Date:
August 18th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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
230/20:35:29
670 1
2 4
0 4
0
N/A -3
2 -0
5 192
2
000/00:10:59
340 2
2 0
2 191
6
Coasting Arc #1 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2010/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4049368
25 A = 6726391
55 meter
Y = -1191135
54 meter E =
0010665
Z = -5245803
45 I = 51
29188
XDOT = 1760
710111 Wp = 113
94044
YDOT = -7478
544393 meter/sec RA = 281
24422 deg
ZDOT = 335
247480 TA = 159
28367
MA = 159
24041
Ha = 192
657 n
mi
Hp = 188
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13285328
90 X = -4010264
76
Y = -3907924
99 feet Y = -1236199
14 meter
Z = -17210641
23 Z = -5265380
24
XDOT = 5776
607975 XDOT = 1842
577140
YDOT = -24535
906802 feet/sec YDOT = -7458
397350 meter/sec
ZDOT = 1099
893306 ZDOT = 343
999513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8367192
10 X = 2550320
15
Y = 10911518
42 feet Y = 3325830
82 meter
Z = -17288923
49 Z = -5269663
88
XDOT = -18295
428465 XDOT = -5576
446596
YDOT = 15846
807332 feet/sec YDOT = 4830
106875 meter/sec
ZDOT = 1134
882008 ZDOT = 345
912036
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 10228
51532697
00016717 00000-0 10270-3 0 9008
2 25544 51
6448 281
8914 0006363 235
1814 124
8750 15
71808937 32961
Satellite: ISS
Catalog Number: 25544
Epoch time: 10228
51532697 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 281
8914 deg
Eccentricity:
0006363
Arg of perigee: 235
1814 deg
Mean anomaly: 124
8750 deg
Mean motion: 15
71808937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 323
Coasting Arc #2 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2010/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -400234
65 A = 6738172
72 meter
Y = 6706704
93 meter E =
0012454
Z = 393348
19 I = 51
32796
XDOT = -4832
463889 Wp = 158
83618
YDOT = 66
008837 meter/sec RA = 276
10088 deg
ZDOT = -5994
974669 TA = 16
87065
MA = 16
82927
Ha = 192
355 n
mi
Hp = 189
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1313105
80 X = -477111
31
Y = 22003625
11 feet Y = 6701799
41 meter
Z = 1290512
43 Z = 391217
49
XDOT = -15854
540317 XDOT = -4803
720565
YDOT = 216
564426 feet/sec YDOT = 12
130364 meter/sec
ZDOT = -19668
552064 ZDOT = -6018
380785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13708325
60 X = 4178297
64
Y = -17262313
39 feet Y = -5261553
12 meter
Z = 1282003
42 Z = 390754
64
XDOT = 11753
753219 XDOT = 3582
543981
YDOT = 7854
552793 feet/sec YDOT = 2394
067691 meter/sec
ZDOT = -19762
149891 ZDOT = -6023
503287
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 10229
53255395
00016717 00000-0 10270-3 0 9019
2 25544 51
6454 276
6847 0006160 239
3881 120
6674 15
71873321 33127
Satellite: ISS
Catalog Number: 25544
Epoch time: 10229
53255395 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 276
6847 deg
Eccentricity:
0006160
Arg of perigee: 239
3881 deg
Mean anomaly: 120
6674 deg
Mean motion: 15
71873321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 310
Coasting Arc #3 (Orbit 3327)
---------------------------------------
Vector Time (GMT): 2010/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4142107
32 A = 6726630
40 meter
Y = -1306178
94 meter E =
0005552
Z = 5139296
13 I = 51
28649
XDOT = 854
271712 Wp = 202
03652
YDOT = 7549
100435 meter/sec RA = 270
97245 deg
ZDOT = 1225
479844 TA = 236
16091
MA = 236
21377
Ha = 192
145 n
mi
Hp = 189
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13589590
94 X = 4131439
90
Y = -4285363
99 feet Y = -1259919
37 meter
Z = 16861207
77 Z = 5159392
28
XDOT = 2802
728714 XDOT = 763
839702
YDOT = 24767
389877 feet/sec YDOT = 7558
147708 meter/sec
ZDOT = 4020
603162 ZDOT = 1229
410635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13576983
81 X = -4138264
67
Y = -3998789
76 feet Y = -1218831
12 meter
Z = 16941571
50 Z = 5163790
99
XDOT = 11267
238289 XDOT = 3434
254230
