Date:
August 26th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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 3437)
---------------------------------------
Vector Time (GMT): 2010/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4043075
24 A = 6728304
59 meter
Y = -1453646
46 meter E =
0006874
Z = 5182586
74 I = 51
34258
XDOT = 3692
087406 Wp = 318
19724
YDOT = 6673
751915 meter/sec RA = 235
00228 deg
ZDOT = -1004
115382 TA = 141
44951
MA = 141
40041
Ha = 193
327 n
mi
Hp = 190
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13264682
56 X = 4033853
99
Y = -4769181
29 feet Y = -1408485
70 meter
Z = 17003237
34 Z = 5202205
38
XDOT = 12113
147658 XDOT = 3622
063624
YDOT = 21895
511533 feet/sec YDOT = 6714
647482 meter/sec
ZDOT = -3294
341803 ZDOT = -986
349855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13889763
50 X = -4233599
91
Y = -1759746
77 feet Y = -536370
82 meter
Z = 17081707
60 Z = 5206504
48
XDOT = -939
650216 XDOT = -286
405386
YDOT = -24006
083075 feet/sec YDOT = -7317
054121 meter/sec
ZDOT = -3223
168825 ZDOT = -982
421858
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
54605277
00016717 00000-0 10270-3 0 9006
2 25544 51
6414 235
7056 0008258 292
8948 67
1341 15
71238105 34389
Satellite: ISS
Catalog Number: 25544
Epoch time: 10237
54605277 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 235
7056 deg
Eccentricity:
0008258
Arg of perigee: 292
8948 deg
Mean anomaly: 67
1341 deg
Mean motion: 15
71238105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 309
Coasting Arc #2 (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 = -4341501
02 A = 6739833
15 meter
Y = -5144577
63 meter E =
0012191
Z = -5656
05 I = 51
40059
XDOT = 3668
484300 Wp = 6
30681
YDOT = -3101
083157 meter/sec RA = 229
87746 deg
ZDOT = 6017
475920 TA = 353
63159
MA = 353
64708
Ha = 193
350 n
mi
Hp = 190
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14243769
76 X = -4283623
27
Y = -16878535
53 feet Y = -5192803
28 meter
Z = -18556
59 Z = -26605
98
XDOT = 12035
709645 XDOT = 3673
657016
YDOT = -10174
157340 feet/sec YDOT = -3060
030724 meter/sec
ZDOT = 19742
375067 ZDOT = 6035
309964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5347388
22 X = 1629883
93
Y = 21428140
95 feet Y = 6531297
36 meter
Z = -102457
64 Z = -31229
09
XDOT = -13619
576909 XDOT = -4151
247042
YDOT = 3489
984330 feet/sec YDOT = 1063
747224 meter/sec
ZDOT = 19813
680585 ZDOT = 6039
209842
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
50006275
00016717 00000-0 10270-3 0 9017
2 25544 51
6415 230
8270 0008143 295
6184 64
4136 15
71313537 34532
Satellite: ISS
Catalog Number: 25544
Epoch time: 10238
50006275 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 230
8270 deg
Eccentricity:
0008143
Arg of perigee: 295
6184 deg
Mean anomaly: 64
4136 deg
Mean motion: 15
71313537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3453
Checksum: 283
Coasting Arc #3 (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 = -2115282
67 A = 6728221
76 meter
Y = 3737247
96 meter E =
0009572
Z = -5186696
48 I = 51
38124
XDOT = -5949
615014 Wp = 49
34785
YDOT = -4768
528007 meter/sec RA = 224
75313 deg
ZDOT = -1004
589732 TA = 210
99964
MA = 211
05617
Ha = 193
698 n
mi
Hp = 190
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6939903
78 X = -2131720
16
Y = 12261312
22 feet Y = 3713501
40 meter
Z = -17016720
73 Z = -5197012
60
XDOT = -19519
734297 XDOT = -5890
970181
YDOT = -15644
776926 feet/sec YDOT = -4834
732325 meter/sec
ZDOT = -3295
898072 ZDOT = -1033
