Date:
September 2nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15500 03 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 3515)
---------------------------------------
Vector Time (GMT): 2010/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5896601
72 A = 6735138
71 meter
Y = -368477
76 meter E =
0006381
Z = -3225547
22 I = 51
47931
XDOT = -2251
511894 Wp = 347
71135
YDOT = -5613
212319 meter/sec RA = 209
33513 deg
ZDOT = 4761
619152 TA = 334
52005
MA = 334
55150
Ha = 194
104 n
mi
Hp = 189
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19345806
18 X = -5876373
92
Y = -1208916
53 feet Y = -434304
08 meter
Z = -10582504
01 Z = -3254143
84
XDOT = -7386
850045 XDOT = -2211
707731
YDOT = -18416
050914 feet/sec YDOT = -5638
167393 meter/sec
ZDOT = 15622
110079 ZDOT = 4750
778110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17395560
31 X = 5302166
78
Y = 8407187
45 feet Y = 2562510
74 meter
Z = -10696951
33 Z = -3260430
77
XDOT = 577
768514 XDOT = 176
103843
YDOT = 18607
912228 feet/sec YDOT = 5671
691647 meter/sec
ZDOT = 15578
627316 ZDOT = 4748
365606
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
50673758
00016717 00000-0 10270-3 0 9007
2 25544 51
6431 210
3371 0008326 313
5665 46
4805 15
71341608 35165
Satellite: ISS
Catalog Number: 25544
Epoch time: 10242
50673758 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 210
3371 deg
Eccentricity:
0008326
Arg of perigee: 313
5665 deg
Mean anomaly: 46
4805 deg
Mean motion: 15
71341608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 286
Coasting Arc #2 (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 = 3314324
88 A = 6734054
06 meter
Y = 4632563
24 meter E =
0006909
Z = -3598059
99 I = 51
50350
XDOT = -6223
503061 Wp = 357
57625
YDOT = 1031
510212 meter/sec RA = 204
26015 deg
ZDOT = -4397
551386 TA = 225
45239
MA = 225
50883
Ha = 194
326 n
mi
Hp = 189
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10873769
28 X = 3279755
14
Y = 15198698
31 feet Y = 4669432
69 meter
Z = -11804658
77 Z = -3582042
98
XDOT = -20418
317128 XDOT = -6213
212488
YDOT = 3384
219855 feet/sec YDOT = 961
972767 meter/sec
ZDOT = -14427
662028 ZDOT = -4427
760250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4700446
90 X = -1432696
22
Y = -18128881
18 feet Y = -5525682
99 meter
Z = -11740473
72 Z = -3578496
39
XDOT = 18856
603510 XDOT = 5747
492750
YDOT = 4547
831140 feet/sec YDOT = 1386
178932 meter/sec
ZDOT = -14548
548236 ZDOT = -4434
397502
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
52426899
00016717 00000-0 10270-3 0 9013
2 25544 51
6437 205
1323 0008380 317
4967 42
5546 15
71395946 35329
Satellite: ISS
Catalog Number: 25544
Epoch time: 10243
52426899 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 205
1323 deg
Eccentricity:
0008380
Arg of perigee: 317
4967 deg
Mean anomaly: 42
5546 deg
Mean motion: 15
71395946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 316
Coasting Arc #3 (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 = 4695975
20 A = 6731159
22 meter
Y = -2048957
90 meter E =
0010384
Z = 4368239
41 I = 51
52231
XDOT = 5154
781531 Wp = 19
56009
YDOT = 4614
025714 meter/sec RA = 199
08648 deg
ZDOT = -3365
357102 TA = 104
46897
MA = 104
35373
Ha = 194
396 n
mi
Hp = 189
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15406742
78 X = 4697317
88
Y = -6722302
84 feet Y = -1996437
21 meter
Z = 14331494
12 Z = 4391055
72
XDOT = 16912
012897 XDOT = 5119
151835
YDOT = 15137
879638 feet/sec YDOT = 4671
470370 meter/sec
ZDOT = -11041
197840 ZDOT = -3340