YDOT = -21090
381339 feet/sec YDOT = -6428
348232 meter/sec
ZDOT = 4036
342917 ZDOT = 1230
277321
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 10230
54976562
00016717 00000-0 10270-3 0 9029
2 25544 51
6446 271
4780 0006130 242
9049 117
1488 15
71886713 33280
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
54976562 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 271
4780 deg
Eccentricity:
0006130
Arg of perigee: 242
9049 deg
Mean anomaly: 117
1488 deg
Mean motion: 15
71886713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3328
Checksum: 313
Coasting Arc #4 (Orbit 3332)
---------------------------------------
Vector Time (GMT): 2010/230/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2385501
70 A = 6736812
45 meter
Y = -5607954
88 meter E =
0004300
Z = -2865928
80 I = 51
31482
XDOT = 3963
088062 Wp = 290
31732
YDOT = -4261
034358 meter/sec RA = 269
07670 deg
ZDOT = 5034
472370 TA = 36
64599
MA = 36
61659
Ha = 192
233 n
mi
Hp = 191
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7826449
15 X = -2308693
23
Y = -18398802
09 feet Y = -5634201
36 meter
Z = -9402653
55 Z = -2877331
19
XDOT = 13002
257420 XDOT = 3985
984927
YDOT = -13979
771515 feet/sec YDOT = -4216
589007 meter/sec
ZDOT = 16517
297803 ZDOT = 5053
780183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17389073
95 X = 5300189
74
Y = -9824937
08 feet Y = -2994640
82 meter
Z = -9448271
65 Z = -2879833
20
XDOT = 14647
572043 XDOT = 4464
579959
YDOT = 9951
742583 feet/sec YDOT = 3033
291139 meter/sec
ZDOT = 16594
501152 ZDOT = 5058
003951
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 10230
86764134
00016717 00000-0 10270-3 0 9035
2 25544 51
6462 269
8501 0008200 266
4950 93
5274 15
71111965 33338
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
86764134 = yrday
fracday
Element set: 903
Inclination: 51
6462 deg
RA of node: 269
8501 deg
Eccentricity:
0008200
Arg of perigee: 266
4950 deg
Mean anomaly: 93
5274 deg
Mean motion: 15
71111965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3333
Checksum: 297
Coasting Arc #5 (Orbit 3348)
---------------------------------------
Vector Time (GMT): 2010/231/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2569014
39 A = 6733931
13 meter
Y = 4905703
62 meter E =
0002767
Z = -3831187
27 I = 51
30738
XDOT = -3860
946887 Wp = 312
08392
YDOT = -5234
376153 meter/sec RA = 263
98977 deg
ZDOT = -4109
739257 TA = 274
71423
MA = 274
74583
Ha = 191
709 n
mi
Hp = 191
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8428524
89 X = -2605069
01
Y = 16094828
14 feet Y = 4876773
97 meter
Z = -12569512
05 Z = -3843754
66
XDOT = -12667
148578 XDOT = -3782
164131
YDOT = -17173
150109 feet/sec YDOT = -5277
110856 meter/sec
ZDOT = -13483
396513 ZDOT = -4128
304354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17053197
75 X = -5197814
67
Y = -6164934
36 feet Y = -1879071
99 meter
Z = -12619753
91 Z = -3846500
99
XDOT = 14919
706923 XDOT = 4547
526670
YDOT = -13492
508051 feet/sec YDOT = -4112
516454 meter/sec
ZDOT = -13557
671528 ZDOT = -4132
378282
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 10231
88534211
00016717 00000-0 10270-3 0 9040
2 25544 51
6466 264
6470 0008231 271
0844 88
9374 15
71135107 33498
Satellite: ISS
Catalog Number: 25544
Epoch time: 10231
88534211 = yrday
fracday
Element set: 904
Inclination: 51
6466 deg
RA of node: 264
6470 deg
Eccentricity:
0008231
Arg of perigee: 271
0844 deg
Mean anomaly: 88
9374 deg
Mean motion: 15
71135107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3349
Checksum: 302
Coasting Arc #6 (Orbit 3364)
---------------------------------------
Vector Time (GMT): 2010/232/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4090534
99 A = 6732506
91 meter
Y = 3298284
73 meter E =
0003908
Z = 4210079
84 I = 51
30646
XDOT = -1625
148968 Wp = 21
55418
YDOT = 6606
681853 meter/sec RA = 258
80198 deg
ZDOT = -3592
200655 TA = 105
20897
MA = 105
16576
Ha = 192
