Date:
August 15th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17437 53 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
230/20:35:30
477 1
5 4
0 4
0
N/A -3
1 -0
0 192
1
000/00:11:00
955 2
0 0
2 191
7
Coasting Arc #1 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2010/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4374153
96 A = 6736154
60 meter
Y = 4554438
12 meter E =
0008870
Z = -2329345
20 I = 51
35488
XDOT = -2320
397635 Wp = 182
79373
YDOT = -4981
884880 meter/sec RA = 296
68910 deg
ZDOT = -5391
313153 TA = 23
50852
MA = 23
46800
Ha = 193
260 n
mi
Hp = 188
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14350898
82 X = -4413442
00
Y = 14942382
30 feet Y = 4505304
03 meter
Z = -7642208
68 Z = -2350690
09
XDOT = -7612
853132 XDOT = -2238
327068
YDOT = -16344
766667 feet/sec YDOT = -5007
374115 meter/sec
ZDOT = -17688
035278 ZDOT = -5402
386145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20518987
26 X = 6254187
32
Y = -2623438
87 feet Y = -799624
17 meter
Z = -7727559
07 Z = -2355360
01
XDOT = -4631
198609 XDOT = -1411
589336
YDOT = 15934
339833 feet/sec YDOT = 4856
786781 meter/sec
ZDOT = -17732
308481 ZDOT = -5404
807625
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 10225
52713179
00016717 00000-0 10270-3 0 9002
2 25544 51
6454 297
1838 0006660 222
9112 137
1531 15
71758576 32493
Satellite: ISS
Catalog Number: 25544
Epoch time: 10225
52713179 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 297
1838 deg
Eccentricity:
0006660
Arg of perigee: 222
9112 deg
Mean anomaly: 137
1531 deg
Mean motion: 15
71758576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 309
Coasting Arc #2 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2010/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2928571
48 A = 6727523
83 meter
Y = 3445988
26 meter E =
0001197
Z = 4980666
58 I = 51
31440
XDOT = -4096
112561 Wp = 192
27934
YDOT = 6232
502662 meter/sec RA = 291
51232 deg
ZDOT = -1904
872896 TA = 276
19712
MA = 276
21076
Ha = 192
918 n
mi
Hp = 188
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9608174
15 X = 2865625
13
Y = 11305735
76 feet Y = 3478385
32 meter
Z = 16340769
63 Z = 4994740
62
XDOT = -13438
689503 XDOT = -4156
247645
YDOT = 20447
843380 feet/sec YDOT = 6186
361258 meter/sec
ZDOT = -6249
582992 ZDOT = -1924
917710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -540383
94 X = -164709
02
Y = -14764901
81 feet Y = -4500342
07 meter
Z = 16397044
96 Z = 4997819
30
XDOT = 22069
278244 XDOT = 6726
716009
YDOT = -7832
657583 feet/sec YDOT = -2387
394031 meter/sec
ZDOT = -6329
731230 ZDOT = -1929
302079
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 10226
54439725
00016717 00000-0 10270-3 0 9018
2 25544 51
6459 291
9770 0006663 228
6184 131
4406 15
71827300 32658
Satellite: ISS
Catalog Number: 25544
Epoch time: 10226
54439725 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 291
9770 deg
Eccentricity:
0006663
Arg of perigee: 228
6184 deg
Mean anomaly: 131
4406 deg
Mean motion: 15
71827300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 310
Coasting Arc #3 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2010/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2623761
47 A = 6738047
09 meter
Y = -6123805
41 meter E =
0007400
Z = 985489
07 I = 51
33872
XDOT = 4121
362937 Wp = 58
80538
YDOT = 2720
208975 meter/sec RA = 286
39631 deg
ZDOT = 5901
709439 TA = 311
99556
MA = 312
05856
Ha = 192
874 n
mi
Hp = 188
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8608141
30 X = 2687256
67
Y = -20091225