401684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16700788
48 X = -5090400
33
Y = 1007826
51 feet Y = 307185
52 meter
Z = 14422785
87 Z = 4396065
13
XDOT = -10620
373769 XDOT = -3237
089925
YDOT = -18857
278014 feet/sec YDOT = -5747
698339 meter/sec
ZDOT = -10941
228229 ZDOT = -3334
886364
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
54178285
00016717 00000-0 10270-3 0 9020
2 25544 51
6437 199
9278 0008464 320
8332 39
2217 15
71419749 35488
Satellite: ISS
Catalog Number: 25544
Epoch time: 10244
54178285 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 199
9278 deg
Eccentricity:
0008464
Arg of perigee: 320
8332 deg
Mean anomaly: 39
2217 deg
Mean motion: 15
71419749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 332
Coasting Arc #4 (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 = -5495948
54 A = 6737363
58 meter
Y = -3184668
19 meter E =
0014106
Z = 2217930
91 I = 51
57245
XDOT = 4197
767505 Wp = 36
66456
YDOT = -3427
998672 meter/sec RA = 194
00781 deg
ZDOT = 5473
016757 TA = 348
22066
MA = 348
25362
Ha = 194
563 n
mi
Hp = 188
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18031327
23 X = -5470702
80
Y = -10448386
47 feet Y = -3245986
06 meter
Z = 7276676
21 Z = 2191292
95
XDOT = 13772
203100 XDOT = 4209
201179
YDOT = -11246
714803 feet/sec YDOT = -3380
992864 meter/sec
ZDOT = 17956
091722 ZDOT = 5493
437178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13619222
07 X = 4151138
89
Y = 15822632
26 feet Y = 4822738
31 meter
Z = 7169983
03 Z = 2185410
83
XDOT = -15455
295405 XDOT = -4710
774040
YDOT = 5119
130299 feet/sec YDOT = 1560
310915 meter/sec
ZDOT = 18037
779302 ZDOT = 5497
915131
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
55927861
00016717 00000-0 10270-3 0 9035
2 25544 51
6438 194
7228 0008403 324
3827 35
6773 15
71454360 35641
Satellite: ISS
Catalog Number: 25544
Epoch time: 10245
55927861 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 194
7228 deg
Eccentricity:
0008403
Arg of perigee: 324
3827 deg
Mean anomaly: 35
6773 deg
Mean motion: 15
71454360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3564
Checksum: 320
Coasting Arc #5 (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 = -2439520
53 A = 6728186
69 meter
Y = 3693786
65 meter E =
0009892
Z = -5073477
61 I = 51
57179
XDOT = -7106
632921 Wp = 64
31338
YDOT = -2433
573231 meter/sec RA = 188
85408 deg
ZDOT = 1652
059980 TA = 221
56270
MA = 221
63794
Ha = 194
660 n
mi
Hp = 188
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8003676
28 X = -2455997
96
Y = 12118722
60 feet Y = 3666414
40 meter
Z = -16645267
76 Z = -5085368
69
XDOT = -23315
724805 XDOT = -7086
917427
YDOT = -7984
164145 feet/sec YDOT = -2512
933645 meter/sec
ZDOT = 5420
144290 ZDOT = 1617
584060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11304318
36 X = 3445556
24
Y = -9030484
75 feet Y = -2752491
75 meter
Z = -16692811
08 Z = -5087968
82
XDOT = 19010
760362 XDOT = 5794
479758
YDOT = 14074
242985 feet/sec YDOT = 4289
829262 meter/sec
ZDOT = 5282
067838 ZDOT = 1609
974277
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
51316528
00016717 00000-0 10270-3 0 9045
2 25544 51
6441 189
8430 0008522 328
1860 31
8786 15
71464573 35791
Satellite: ISS
Catalog Number: 25544
Epoch time: 10246
51316528 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 189
8430 deg
Eccentricity:
0008522
Arg of perigee: 328
1860 deg
Mean anomaly: 31
8786 deg
Mean motion: 15
71464573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 320
Coasting Arc #6 (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 = 6637824