475 n
mi
Hp = 191
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13420390
39 X = 4032897
54
Y = 10821144
11 feet Y = 3343705
10 meter
Z = 13812597
89 Z = 4229811
41
XDOT = -5331
853568 XDOT = -1681
455384
YDOT = 21675
465397 feet/sec YDOT = 6588
193783 meter/sec
ZDOT = -11785
435219 ZDOT = -3600
231977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8720381
26 X = -2657972
21
Y = 14797700
43 feet Y = 4510339
09 meter
Z = 13891541
00 Z = 4234141
70
XDOT = -21137
157357 XDOT = -6442
605562
YDOT = -1348
197548 feet/sec YDOT = -410
930613 meter/sec
ZDOT = -11817
518790 ZDOT = -3601
979727
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
90302829
00016717 00000-0 10270-3 0 9053
2 25544 51
6458 259
4436 0008212 275
3468 84
6757 15
71159127 33655
Satellite: ISS
Catalog Number: 25544
Epoch time: 10232
90302829 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 259
4436 deg
Eccentricity:
0008212
Arg of perigee: 275
3468 deg
Mean anomaly: 84
6757 deg
Mean motion: 15
71159127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3365
Checksum: 322
Coasting Arc #7 (Orbit 3380)
---------------------------------------
Vector Time (GMT): 2010/233/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 131231
71 A = 6737850
90 meter
Y = -6302175
86 meter E =
0007444
Z = 2366387
12 I = 51
33155
XDOT = 5093
738304 Wp = 44
90724
YDOT = 2122
705088 meter/sec RA = 253
71022 deg
ZDOT = 5365
643477 TA = 341
84532
MA = 341
87188
Ha = 192
715 n
mi
Hp = 191
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 430550
23 X = 190198
80
Y = -20676430
00 feet Y = -6300378
70 meter
Z = 7763737
27 Z = 2367167
72
XDOT = 16711
739844 XDOT = 5043
558468
YDOT = 6964
255538 feet/sec YDOT = 2179
385630 meter/sec
ZDOT = 17603
817182 ZDOT = 5390
266504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20454629
59 X = 6234571
10
Y = -3043113
92 feet Y = -927541
12 meter
Z = 7766809
73 Z = 2367323
60
XDOT = -4341
829549 XDOT = -1323
389646
YDOT = 16039
291408 feet/sec YDOT = 4888
776021 meter/sec
ZDOT = 17702
328728 ZDOT = 5395
669796
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
92069953
00016717 00000-0 10270-3 0 9065
2 25544 51
6459 254
2391 0008226 279
6897 80
3335 15
71157687 33819
Satellite: ISS
Catalog Number: 25544
Epoch time: 10233
92069953 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 254
2391 deg
Eccentricity:
0008226
Arg of perigee: 279
6897 deg
Mean anomaly: 80
3335 deg
Mean motion: 15
71157687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3381
Checksum: 338
Coasting Arc #8 (Orbit 3395)
---------------------------------------
Vector Time (GMT): 2010/234/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4462372
34 A = 6729055
85 meter
Y = -342353
22 meter E =
0005130
Z = -5029572
71 I = 51
31209
XDOT = -1396
544596 Wp = 103
25811
YDOT = -7361
759012 meter/sec RA = 248
53842 deg
ZDOT = 1740
483510 TA = 183
58981
MA = 183
59349
Ha = 192
787 n
mi
Hp = 191
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14640329
21 X = -4433780
19
Y = -1123206
10 feet Y = -392094
26 meter
Z = -16501222
81 Z = -5051181
01
XDOT = -4581
839226 XDOT = -1322
575039
YDOT = -24152
752665 feet/sec YDOT = -7376
962428 meter/sec
ZDOT = 5710
247736 ZDOT = 1733
878893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1548524
44 X = -471990
25
Y = -14503191
40 feet Y = -4420572
74 meter
Z = -16587667
01 Z = -5055920
90
XDOT = 21847
374163 XDOT = 6659
079645
YDOT = -8832
090724 feet/sec YDOT = -2692
021253 meter/sec
ZDOT = 5683
754433 ZDOT = 1732
408351
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
87475082
00016717 00000-0 10270-3 0 9075
2 25544 51
6459 249
3605 0008338 283
0391 76
9840 15
71208866 33968
Satellite: ISS
Catalog Number: 25544
Epoch time: 10234
87475082 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 249
3605 deg
Eccentricity:
0008338
Arg of perigee: 283
0391 deg
Mean anomaly: 76
9840 deg
Mean motion: 15
