion: 15
71256289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 303
Coasting Arc #9 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2010/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5784019
27 A = 6738481
92 meter
Y = 2981820
05 meter E =
0006042
Z = 1742011
91 I = 51
43996
XDOT = -920
407013 Wp = 99
42655
YDOT = 5110
738065 meter/sec RA = 219
59370 deg
ZDOT = -5676
310651 TA = 61
26222
MA = 61
20153
Ha = 193
942 n
mi
Hp = 190
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18976441
19 X = 5741783
77
Y = 9782874
19 feet Y = 3046264
37 meter
Z = 5715262
17 Z = 1770007
87
XDOT = -3019
708047 XDOT = -949
913377
YDOT = 16767
513335 feet/sec YDOT = 5100
280243 meter/sec
ZDOT = -18623
066439 ZDOT = -5680
853919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13273972
19 X = -4045906
72
Y = -16682865
38 feet Y = -5084937
37 meter
Z = 5827335
10 Z = 1776171
74
XDOT = 8304
578468 XDOT = 2531
235517
YDOT = -13136
740490 feet/sec YDOT = -4004
078501 meter/sec
ZDOT = -18641
158168 ZDOT = -5681
825010
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 10240
53528440
00016717 00000-0 10270-3 0 9083
2 25544 51
6425 220
4130 0008432 305
8272 54
2105 15
71307655 34858
Satellite: ISS
Catalog Number: 25544
Epoch time: 10240
53528440 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 220
4130 deg
Eccentricity:
0008432
Arg of perigee: 305
8272 deg
Mean anomaly: 54
2105 deg
Mean motion: 15
71307655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 275
Coasting Arc #10 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2010/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -591247
16 A = 6730584
65 meter
Y = -4866373
03 meter E =
0001904
Z = 4610337
92 I = 51
43761
XDOT = 6867
362268 Wp = 27
73045
YDOT = 1913
443846 meter/sec RA = 214
50330 deg
ZDOT = 2901
582507 TA = 33
45158
MA = 33
43955
Ha = 194
027 n
mi
Hp = 189
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1939787
27 X = -559182
75
Y = -15965790
79 feet Y = -4872805
24 meter
Z = 15125780
59 Z = 4607543
73
XDOT = 22530
716101 XDOT = 6831
360008
YDOT = 6277
702908 feet/sec YDOT = 1990
037629 meter/sec
ZDOT = 9519
627648 ZDOT = 2934
856656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4421798
17 X = -1347764
08
Y = 15474418
69 feet Y = 4716602
82 meter
Z = 15114514
74 Z = 4606904
09
XDOT = -17057
152389 XDOT = -5199
020048
YDOT = -14298
587101 feet/sec YDOT = -4358
209348 meter/sec
ZDOT = 9652
810715 ZDOT = 2942
176706
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 10241
55286468
00016717 00000-0 10270-3 0 9098
2 25544 51
6426 215
2089 0008475 308
6364 51
4039 15
71328228 35017
Satellite: ISS
Catalog Number: 25544
Epoch time: 10241
55286468 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 215
2089 deg
Eccentricity:
0008475
Arg of perigee: 308
6364 deg
Mean anomaly: 51
4039 deg
Mean motion: 15
71328228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 309
Coasting Arc #11 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2010/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5877549
87 A = 6735116
50 meter
Y = -320707
69 meter E =
0006290
Z = -3265265
23 I = 51
47857
XDOT = -2316
632310 Wp = 347
43661
YDOT = -5616
741928 meter/sec RA = 209
32835 deg
ZDOT = 4725
989071 TA = 334
24593
MA = 334
27724
Ha = 194
174 n
mi
Hp = 189
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19283300
10 X = -5857664
71
Y = -1052190
57 feet Y = -386322
87 meter
Z = -10712812
44 Z = -3293770
13
XDOT = -7600
499706 XDOT = -2276
610754
YDOT = -18427
630997 feet/sec YDOT = -5642
424003 meter/sec
ZDOT = 15505
213489 ZDOT = 4714
832202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17396206
78 X = 5302363
83
Y = 8238174
56 feet Y = 2510995
60 meter
Z = -10826891
88 Z = -3300036
65
XDOT = 758
224713 XDOT = 231
106893
YDOT = 18699
072138 feet/sec YDOT = 5699
477188 meter/sec
ZDOT = 15460
466747 ZDOT = 4712
350265
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 10242
50683450
00016717 00000-0 10270-3 0 9108
2 25544 51
6426 210
3295 0008427 313
4829 46
5631 15
71309968 35168
Satellite: ISS
Catalog Number: 25544
Epoch time: 10242
50683450 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 210
3295 deg
Eccentricity:
0008427
Arg of perigee: 313
4829 deg
Mean anomaly: 46
5631 deg
Mean motion: 15
71309968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 300
Coasting Arc #12 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2010/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3378437
95 A = 6734296
15 meter
Y = 4621360
12 meter E =
0006820
Z = -3552819
17 I = 51
50360
XDOT = -6178
738729 Wp = 355
88969
YDOT = 1093
956428 meter/sec RA = 204
25365 deg
ZDOT = -4445
283860 TA = 226
46894
MA = 226
52562
Ha = 194
404 n
mi
Hp = 189
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11084114
00 X = 3343768
95
Y = 15161942
66 feet Y = 4658945
96 meter
Z = -11656230
86 Z = -3536490
93
XDOT = -20271
452523 XDOT = -6168
917892
YDOT = 3589
095893 feet/sec YDOT = 1024
916938 meter/sec
ZDOT = -14584
264634 ZDOT = -4475
276400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4909007