350072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11403095
89 X = 3475663
63
Y = -8189448
58 feet Y = -2496143
93 meter
Z = -17057935
47 Z = -5199258
73
XDOT = 10400
175631 XDOT = 3169
973532
YDOT = 21619
861106 feet/sec YDOT = 6589
733665 meter/sec
ZDOT = -3411
051787 ZDOT = -1039
688585
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
51765676
00016717 00000-0 10270-3 0 9027
2 25544 51
6412 225
6215 0008274 301
0312 59
0036 15
71280741 34696
Satellite: ISS
Catalog Number: 25544
Epoch time: 10239
51765676 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 225
6215 deg
Eccentricity:
0008274
Arg of perigee: 301
0312 deg
Mean anomaly: 59
0036 deg
Mean motion: 15
71280741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 287
Coasting Arc #4 (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 = 5779620
72 A = 6738430
88 meter
Y = 3004797
70 meter E =
0005981
Z = 1716679
61 I = 51
43884
XDOT = -954
398251 Wp = 100
32104
YDOT = 5093
413073 meter/sec RA = 219
59704 deg
ZDOT = -5686
327106 TA = 60
65893
MA = 60
59919
Ha = 193
891 n
mi
Hp = 190
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18962010
24 X = 5737251
66
Y = 9858260
18 feet Y = 3069192
08 meter
Z = 5632150
96 Z = 1744653
88
XDOT = -3131
227856 XDOT = -983
659699
YDOT = 16710
672812 feet/sec YDOT = 5082
576510 meter/sec
ZDOT = -18655
928825 ZDOT = -5691
034908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13230382
83 X = -4032620
69
Y = -16745928
02 feet Y = -5104158
86 meter
Z = 5744137
48 Z = 1750813
10
XDOT = 8378
258235 XDOT = 2553
693110
YDOT = -13042
470186 feet/sec YDOT = -3975
344913 meter/sec
ZDOT = -18674
679211 ZDOT = -5692
042224
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
53523203
00016717 00000-0 10270-3 0 9030
2 25544 51
6414 220
4166 0008459 305
6261 54
4112 15
71339073 34859
Satellite: ISS
Catalog Number: 25544
Epoch time: 10240
53523203 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 220
4166 deg
Eccentricity:
0008459
Arg of perigee: 305
6261 deg
Mean anomaly: 54
4112 deg
Mean motion: 15
71339073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 273
Coasting Arc #5 (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 = -547036
20 A = 6730401
80 meter
Y = -4854074
71 meter E =
0001813
Z = 4628612
65 I = 51
43610
XDOT = 6872
066490 Wp = 23
70699
YDOT = 1954
294530 meter/sec RA = 214
50582 deg
ZDOT = 2862
915788 TA = 37
89402
MA = 37
88126
Ha = 193
963 n
mi
Hp = 189
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1794738
20 X = -515201
38
Y = -15925441
98 feet Y = -4860013
81 meter
Z = 15185737
05 Z = 4626032
68
XDOT = 22546
149901 XDOT = 6835
794917
YDOT = 6411
727459 feet/sec YDOT = 2030
939410 meter/sec
ZDOT = 9392
768333 ZDOT = 2896
212134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4538907
12 X = -1383458
89
Y = 15380348
50 feet Y = 4687930
22 meter
Z = 15175328
63 Z = 4625440
17
XDOT = -17026
111732 XDOT = -5189
558856
YDOT = -14419
612241 feet/sec YDOT = -4395
097811 meter/sec
ZDOT = 9526
040933 ZDOT = 2903
537276
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
55278941
00016717 00000-0 10270-3 0 9040
2 25544 51
6415 215
2122 0008499 308
4139 51
6259 15
71366183 35015
Satellite: ISS
Catalog Number: 25544
Epoch time: 10241
55278941 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 215
2122 deg
Eccentricity:
0008499
Arg of perigee: 308
4139 deg
Mean anomaly: 51
6259 deg
Mean motion: 15
71366183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 299
Coasting Arc #6 (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 = -5897343