10 feet Y = -6094109
94 meter
Z = 3233231
86 Z = 998389
32
XDOT = 13521
531944 XDOT = 4061
969452
YDOT = 8924
570128 feet/sec YDOT = 2765
964293 meter/sec
ZDOT = 19362
563776 ZDOT = 5921
586724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18948592
59 X = -5775531
02
Y = 10879892
90 feet Y = 3316191
36 meter
Z = 3284810
52 Z = 1001210
25
XDOT = -4544
936042 XDOT = -1385
296506
YDOT = -13813
574196 feet/sec YDOT = -4210
377415 meter/sec
ZDOT = 19442
045216 ZDOT = 5925
935382
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 10227
56165029
00016717 00000-0 10270-3 0 9025
2 25544 51
6452 286
7702 0006333 232
3221 127
7367 15
71787422 32818
Satellite: ISS
Catalog Number: 25544
Epoch time: 10227
56165029 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 286
7702 deg
Eccentricity:
0006333
Arg of perigee: 232
3221 deg
Mean anomaly: 127
7367 deg
Mean motion: 15
71787422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 297
Coasting Arc #4 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2010/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4046287
43 A = 6726356
49 meter
Y = -1203840
39 meter E =
0010544
Z = -5245143
18 I = 51
29211
XDOT = 1769
516210 Wp = 113
96297
YDOT = -7476
028719 meter/sec RA = 281
24132 deg
ZDOT = 347
125380 TA = 159
37433
MA = 159
33173
Ha = 192
598 n
mi
Hp = 188
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13275221
23 X = -4007045
31
Y = -3949607
57 feet Y = -1248868
77 meter
Z = -17208475
01 Z = -5264704
68
XDOT = 5805
499377 XDOT = 1851
296754
YDOT = -24527
653279 feet/sec YDOT = -7455
783685 meter/sec
ZDOT = 1138
862794 ZDOT = 355
919983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8334522
84 X = 2540362
56
Y = 10939304
27 feet Y = 3334299
94 meter
Z = -17286696
10 Z = -5268984
97
XDOT = -18311
734887 XDOT = -5581
416794
YDOT = 15825
664013 feet/sec YDOT = 4823
662391 meter/sec
ZDOT = 1174
021716 ZDOT = 357
841819
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
51530650
00016717 00000-0 10270-3 0 9038
2 25544 51
6450 281
8886 0006412 236
2327 123
8224 15
71822136 32960
Satellite: ISS
Catalog Number: 25544
Epoch time: 10228
51530650 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 281
8886 deg
Eccentricity:
0006412
Arg of perigee: 236
2327 deg
Mean anomaly: 123
8224 deg
Mean motion: 15
71822136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 292
Coasting Arc #5 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2010/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -411976
50 A = 6738135
08 meter
Y = 6706874
88 meter E =
0012343
Z = 378386
02 I = 51
32821
XDOT = -4831
081111 Wp = 159
33935
YDOT = 44
249769 meter/sec RA = 276
09815 deg
ZDOT = -5996
232142 TA = 16
53110
MA = 16
49089
Ha = 192
290 n
mi
Hp = 189
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1351628
93 X = -488781
50
Y = 22004182
68 feet Y = 6701838
45 meter
Z = 1241423
94 Z = 376198
45
XDOT = -15850
003645 XDOT = -4802
088468
YDOT = 145
176408 feet/sec YDOT = -9
611847 meter/sec
ZDOT = -19672
677632 ZDOT = -6019
630936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13739954
95 X = 4187938
27
Y = -17240829
70 feet Y = -5255004
89 meter
Z = 1232687
53 Z = 375723
16
XDOT = 11710
618770 XDOT = 3569
396601
YDOT = 7908
093330 feet/sec YDOT = 2410
386847 meter/sec
ZDOT = -19766
246215 ZDOT = -6024
751846
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
53252436
00016717 00000-0 10270-3 0 9045
2 25544 51
6455 276
6818 0006209 240
4634 119
5910 15
71888243 33128
Satellite: ISS
Catalog Number: 25544
Epoch time: 10229