71208866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3396
Checksum: 337
Coasting Arc #9 (Orbit 3411)
---------------------------------------
Vector Time (GMT): 2010/235/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2529052
96 A = 6740035
78 meter
Y = 6209640
73 meter E =
0006079
Z = -645897
57 I = 51
36080
XDOT = -4687
305317 Wp = 189
82298
YDOT = 1288
349005 meter/sec RA = 243
42333 deg
ZDOT = -5964
933839 TA = 357
22852
MA = 357
23189
Ha = 193
125 n
mi
Hp = 191
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8297417
85 X = 2462565
25
Y = 20372837
05 feet Y = 6237550
35 meter
Z = -2119086
52 Z = -633773
28
XDOT = -15378
298284 XDOT = -4672
387497
YDOT = 4226
866813 feet/sec YDOT = 1236
016054 meter/sec
ZDOT = -19569
992910 ZDOT = -5987
668109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18307341
12 X = -5580077
57
Y = 12204278
37 feet Y = 3719864
05 meter
Z = -2070509
85 Z = -631091
40
XDOT = -6293
903302 XDOT = -1918
381727
YDOT = -12778
237584 feet/sec YDOT = -3894
806816 meter/sec
ZDOT = -19660
927611 ZDOT = -5992
650736
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
89239238
00016717 00000-0 10270-3 0 9080
2 25544 51
6457 244
1567 0008328 285
7868 74
2376 15
71181397 34126
Satellite: ISS
Catalog Number: 25544
Epoch time: 10235
89239238 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 244
1567 deg
Eccentricity:
0008328
Arg of perigee: 285
7868 deg
Mean anomaly: 74
2376 deg
Mean motion: 15
71181397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 340
Coasting Arc #10 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2010/236/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3410390
33 A = 6727979
66 meter
Y = -2472842
12 meter E =
0005863
Z = 5250476
91 I = 51
33545
XDOT = 4229
735115 Wp = 293
84922
YDOT = 6419
867774 meter/sec RA = 238
28382 deg
ZDOT = 278
798095 TA = 153
50554
MA = 153
47556
Ha = 193
223 n
mi
Hp = 191
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11188944
66 X = 3412283
20
Y = -8112999
10 feet Y = -2434694
33 meter
Z = 17225974
13 Z = 5267048
99
XDOT = 13877
083712 XDOT = 4156
278285
YDOT = 21062
558313 feet/sec YDOT = 6466
756497 meter/sec
ZDOT = 914
691914 ZDOT = 299
167158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10317272
73 X = 3144704
73
Y = 9070815
06 feet Y = 2764784
43 meter
Z = 17292241
59 Z = 5270675
24
XDOT = -16904
491967 XDOT = -5152
489152
YDOT = 17344
239460 feet/sec YDOT = 5286
524187 meter/sec
ZDOT = 996
269326 ZDOT = 303
662891
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
91001621
00016717 00000-0 10270-3 0 9098
2 25544 51
6457 238
9519 0008353 290
9744 69
0524 15
71249225 34282
Satellite: ISS
Catalog Number: 25544
Epoch time: 10236
91001621 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 238
9519 deg
Eccentricity:
0008353
Arg of perigee: 290
9744 deg
Mean anomaly: 69
0524 deg
Mean motion: 15
71249225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3428
Checksum: 314
Coasting Arc #11 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2010/237/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4663318
14 A = 6739384
10 meter
Y = -4723215
24 meter E =
0011175
Z = -1123676
08 I = 51
39058
XDOT = 2768
630379 Wp = 350
24164
YDOT = -4131
248413 meter/sec RA = 233
13530 deg
ZDOT = 5877
468801 TA = 357
42434
MA = 357
43009
Ha = 193
429 n
mi
Hp = 190
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15299600
19 X = -4604697
14
Y = -15496112
99 feet Y = -4775035
54 meter
Z = -3686601
31 Z = -1146187
57
XDOT = 9083
433001 XDOT = 2786
069672
YDOT = -13553
964608 feet/sec YDOT = -4100
190140 meter/sec
ZDOT = 19283
034124 ZDOT = 5890
961189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11511299
36 X = 3508644
05
Y = -18466850
08 feet Y = -5628695
90 meter
Z = -3776737
73 Z = -1151149
66
XDOT = 13923
109943 XDOT = 4243
763911
YDOT = 4725
790596 feet/sec YDOT = 1440
420974 meter/sec
ZDOT = 19336
954388 ZDOT = 5893
903698