66 A = 6735102
78 meter
Y = -369858
60 meter E =
0006457
Z = -3223794
09 I = 51
47771
XDOT = -2249
321687 Wp = 346
72852
YDOT = -5613
073188 meter/sec RA = 209
33073 deg
ZDOT = 4762
995834 TA = 335
52527
MA = 335
55591
Ha = 194
094 n
mi
Hp = 189
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19348240
34 X = -5877108
87
Y = -1213446
86 feet Y = -435693
18 meter
Z = -10576752
26 Z = -3252394
30
XDOT = -7379
664328 XDOT = -2209
525931
YDOT = -18415
594448 feet/sec YDOT = -5638
003817 meter/sec
ZDOT = 15626
626752 ZDOT = 4752
165411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17396133
35 X = 5302341
45
Y = 8412314
43 feet Y = 2564073
44 meter
Z = -10691213
97 Z = -3258682
02
XDOT = 571
687084 XDOT = 174
250223
YDOT = 18604
742129 feet/sec YDOT = 5670
725401 meter/sec
ZDOT = 15583
186489 ZDOT = 4749
755242
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
50673345
00016717 00000-0 10270-3 0 9054
2 25544 51
6415 210
3325 0008442 313
2055 46
8401 15
71355893 35162
Satellite: ISS
Catalog Number: 25544
Epoch time: 10242
50673345 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 210
3325 deg
Eccentricity:
0008442
Arg of perigee: 313
2055 deg
Mean anomaly: 46
8401 deg
Mean motion: 15
71355893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 280
Coasting Arc #7 (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 = 3307247
35 A = 6733988
98 meter
Y = 4633550
15 meter E =
0006980
Z = -3603138
81 I = 51
50183
XDOT = -6228
672859 Wp = 356
74487
YDOT = 1024
927505 meter/sec RA = 204
25545 deg
ZDOT = -4391
872235 TA = 226
36123
MA = 226
41913
Ha = 194
312 n
mi
Hp = 189
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10850549
03 X = 3272691
77
Y = 15201936
18 feet Y = 4670340
52 meter
Z = -11821321
54 Z = -3587156
14
XDOT = -20435
278409 XDOT = -6218
335881
YDOT = 3362
623048 feet/sec YDOT = 955
332508 meter/sec
ZDOT = -14409
029642 ZDOT = -4422
106101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4677721
77 X = -1425769
60
Y = -18123530
27 feet Y = -5524052
03 meter
Z = -11757273
94 Z = -3583617
10
XDOT = 18865
090794 XDOT = 5750
079674
YDOT = 4572
484979 feet/sec YDOT = 1393
693422 meter/sec
ZDOT = -14530
016038 ZDOT = -4428
748888
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
52425452
00016717 00000-0 10270-3 0 9062
2 25544 51
6421 205
1274 0008494 317
1202 42
9296 15
71413141 35326
Satellite: ISS
Catalog Number: 25544
Epoch time: 10243
52425452 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 205
1274 deg
Eccentricity:
0008494
Arg of perigee: 317
1202 deg
Mean anomaly: 42
9296 deg
Mean motion: 15
71413141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 272
Coasting Arc #8 (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 = 4707383
34 A = 6731130
16 meter
Y = -2039148
43 meter E =
0010394
Z = 4360610
19 I = 51
52079
XDOT = 5141
368417 Wp = 19
11047
YDOT = 4619
609353 meter/sec RA = 199
08140 deg
ZDOT = -3378
041375 TA = 105
06527
MA = 104
95024
Ha = 194
378 n
mi
Hp = 189
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15444171
07 X = 4708652
54
Y = -6690119
53 feet Y = -1986500
57 meter
Z = 14306463
89 Z = 4383481
75
XDOT = 16868
006617 XDOT = 5105
738899
YDOT = 15156
198664 feet/sec YDOT = 4676
904016 meter/sec
ZDOT = -11082
812909 ZDOT = -3353
151118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16724914
65 X = -5097753
99
Y = 964633
92 feet Y = 294020
42 meter
Z = 14397976
93 Z = 4388503
37
XDOT = -10576
129764 XDOT = -3223
604352
YDOT = -18857