53252436 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 276
6818 deg
Eccentricity:
0006209
Arg of perigee: 240
4634 deg
Mean anomaly: 119
5910 deg
Mean motion: 15
71888243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 307
Coasting Arc #6 (Orbit 3327)
---------------------------------------
Vector Time (GMT): 2010/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4144904
45 A = 6726563
63 meter
Y = -1280663
80 meter E =
0005493
Z = 5143449
71 I = 51
28666
XDOT = 836
266968 Wp = 203
77509
YDOT = 7554
760259 meter/sec RA = 270
96928 deg
ZDOT = 1202
627839 TA = 234
64574
MA = 234
69709
Ha = 192
074 n
mi
Hp = 189
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13598767
88 X = 4133931
33
Y = -4201652
89 feet Y = -1234374
65 meter
Z = 16874835
01 Z = 5163558
71
XDOT = 2743
658031 XDOT = 745
884017
YDOT = 24785
958856 feet/sec YDOT = 7563
606469 meter/sec
ZDOT = 3945
629394 ZDOT = 1206
471284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13537670
73 X = -4126282
04
Y = -4073253
46 feet Y = -1241527
65 meter
Z = 16955250
19 Z = 5167960
26
XDOT = 11320
783181 XDOT = 3450
574713
YDOT = -21075
823398 feet/sec YDOT = -6423
910972 meter/sec
ZDOT = 3961
019859 ZDOT = 1207
318853
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
54972568
00016717 00000-0 10270-3 0 9054
2 25544 51
6448 271
4751 0006178 243
9911 116
0615 15
71903551 33281
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
54972568 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 271
4751 deg
Eccentricity:
0006178
Arg of perigee: 243
9911 deg
Mean anomaly: 116
0615 deg
Mean motion: 15
71903551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3328
Checksum: 309
Coasting Arc #7 (Orbit 3332)
---------------------------------------
Vector Time (GMT): 2010/230/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2364434
43 A = 6736841
70 meter
Y = -5630420
48 meter E =
0004485
Z = -2838915
55 I = 51
31472
XDOT = 3979
606494 Wp = 292
46194
YDOT = -4222
069389 meter/sec RA = 269
07472 deg
ZDOT = 5054
476009 TA = 34
85114
MA = 34
82177
Ha = 192
143 n
mi
Hp = 191
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7757330
80 X = -2287507
54
Y = -18472508
12 feet Y = -5656430
71 meter
Z = -9314027
40 Z = -2850215
31
XDOT = 13056
451751 XDOT = 4001
969246
YDOT = -13851
933692 feet/sec YDOT = -4177
442307 meter/sec
ZDOT = 16582
926538 ZDOT = 5073
862772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17468991
72 X = 5324548
68
Y = -9767286
72 feet Y = -2977068
99 meter
Z = -9359235
13 Z = -2852694
87
XDOT = 14532
261750 XDOT = 4429
433381
YDOT = 10012
199271 feet/sec YDOT = 3051
718338 meter/sec
ZDOT = 16660
445747 ZDOT = 5078
103864
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
86759800
00016717 00000-0 10270-3 0 9062
2 25544 51
6458 269
8482 0008286 267
3247 92
6966 15
71125290 33338
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
86759800 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 269
8482 deg
Eccentricity:
0008286
Arg of perigee: 267
3247 deg
Mean anomaly: 92
6966 deg
Mean motion: 15
71125290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3333
Checksum: 334
Coasting Arc #8 (Orbit 3348)
---------------------------------------
Vector Time (GMT): 2010/231/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2592368
03 A = 6733802
58 meter
Y = 4873701
57 meter E =
0002904
Z = -3856144
45 I = 51
30677
XDOT = -3840
559362 Wp = 315
23848
YDOT = -5273
258713 meter/sec RA = 263
98749 deg
ZDOT = -4078
973099 TA = 271
95949
MA = 271
99275
Ha = 191
913 n
mi
Hp = 191