95 X = -1496265
62
Y = -18170437
35 feet Y = -5538349
30 meter
Z = -11590800
40 Z = -3532875
96
XDOT = 18789
957480 XDOT = 5727
179040
YDOT = 4318
566339 feet/sec YDOT = 1316
299020 meter/sec
ZDOT = -14704
283975 ZDOT = -4481
865756
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 10243
52438767
00016717 00000-0 10270-3 0 9111
2 25544 51
6432 205
1248 0008484 317
4468 42
6035 15
71360359 35325
Satellite: ISS
Catalog Number: 25544
Epoch time: 10243
52438767 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 205
1248 deg
Eccentricity:
0008484
Arg of perigee: 317
4468 deg
Mean anomaly: 42
6035 deg
Mean motion: 15
71360359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 300
Coasting Arc #13 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2010/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4631969
75 A = 6731120
35 meter
Y = -2106170
65 meter E =
0010439
Z = 4409311
06 I = 51
52140
XDOT = 5230
069717 Wp = 17
75347
YDOT = 4579
997071 meter/sec RA = 199
08057 deg
ZDOT = -3294
651532 TA = 105
46942
MA = 105
35411
Ha = 194
484 n
mi
Hp = 189
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15196751
16 X = 4633757
44
Y = -6910008
69 feet Y = -2054363
21 meter
Z = 14466243
63 Z = 4431817
51
XDOT = 17159
021380 XDOT = 5194
471465
YDOT = 15026
237108 feet/sec YDOT = 4638
283819 meter/sec
ZDOT = -10809
224185 ZDOT = -3269
330288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16567930
05 X = -5049905
08
Y = 1256847
75 feet Y = 383087
20 meter
Z = 14556294
11 Z = 4436758
44
XDOT = -10871
295381 XDOT = -3313
570832
YDOT = -18847
175188 feet/sec YDOT = -5744
618997 meter/sec
ZDOT = -10707
790856 ZDOT = -3263
734653
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 10244
54192623
00016717 00000-0 10270-3 0 9123
2 25544 51
6432 199
9204 0008568 320
8094 39
2447 15
71378990 35489
Satellite: ISS
Catalog Number: 25544
Epoch time: 10244
54192623 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 199
9204 deg
Eccentricity:
0008568
Arg of perigee: 320
8094 deg
Mean anomaly: 39
2447 deg
Mean motion: 15
71378990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 326
Coasting Arc #14 (Orbit 3563)
---------------------------------------
Vector Time (GMT): 2010/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5557020
87 A = 6737643
06 meter
Y = -3133476
89 meter E =
0014329
Z = 2137582
21 I = 51
57255
XDOT = 4091
413685 Wp = 35
39085
YDOT = -3489
072077 meter/sec RA = 194
00130 deg
ZDOT = 5514
831040 TA = 348
53472
MA = 348
56732
Ha = 194
661 n
mi
Hp = 188
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18231695
78 X = -5531952
70
Y = -10280435
99 feet Y = -3195478
69 meter
Z = 7013065
00 Z = 2110647
13
XDOT = 13423
273245 XDOT = 4103
335072
YDOT = -11447
086866 feet/sec YDOT = -3443
252855 meter/sec
ZDOT = 18093
277691 ZDOT = 5534
735980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13862276
39 X = 4225221
84
Y = 15729618
98 feet Y = 4794387
86 meter
Z = 6905183
27 Z = 2104699
86
XDOT = -15197
949228 XDOT = -4632
334925
YDOT = 5405
871924 feet/sec YDOT = 1647
709762 meter/sec
ZDOT = 18172
900624 ZDOT = 5539
100110
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 10245
55944965
00016717 00000-0 10270-3 0 9130
2 25544 51
6433 194
7155 0008514 324
4046 35
6547 15
71409203 35647
Satellite: ISS
Catalog Number: 25544
Epoch time: 10245
55944965 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 194
7155 deg
Eccentricity:
0008514
Arg of perigee: 324
4046 deg
Mean anomaly: 35
6547 deg
Mean motion: 15
71409203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3564
Checksum: 311
Coasting Arc #15 (Orbit 3578)
---------------------------------------
Vector Time (GMT): 2010/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2316104
04 A = 6728210
45 meter
Y = 3735386
88 meter E =
0010155
Z = -5101019
43 I = 51
57100
XDOT = -7160
270640 Wp = 63
42869
YDOT = -2349
365753 meter/sec RA = 188
84934 deg
ZDOT = 1537
513873 TA = 221
31754
MA = 221
39442
Ha = 194
771 n
mi
Hp = 188
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7598766
52 X = -2332922
03
Y = 12255206
30 feet Y = 3709392
85 meter
Z = -16735628
04 Z = -5112311
78
XDOT = -23491
701575 XDOT = -7140
936343
YDOT = -7707
892889 feet/sec YDOT = -2429
328105 meter/sec
ZDOT = 5044
336855 ZDOT = 1502
776459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10962074
73 X = 3341240
38
Y = -9287149
14 feet Y = -2830723
06 meter
Z = -16780773
48 Z = -5114779
76
XDOT = 19243
613136 XDOT = 5865
453284
YDOT = 13891
306148 feet/sec YDOT = 4234
070114 meter/sec
ZDOT = 4905
214930 ZDOT = 1495
109511
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 10246
51336499
00016717 00000-0 10270-3 0 9145
2 25544 51
6436 189
8359 0008637 328
2184 31
8456 15
71415147 35799
Satellite: ISS
Catalog Number: 25544
Epoch time: 10246
51336499 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 189
8359 deg
Eccentricity:
0008637
Arg of perigee: 328
2184 deg
Mean anomaly: 31
8456 deg
Mean motion: 15
71415147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 338
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list