571273 feet/sec YDOT = -5747
787724 meter/sec
ZDOT = -10983
104015 ZDOT = -3347
650104
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
54175610
00016717 00000-0 10270-3 0 9074
2 25544 51
6420 199
9226 0008576 320
4510 39
6026 15
71440042 35483
Satellite: ISS
Catalog Number: 25544
Epoch time: 10244
54175610 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 199
9226 deg
Eccentricity:
0008576
Arg of perigee: 320
4510 deg
Mean anomaly: 39
6026 deg
Mean motion: 15
71440042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 291
Coasting Arc #9 (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 = -5481566
81 A = 6737260
76 meter
Y = -3196063
95 meter E =
0014039
Z = 2236819
36 I = 51
57072
XDOT = 4222
366862 Wp = 36
36594
YDOT = -3414
101923 meter/sec RA = 194
00257 deg
ZDOT = 5462
810295 TA = 348
74678
MA = 348
77815
Ha = 194
540 n
mi
Hp = 188
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17984143
08 X = -5456286
47
Y = -10485774
11 feet Y = -3257220
79 meter
Z = 7338646
18 Z = 2210251
35
XDOT = 13852
909653 XDOT = 4233
692893
YDOT = -11201
121794 feet/sec YDOT = -3366
821632 meter/sec
ZDOT = 17922
605956 ZDOT = 5483
349959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13562698
30 X = 4133910
44
Y = 15842493
87 feet Y = 4828792
13 meter
Z = 7232232
82 Z = 2204384
56
XDOT = -15515
197297 XDOT = -4729
032136
YDOT = 5053
537101 feet/sec YDOT = 1540
318108 meter/sec
ZDOT = 18004
771138 ZDOT = 5487
854243
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
55923760
00016717 00000-0 10270-3 0 9084
2 25544 51
6422 194
7174 0008512 323
9832 36
0755 15
71477661 35640
Satellite: ISS
Catalog Number: 25544
Epoch time: 10245
55923760 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 194
7174 deg
Eccentricity:
0008512
Arg of perigee: 323
9832 deg
Mean anomaly: 36
0755 deg
Mean motion: 15
71477661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3564
Checksum: 318
Coasting Arc #10 (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 = -2473300
99 A = 6728146
05 meter
Y = 3682309
87 meter E =
0009744
Z = -5065218
35 I = 51
57029
XDOT = -7091
579555 Wp = 63
77374
YDOT = -2456
113695 meter/sec RA = 188
84808 deg
ZDOT = 1683
935489 TA = 222
41767
MA = 222
49302
Ha = 194
630 n
mi
Hp = 188
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8114504
55 X = -2489687
69
Y = 12081069
13 feet Y = 3654560
38 meter
Z = -16618170
44 Z = -5077273
32
XDOT = -23266
337124 XDOT = -7071
767974
YDOT = -8058
115798 feet/sec YDOT = -2535
305236 meter/sec
ZDOT = 5524
722733 ZDOT = 1649
532931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11397914
67 X = 3474084
39
Y = -8959947
11 feet Y = -2730991
88 meter
Z = -16666370
13 Z = -5079909
62
XDOT = 18946
419492 XDOT = 5774
868661
YDOT = 14122
358275 feet/sec YDOT = 4304
494802 meter/sec
ZDOT = 5386
939594 ZDOT = 1641
939188
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
51310907
00016717 00000-0 10270-3 0 9095
2 25544 51
6424 189
8373 0008629 327
7756 32
2877 15
71490927 35793
Satellite: ISS
Catalog Number: 25544
Epoch time: 10246
51310907 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 189
8373 deg
Eccentricity:
0008629
Arg of perigee: 327
7756 deg
Mean anomaly: 32
2877 deg
Mean motion: 15
71490927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 342
Coasting Arc #11 (Orbit 3594)
---------------------------------------
Vector Time (GMT): 2010/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6629680
53 A = 6739037
83 meter
Y = 987010
89 meter E =
0002893
Z = -696579
86 I = 51
63810