77 A = 6739143
63 meter
Y = 958126
46 meter E =
0003117
Z = -658679
18 I = 51
63979
XDOT = -1264
479448 Wp = 104
19343
YDOT = 4663
216475 meter/sec RA = 183
75533 deg
ZDOT = -5983
903841 TA = 82
96725
MA = 82
93181
Ha = 194
795 n
mi
Hp = 188
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21777640
32 X = 6629817
19
Y = 3143459
50 feet Y = 1032309
82 meter
Z = -2161020
93 Z = -626452
44
XDOT = -4148
554619 XDOT = -1287
462015
YDOT = 15299
266651 feet/sec YDOT = 4648
947810 meter/sec
ZDOT = -19632
230451 ZDOT = -5990
102434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19873214
85 X = -6057355
89
Y = -9473301
70 feet Y = -2887462
36 meter
Z = -2031958
11 Z = -619340
83
XDOT = 7703
097617 XDOT = 2347
904154
YDOT = -11961
588750 feet/sec YDOT = -3645
892251 meter/sec
ZDOT = -19656
965570 ZDOT = -5991
443106
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
53062653
00016717 00000-0 10270-3 0 9056
2 25544 51
6448 184
6378 0008517 332
0531 28
0173 15
71494622 35959
Satellite: ISS
Catalog Number: 25544
Epoch time: 10247
53062653 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 184
6378 deg
Eccentricity:
0008517
Arg of perigee: 332
0531 deg
Mean anomaly: 28
0173 deg
Mean motion: 15
71494622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 309
Coasting Arc #7 (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 = -280079
76 A = 6727085
19 meter
Y = -4169121
93 meter E =
0007451
Z = 5272799
48 I = 51
63043
XDOT = 7688
602362 Wp = 350
95394
YDOT = -315
119801 meter/sec RA = 178
63458 deg
ZDOT = 166
496699 TA = 97
50736
MA = 97
42270
Ha = 194
819 n
mi
Hp = 188
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -918896
85 X = -259053
00
Y = -13678221
57 feet Y = -4172136
27 meter
Z = 17299210
90 Z = 5271490
04
XDOT = 25225
073365 XDOT = 7690
745856
YDOT = -1033
857615 feet/sec YDOT = -229
129251 meter/sec
ZDOT = 546
249012 ZDOT = 203
852611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2856633
97 X = -870702
03
Y = 13414989
29 feet Y = 4088888
74 meter
Z = 17293886
76 Z = 5271176
68
XDOT = -23520
383738 XDOT = -7169
012963
YDOT = -5874
863104 feet/sec YDOT = -1790
658274 meter/sec
ZDOT = 695
845221 ZDOT = 212
093623
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
54806812
00016717 00000-0 10270-3 0 9062
2 25544 51
6452 179
4330 0008582 335
1519 24
9229 15
71555370 36110
Satellite: ISS
Catalog Number: 25544
Epoch time: 10248
54806812 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 179
4330 deg
Eccentricity:
0008582
Arg of perigee: 335
1519 deg
Mean anomaly: 24
9229 deg
Mean motion: 15
71555370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3611
Checksum: 306
Coasting Arc #8 (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 = -6492086
61 A = 6738768
56 meter
Y = 1492706
65 meter E =
0016103
Z = -948641
82 I = 51
70008
XDOT = -1901
335907 Wp = 11
45917
YDOT = -4510
612597 meter/sec RA = 173
50869 deg
ZDOT = 5947
002784 TA = 338
19150
MA = 338
25998
Ha = 194
987 n
mi
Hp = 187
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21299496
76 X = -6503687
56
Y = 4897331
54 feet Y = 1420043
33 meter
Z = -3112341
93 Z = -980208
17
XDOT = -6237
978697 XDOT = -1879
645135
YDOT = -14798
597760 feet/sec YDOT = -4531
752883 meter/sec
ZDOT = 19511
163990 ZDOT = 5937
819156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21818570
10 X = 6650300
17
Y = 894228
06 feet Y = 272560
71 meter
Z = -3238741
37 Z = -987168
37
XDOT = 2286
973258 XDOT = 697
069449
YDOT = 14359
267025 feet/sec YDOT = 4376