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
86402474
00016717 00000-0 10270-3 0 9106
2 25544 51
6453 234
0721 0008484 294
9617 65
0663 15
71269385 34434
Satellite: ISS
Catalog Number: 25544
Epoch time: 10237
86402474 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 234
0721 deg
Eccentricity:
0008484
Arg of perigee: 294
9617 deg
Mean anomaly: 65
0663 deg
Mean motion: 15
71269385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 314
Coasting Arc #12 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2010/238/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1218298
91 A = 6729531
46 meter
Y = 4476874
69 meter E =
0008736
Z = -4880776
14 I = 51
37590
XDOT = -6103
064522 Wp = 29
72060
YDOT = -4109
199651 meter/sec RA = 228
03081 deg
ZDOT = -2239
995225 TA = 218
36004
MA = 218
42220
Ha = 193
633 n
mi
Hp = 190
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3997043
66 X = -1244559
87
Y = 14687909
08 feet Y = 4463103
84 meter
Z = -16013045
07 Z = -4886758
62
XDOT = -20023
177565 XDOT = -6045
779703
YDOT = -13481
626152 feet/sec YDOT = -4177
127604 meter/sec
ZDOT = -7349
065700 ZDOT = -2269
504284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15196499
51 X = -4631893
05
Y = -112125
20 feet Y = -34175
76 meter
Z = -16036909
75 Z = -4888050
09
XDOT = 8059
462550 XDOT = 2456
524185
YDOT = -21604
070624 feet/sec YDOT = -6584
920726 meter/sec
ZDOT = -7467
198846 ZDOT = -2276
002208
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
88161797
00016717 00000-0 10270-3 0 9110
2 25544 51
6445 228
8673 0008552 298
6324 61
3978 15
71298126 34594
Satellite: ISS
Catalog Number: 25544
Epoch time: 10238
88161797 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 228
8673 deg
Eccentricity:
0008552
Arg of perigee: 298
6324 deg
Mean anomaly: 61
3978 deg
Mean motion: 15
71298126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 348
Coasting Arc #13 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2010/239/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5703053
47 A = 6736392
90 meter
Y = 2316159
16 meter E =
0006518
Z = 2734544
38 I = 51
42166
XDOT = 144
355331 Wp = 70
22735
YDOT = 5724
543244 meter/sec RA = 222
85783 deg
ZDOT = -5137
649387 TA = 78
48538
MA = 78
41220
Ha = 193
769 n
mi
Hp = 190
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18710805
35 X = 5663446
02
Y = 7598947
39 feet Y = 2379712
82 meter
Z = 8971602
30 Z = 2762153
36
XDOT = 473
606730 XDOT = 105
289374
YDOT = 18781
309857 feet/sec YDOT = 5725
938794 meter/sec
ZDOT = -16855
805074 ZDOT = -5137
043324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2357445
62 X = -718549
43
Y = 20007138
59 feet Y = 6098175
84 meter
Z = 9082111
08 Z = 2768227
46
XDOT = -16491
243833 XDOT = -5026
531120
YDOT = 5725
074322 feet/sec YDOT = 1745
002653 meter/sec
ZDOT = -16853
283941 ZDOT = -5136
880945
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
89919443
00016717 00000-0 10270-3 0 9122
2 25544 51
6452 223
6628 0008597 303
0647 56
9689 15
71355884 34755
Satellite: ISS
Catalog Number: 25544
Epoch time: 10239
89919443 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 223
6628 deg
Eccentricity:
0008597
Arg of perigee: 303
0647 deg
Mean anomaly: 56
9689 deg
Mean motion: 15
71355884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 351
Coasting Arc #14 (Orbit 3490)
---------------------------------------
Vector Time (GMT): 2010/240/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1519954
01 A = 6732930
59 meter
Y = -5202357
69 meter E =
0004813
Z = 3989239
40 I = 51
43144
XDOT = 6530
189500 Wp = 52
87641
YDOT = 1101
725987 meter/sec RA = 217
77511 deg
ZDOT = 3924
459159 TA = 356
42634
MA = 356
42978
Ha = 193
982 n
mi
Hp = 190
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4986725
75 X = -1481046
31
Y = -17068102
64 feet Y = -5219136
98 meter
Z = 13088055
78 Z = 3981950
23
XDOT = 21424
506234 XDOT = 6498
320156
YDOT = 3614
586573 feet/sec YDOT = 1174
572484 meter/sec