XDOT = -1318
967124 Wp = 103
13368
YDOT = 4655
466120 meter/sec RA = 183
74955 deg
ZDOT = -5978
151097 TA = 84
44160
MA = 84
40860
Ha = 194
761 n
mi
Hp = 188
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21750920
38 X = 6621534
68
Y = 3238224
69 feet Y = 1061102
40 meter
Z = -2285366
98 Z = -664393
01
XDOT = -4327
319962 XDOT = -1341
886921
YDOT = 15273
838976 feet/sec YDOT = 4640
588492 meter/sec
ZDOT = -19613
356618 ZDOT = -5984
614236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19820260
55 X = -6041215
42
Y = -9556070
13 feet Y = -2912690
18 meter
Z = -2156463
39 Z = -657290
04
XDOT = 7860
312689 XDOT = 2395
823307
YDOT = -11888
044085 feet/sec YDOT = -3623
475837 meter/sec
ZDOT = -19639
151202 ZDOT = -5986
013286
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 10247
53055211
00016717 00000-0 10270-3 0 9104
2 25544 51
6432 184
6318 0008623 331
6249 28
4442 15
71524330 35958
Satellite: ISS
Catalog Number: 25544
Epoch time: 10247
53055211 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 184
6318 deg
Eccentricity:
0008623
Arg of perigee: 331
6249 deg
Mean anomaly: 28
4442 deg
Mean motion: 15
71524330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 286
Coasting Arc #12 (Orbit 3610)
---------------------------------------
Vector Time (GMT): 2010/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -218336
82 A = 6726987
83 meter
Y = -4171602
44 meter E =
0007647
Z = 5273782
71 I = 51
62879
XDOT = 7691
175207 Wp = 350
34297
YDOT = -271
960131 meter/sec RA = 178
62753 deg
ZDOT = 110
719225 TA = 98
64901
MA = 98
56237
Ha = 194
781 n
mi
Hp = 188
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -716328
15 X = -197291
69
Y = -13686359
71 feet Y = -4173926
22 meter
Z = 17302436
70 Z = 5272773
25
XDOT = 25233
514460 XDOT = 7693
106844
YDOT = -892
257648 feet/sec YDOT = -185
941996 meter/sec
ZDOT = 363
252049 ZDOT = 148
087120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3053329
47 X = -930654
82
Y = 13365979
18 feet Y = 4073950
45 meter
Z = 17298313
89 Z = 5272526
07
XDOT = -23493
378924 XDOT = -7160
781896
YDOT = -5999
100563 feet/sec YDOT = -1828
525852 meter/sec
ZDOT = 512
897090 ZDOT = 156
331033
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 10248
54797346
00016717 00000-0 10270-3 0 9119
2 25544 51
6436 179
4267 0008684 334
7382 25
3354 15
71587360 36115
Satellite: ISS
Catalog Number: 25544
Epoch time: 10248
54797346 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 179
4267 deg
Eccentricity:
0008684
Arg of perigee: 334
7382 deg
Mean anomaly: 25
3354 deg
Mean motion: 15
71587360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3611
Checksum: 328
Coasting Arc #13 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2010/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6510321
00 A = 6738715
86 meter
Y = 1448311
10 meter E =
0016276
Z = -889183
53 I = 51
69863
XDOT = -1816
939244 Wp = 11
49141
YDOT = -4529
858561 meter/sec RA = 173
50222 deg
ZDOT = 5959
009719 TA = 338
81391
MA = 338
88124
Ha = 194
945 n
mi
Hp = 187
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21359320
85 X = -6521712
99
Y = 4751676
83 feet Y = 1375445
04 meter
Z = -2917268
81 Z = -920837
95
XDOT = -5961
086760 XDOT = -1795
097860
YDOT = -14861
740686 feet/sec YDOT = -4550
054230 meter/sec
ZDOT = 19550
556820 ZDOT = 5950
236450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21838937
96 X = 6656508
29
Y = 1050807
80 feet Y = 320286
22 meter
Z = -3044021
90 Z = -927817
87
XDOT = 2014
883074 XDOT = 614
136361
YDOT = 14345