704589 meter/sec
ZDOT = 19474
291028 ZDOT = 5935
763905
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
50190494
00016717 00000-0 10270-3 0 9072
2 25544 51
6453 174
5527 0008626 339
3560 20
7252 15
71538943 36269
Satellite: ISS
Catalog Number: 25544
Epoch time: 10249
50190494 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 174
5527 deg
Eccentricity:
0008626
Arg of perigee: 339
3560 deg
Mean anomaly: 20
7252 deg
Mean motion: 15
71538943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 315
Coasting Arc #9 (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 = 2930245
49 A = 6728275
26 meter
Y = 3432665
58 meter E =
0015329
Z = -5002100
15 I = 51
69629
XDOT = -6817
373526 Wp = 41
62478
YDOT = 2968
125986 meter/sec RA = 168
42141 deg
ZDOT = -1948
955924 TA = 209
48127
MA = 209
56781
Ha = 195
099 n
mi
Hp = 187
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9613666
31 X = 2915942
01
Y = 11262026
19 feet Y = 3465352
97 meter
Z = -16411089
72 Z = -4987900
21
XDOT = -22366
711043 XDOT = -6840
589414
YDOT = 9737
946149 feet/sec YDOT = 2891
760061 meter/sec
ZDOT = -6394
212348 ZDOT = -1982
130943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6623482
48 X = -2018837
46
Y = -13313574
06 feet Y = -4057977
37 meter
Z = -16354140
31 Z = -4984741
97
XDOT = 23072
374628 XDOT = 7032
459787
YDOT = -3429
157368 feet/sec YDOT = -1045
207166 meter/sec
ZDOT = -6527
033953 ZDOT = -1989
439949
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
51931180
00016717 00000-0 10270-3 0 9081
2 25544 51
6465 169
3472 0008572 343
6279 16
4605 15
71598182 36421
Satellite: ISS
Catalog Number: 25544
Epoch time: 10250
51931180 = yrday
fracday
Element set: 908
Inclination: 51
6465 deg
RA of node: 169
3472 deg
Eccentricity:
0008572
Arg of perigee: 343
6279 deg
Mean anomaly: 16
4605 deg
Mean motion: 15
71598182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3642
Checksum: 316
Coasting Arc #10 (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 = 5192391
67 A = 6736411
78 meter
Y = -3547051
95 meter E =
0012358
Z = 2413745
92 I = 51
75340
XDOT = 4588
766303 Wp = 68
18680
YDOT = 3043
178889 meter/sec RA = 163
27375 deg
ZDOT = -5372
813719 TA = 84
66475
MA = 84
52376
Ha = 195
162 n
mi
Hp = 187
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17035405
73 X = 5219944
08
Y = -11637309
56 feet Y = -3488833
22 meter
Z = 7919113
90 Z = 2439037
64
XDOT = 15055
007555 XDOT = 4580
495844
YDOT = 9984
182706 feet/sec YDOT = 3094
446461 meter/sec
ZDOT = -17627
341599 ZDOT = -5350
542040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19214177
01 X = -5856481
15
Y = 7404980
62 feet Y = 2257038
09 meter
Z = 8020352
29 Z = 2444603
38
XDOT = -11907
827235 XDOT = -3629
505741
YDOT = -11809
814751 feet/sec YDOT = -3599
631536 meter/sec
ZDOT = -17538
062497 ZDOT = -5345
601449
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
53670008
00016717 00000-0 10270-3 0 9094
2 25544 51
6464 164
1419 0008554 346
9878 13
1062 15
71605657 36589
Satellite: ISS
Catalog Number: 25544
Epoch time: 10251
53670008 = yrday
fracday
Element set: 909
Inclination: 51
6464 deg
RA of node: 164
1419 deg
Eccentricity:
0008554
Arg of perigee: 346
9878 deg
Mean anomaly: 13
1062 deg
Mean motion: 15
71605657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 317
Coasting Arc #11 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2010/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4890980
15 A = 6731003
88 meter
Y = -1689045
28 meter E =
0009731
Z = 4294619
94 I = 51
76405
XDOT = 4785
627151 Wp = 56