ZDOT = 12875
522175 ZDOT = 3956
105329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14938917
36 X = 4553382
01
Y = -9684073
76 feet Y = -2951705
68 meter
Z = 13058798
91 Z = 3980321
91
XDOT = 1863
337771 XDOT = 567
945353
YDOT = 20409
356078 feet/sec YDOT = 6220
771733 meter/sec
ZDOT = 13002
171380 ZDOT = 3963
061837
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
91675601
00016717 00000-0 10270-3 0 9133
2 25544 51
6442 218
4570 0008580 306
6078 53
4294 15
71323998 34914
Satellite: ISS
Catalog Number: 25544
Epoch time: 10240
91675601 = yrday
fracday
Element set: 913
Inclination: 51
6442 deg
RA of node: 218
4570 deg
Eccentricity:
0008580
Arg of perigee: 306
6078 deg
Mean anomaly: 53
4294 deg
Mean motion: 15
71323998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3491
Checksum: 311
Coasting Arc #15 (Orbit 3505)
---------------------------------------
Vector Time (GMT): 2010/241/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5373802
64 A = 6732476
71 meter
Y = 380870
96 meter E =
0002980
Z = -4036064
97 I = 51
45450
XDOT = -3310
206673 Wp = 9
72552
YDOT = -5772
385061 meter/sec RA = 212
59408 deg
ZDOT = 3865
944155 TA = 300
22339
MA = 300
25289
Ha = 193
898 n
mi
Hp = 189
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17630586
07 X = -5358055
70
Y = 1249576
65 feet Y = 320865
78 meter
Z = -13241682
97 Z = -4062132
71
XDOT = -10860
258113 XDOT = -3264
192873
YDOT = -18938
271198 feet/sec YDOT = -5809
144359 meter/sec
ZDOT = 12683
543815 ZDOT = 3849
975120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6444241
95 X = -1964204
95
Y = -16373680
92 feet Y = -4990697
94 meter
Z = -13345991
68 Z = -4067858
26
XDOT = 13603
730767 XDOT = 4146
417138
YDOT = -15631
331490 feet/sec YDOT = -4764
429838 meter/sec
ZDOT = 12619
539844 ZDOT = 3846
435745
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
87070205
00016717 00000-0 10270-3 0 9149
2 25544 51
6433 213
5768 0008483 309
3344 50
7065 15
71375769 35063
Satellite: ISS
Catalog Number: 25544
Epoch time: 10241
87070205 = yrday
fracday
Element set: 914
Inclination: 51
6433 deg
RA of node: 213
5768 deg
Eccentricity:
0008483
Arg of perigee: 309
3344 deg
Mean anomaly: 50
7065 deg
Mean motion: 15
71375769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3506
Checksum: 306
Coasting Arc #16 (Orbit 3521)
---------------------------------------
Vector Time (GMT): 2010/242/20:40:59
340
Vector Time (MET): N/A
Weight (LBS) : 826387
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4141144
16 A = 6736491
58 meter
Y = 4578346
44 meter E =
0003721
Z = -2698882
62 I = 51
49362
XDOT = -5393
660107 Wp = 325
26332
YDOT = 1827
592217 meter/sec RA = 207
51580 deg
ZDOT = -5169
185134 TA = 245
52655
MA = 245
56536
Ha = 194
171 n
mi
Hp = 189
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13586430
97 X = 4102751
19
Y = 15020821
66 feet Y = 4624440
48 meter
Z = -8854601
77 Z = -2678858
24
XDOT = -17695
735258 XDOT = -5388
584670
YDOT = 5996
037457 feet/sec YDOT = 1767
305352 meter/sec
ZDOT = -16959
268813 ZDOT = -5195
375314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9948215
48 X = -3032216
08
Y = 17682289
45 feet Y = 5389561
83 meter
Z = -8774383
80 Z = -2674432
18
XDOT = -9952
872887 XDOT = -3033
635656
YDOT = -14077
857947 feet/sec YDOT = -4290
931102 meter/sec
ZDOT = -17064
050765 ZDOT = -5201
122673
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
88822850
00016717 00000-0 10270-3 0 9153
2 25544 51
6428 208
3727 0008503 313
4752 46
5702 15
71398282 35220
Satellite: ISS
Catalog Number: 25544
Epoch time: 10242
88822850 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 208
3727 deg
Eccentricity:
0008503
Arg of perigee: 313
4752 deg
Mean anomaly: 46
5702 deg
Mean motion: 15
71398282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3522
Checksum: 307
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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