651722 feet/sec YDOT = 4372
554645 meter/sec
ZDOT = 19515
327045 ZDOT = 5948
271683
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 10249
50178934
00016717 00000-0 10270-3 0 9123
2 25544 51
6437 174
5460 0008724 338
9068 21
1733 15
71574790 36263
Satellite: ISS
Catalog Number: 25544
Epoch time: 10249
50178934 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 174
5460 deg
Eccentricity:
0008724
Arg of perigee: 338
9068 deg
Mean anomaly: 21
1733 deg
Mean motion: 15
71574790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 320
Coasting Arc #14 (Orbit 3641)
---------------------------------------
Vector Time (GMT): 2010/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2848425
96 A = 6728063
39 meter
Y = 3467728
89 meter E =
0015383
Z = -5024816
95 I = 51
69433
XDOT = -6862
290168 Wp = 41
88131
YDOT = 2915
091271 meter/sec RA = 168
41336 deg
ZDOT = -1870
333125 TA = 210
01103
MA = 210
09929
Ha = 195
051 n
mi
Hp = 187
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9345229
54 X = 2833846
83
Y = 11377063
28 feet Y = 3499499
77 meter
Z = -16485619
92 Z = -5011015
16
XDOT = -22514
075353 XDOT = -6885
291604
YDOT = 9563
947739 feet/sec YDOT = 2838
224267 meter/sec
ZDOT = -6136
263535 ZDOT = -1903
725822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6335365
86 X = -1931019
52
Y = -13358745
97 feet Y = -4071745
77 meter
Z = -16430264
57 Z = -5007944
64
XDOT = 23170
308163 XDOT = 7062
309928
YDOT = -3244
754639 feet/sec YDOT = -989
001214 meter/sec
ZDOT = -6269
958166 ZDOT = -1911
083249
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 10250
51917184
00016717 00000-0 10270-3 0 9135
2 25544 51
6449 169
3402 0008666 343
1408 16
9464 15
71636999 36426
Satellite: ISS
Catalog Number: 25544
Epoch time: 10250
51917184 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 169
3402 deg
Eccentricity:
0008666
Arg of perigee: 343
1408 deg
Mean anomaly: 16
9464 deg
Mean motion: 15
71636999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 325
Coasting Arc #15 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2010/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5256687
48 A = 6736450
47 meter
Y = -3503848
50 meter E =
0012174
Z = 2336688
13 I = 51
75233
XDOT = 4491
855361 Wp = 68
87591
YDOT = 3108
428936 meter/sec RA = 163
26626 deg
ZDOT = -5417
064232 TA = 84
90968
MA = 84
77075
Ha = 195
109 n
mi
Hp = 187
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17246349
99 X = 5284126
34
Y = -11495565
93 feet Y = -3444911
42 meter
Z = 7666299
65 Z = 2362291
93
XDOT = 14737
058272 XDOT = 4483
077427
YDOT = 10198
257664 feet/sec YDOT = 3158
609950 meter/sec
ZDOT = -17772
520447 ZDOT = -5395
264581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19388197
37 X = -5909522
56
Y = 7218067
21 feet Y = 2200066
89 meter
Z = 7768789
03 Z = 2367926
90
XDOT = -11563
548662 XDOT = -3524
569632
YDOT = -11932
288365 feet/sec YDOT = -3636
961494 meter/sec
ZDOT = -17685
130812 ZDOT = -5390
427871
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 10251
53653362
00016717 00000-0 10270-3 0 9144
2 25544 51
6448 164
1345 0008647 346
4928 13
6002 15
71648016 36588
Satellite: ISS
Catalog Number: 25544
Epoch time: 10251
53653362 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 164
1345 deg
Eccentricity:
0008647
Arg of perigee: 346
4928 deg
Mean anomaly: 13
6002 deg
Mean motion: 15
71648016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 306
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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