08056
YDOT = -4901
756729 meter/sec RA = 158
21038 deg
ZDOT = 3521
997491 TA = 358
31838
MA = 358
32165
Ha = 195
378 n
mi
Hp = 187
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16046522
79 X = -4892591
89
Y = -5541487
15 feet Y = -1743747
75 meter
Z = 14089960
42 Z = 4270855
83
XDOT = 15700
876480 XDOT = 4822
974602
YDOT = -16081
879032 feet/sec YDOT = -4848
031808 meter/sec
ZDOT = 11555
109877 ZDOT = 3545
337242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14571446
35 X = 4441376
85
Y = 8862647
52 feet Y = 2701334
96 meter
Z = 13994727
17 Z = 4265592
84
XDOT = -18063
567729 XDOT = -5505
775444
YDOT = 11303
475599 feet/sec YDOT = 3445
299363 meter/sec
ZDOT = 11648
507376 ZDOT = 3550
465048
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 10252
55406911
00016717 00000-0 10270-3 0 9109
2 25544 51
6465 158
9361 0008589 350
8956 9
2049 15
71636499 36743
Satellite: ISS
Catalog Number: 25544
Epoch time: 10252
55406911 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 158
9361 deg
Eccentricity:
0008589
Arg of perigee: 350
8956 deg
Mean anomaly: 9
2049 deg
Mean motion: 15
71636499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 336
Coasting Arc #12 (Orbit 3688)
---------------------------------------
Vector Time (GMT): 2010/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3007259
45 A = 6732880
27 meter
Y = 4772075
95 meter E =
0008832
Z = -3673874
53 I = 51
79901
XDOT = -6313
241497 Wp = 33
06668
YDOT = -635
098984 meter/sec RA = 153
05291 deg
ZDOT = 4354
910993 TA = 282
94594
MA = 283
04456
Ha = 195
295 n
mi
Hp = 186
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9866336
79 X = -3042551
08
Y = 15656417
14 feet Y = 4738249
33 meter
Z = -12053394
14 Z = -3688569
99
XDOT = -20712
734570 XDOT = -6326
825952
YDOT = -2083
658083 feet/sec YDOT = -705
773025 meter/sec
ZDOT = 14287
765726 ZDOT = 4324
208192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12687574
97 X = 3867172
85
Y = -13419128
47 feet Y = -4090150
36 meter
Z = -12112173
31 Z = -3691790
43
XDOT = 19000
344051 XDOT = 5791
304867
YDOT = 5215
110538 feet/sec YDOT = 1589
565692 meter/sec
ZDOT = 14164
751728 ZDOT = 4317
416327
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 10253
50783480
00016717 00000-0 10270-3 0 9115
2 25544 51
6468 154
0558 0008646 354
0298 6
0760 15
71676445 36896
Satellite: ISS
Catalog Number: 25544
Epoch time: 10253
50783480 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 154
0558 deg
Eccentricity:
0008646
Arg of perigee: 354
0298 deg
Mean anomaly: 6
0760 deg
Mean motion: 15
71676445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3689
Checksum: 325
Coasting Arc #13 (Orbit 3704)
---------------------------------------
Vector Time (GMT): 2010/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5863445
96 A = 6734243
35 meter
Y = -640570
75 meter E =
0008978
Z = -3261870
02 I = 51
82993
XDOT = -2029
737444 Wp = 27
47077
YDOT = 5682
431905 meter/sec RA = 147
99824 deg
ZDOT = -4761
916882 TA = 190
52211
MA = 190
54090
Ha = 195
390 n
mi
Hp = 186
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19237027
43 X = 5886018
84
Y = -2101610
08 feet Y = -574876
18 meter
Z = -10701673
29 Z = -3233330
32
XDOT = -6659
243584 XDOT = -2069
995887
YDOT = 18643
149296 feet/sec YDOT = 5659
508766 meter/sec
ZDOT = -15623
086883 ZDOT = -4771
875564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19363049
21 X = -5901857
40
Y = -1409369
33 feet Y = -429575
77 meter
Z = -10587341
68 Z = -3227021
74
XDOT = 9714
746361 XDOT = 2961
054691
YDOT = -15742
726849 feet/sec YDOT = -4798
383144 meter/sec
ZDOT = -15662
882139 ZDOT = -4774
046476
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 10254
52516638
00016717 00000-0 10270-3 0 9128
2 25544 51
6468 148
8498 0008641 356
9343 3
1765 15
71692362 37055
Satellite: ISS
Catalog Number: 25544
Epoch time: 10254
52516638 = yrday
fracday
Element set: 912
Inclination: 51
6468 deg
RA of node: 148
8498 deg
Eccentricity:
0008641
Arg of perigee: 356
9343 deg
Mean anomaly: 3
1765 deg
Mean motion: 15
71692362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 327
Coasting Arc #14 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2010/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 516720
12 A = 6729446
13 meter
Y = -4904849
90 meter E =
0014562
Z = 4577673
25 I = 51
83925
XDOT = 6748
566121 Wp = 32
53209
YDOT = -2129
426220 meter/sec RA = 142
84663 deg
ZDOT = -3026
928682 TA = 87
56250
MA = 87
39580
Ha = 195
420 n
mi
Hp = 186
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1695275
97 X = 549290
97
Y = -16092027
23 feet Y = -4898889
32 meter
Z = 15018613
01 Z = 4580262
81
XDOT = 22140
964964 XDOT = 6786
580568
YDOT = -6986
306496 feet/sec YDOT = -2053
747281 meter/sec
ZDOT = -9930
868378 ZDOT = -2994
051479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4210840
75 X = -1283464
26
Y = 15613673
99 feet Y = 4759047
83 meter
Z = 15028906
90 Z = 4580810
82
XDOT = -21903
499930 XDOT = -6676
186779
YDOT = 3576
973523 feet/sec YDOT = 1090
261530 meter/sec
ZDOT = -9799
171584 ZDOT = -2986
787499
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 10255
54247795
00016717 00000-0 10270-3 0 9137
2 25544 51
6463 143
6434 0008776
6805 359
4367 15
71764393 37215
Satellite: ISS
Catalog Number: 25544
Epoch time: 10255
54247795 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 143
6434 deg
Eccentricity:
0008776
Arg of perigee:
6805 deg
Mean anomaly: 359
4367 deg
Mean motion: 15
71764393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 326
Coasting Arc #15 (Orbit 3736)
---------------------------------------
Vector Time (GMT): 2010/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5661729
57 A = 6736967
40 meter
Y = 3042725
26 meter E =
0019692
Z = 1976941
58 I = 51
88767
XDOT = -827
049405 Wp = 44
41792
YDOT = -5204
648082 meter/sec RA = 137
78372 deg
ZDOT = 5622
240466 TA = 337
52245
MA = 337
60860
Ha = 195
649 n
mi
Hp = 186
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18575228
25 X = -5704936
77
Y = 9982694
42 feet Y = 2979170
87 meter
Z = 6486028
79 Z = 1949331
71
XDOT = -2713
416683 XDOT = -796
100588
YDOT = -17075
617068 feet/sec YDOT = -5213
723459 meter/sec
ZDOT = 18445
670819 ZDOT = 5618
297943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19872928
39 X = 6057268
57
Y = -7154186
20 feet Y = -2180595
95 meter
Z = 6375437
18 Z = 1943233
25
XDOT = -225
776573 XDOT = -68
816699
YDOT = 15855
098660 feet/sec YDOT = 4832
634071 meter/sec
ZDOT = 18429
793187 ZDOT = 5617
400964
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 10256
55977214
00016717 00000-0 10270-3 0 9146
2 25544 51
6463 138
4366 0008807 4
5551 355
5690 15
71746179 37372
Satellite: ISS
Catalog Number: 25544
Epoch time: 10256
55977214 = yrday
fracday
Element set: 914
Inclination: 51
6463 deg
RA of node: 138
4366 deg
Eccentricity:
0008807
Arg of perigee: 4
5551 deg
Mean anomaly: 355
5690 deg
Mean motion: 15
71746179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3737
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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