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8505144
45 X = -2627941
83
Y = 15989834
53 feet Y = 4844513
46 meter
Z = -12651392
56 Z = -3868824
12
XDOT = -12600
260374 XDOT = -3761
492784
YDOT = -17300
717562 feet/sec YDOT = -5315
763845 meter/sec
ZDOT = -13382
457675 ZDOT = -4097
438467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16959861
17 X = -5169365
68
Y = -6252215
96 feet Y = -1905675
42 meter
Z = -12702083
65 Z = -3871595
10
XDOT = 15046
785912 XDOT = 4586
260346
YDOT = -13452
201509 feet/sec YDOT = -4100
231020 meter/sec
ZDOT = -13456
334000 ZDOT = -4101
490603
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
88528946
00016717 00000-0 10270-3 0 9071
2 25544 51
6462 264
6450 0008315 271
9088 88
1122 15
71150744 33491
Satellite: ISS
Catalog Number: 25544
Epoch time: 10231
88528946 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 264
6450 deg
Eccentricity:
0008315
Arg of perigee: 271
9088 deg
Mean anomaly: 88
1122 deg
Mean motion: 15
71150744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3349
Checksum: 316
Coasting Arc #9 (Orbit 3364)
---------------------------------------
Vector Time (GMT): 2010/232/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4079147
80 A = 6732553
68 meter
Y = 3344479
93 meter E =
0003980
Z = 4184707
10 I = 51
30645
XDOT = -1662
329732 Wp = 21
95651
YDOT = 6576
265678 meter/sec RA = 258
79945 deg
ZDOT = -3630
698250 TA = 105
26706
MA = 105
22306
Ha = 192
567 n
mi
Hp = 191
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13383030
84 X = 4021117
88
Y = 10972703
18 feet Y = 3389770
77 meter
Z = 13729354
01 Z = 4204382
40
XDOT = -5453
837702 XDOT = -1718
106255
YDOT = 21575
674798 feet/sec YDOT = 6557
364795 meter/sec
ZDOT = -11911
739666 ZDOT = -3638
908907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8873991
15 X = -2704792
50
Y = 14784799
98 feet Y = 4506407
03 meter
Z = 13808072
34 Z = 4208700
45
XDOT = -21057
666850 XDOT = -6418
376856
YDOT = -1469
100724 feet/sec YDOT = -447
781901 meter/sec
ZDOT = -11944
540728 ZDOT = -3640
696014
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
90296518
00016717 00000-0 10270-3 0 9083
2 25544 51
6454 259
4415 0008294 276
1468 83
8749 15
71175376 33653
Satellite: ISS
Catalog Number: 25544
Epoch time: 10232
90296518 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 259
4415 deg
Eccentricity:
0008294
Arg of perigee: 276
1468 deg
Mean anomaly: 83
8749 deg
Mean motion: 15
71175376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3365
Checksum: 340
Coasting Arc #10 (Orbit 3380)
---------------------------------------
Vector Time (GMT): 2010/233/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 171887
57 A = 6737707
76 meter
Y = -6284780
21 meter E =
0007389
Z = 2409301
85 I = 51
33093
XDOT = 5092
322525 Wp = 44
79117
YDOT = 2188
453358 meter/sec RA = 253
70791 deg
ZDOT = 5340
603595 TA = 342
48721
MA = 342
51268
Ha = 192
774 n
mi
Hp = 191
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 563935
58 X = 230448
65
Y = -20619357
63 feet Y = -6282530
68 meter
Z = 7904533
62 Z = 2410278
96
XDOT = 16707
094898 XDOT = 5041
529221
YDOT = 7179
965084 feet/sec YDOT = 2245
114638 meter/sec
ZDOT = 17521
665339 ZDOT = 5365
218256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20419937
57 X = 6223996
97
Y = -2905351
08 feet Y = -885551
01 meter
Z = 7908392
29 Z = 2410477
97
XDOT = -4543
135173 XDOT = -1384
747601
YDOT = 16073
934766 feet/sec YDOT = 4899
335317 meter/sec
ZDOT = 17620
143944 ZDOT = 5370
619874
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
92062471
00016717 00000-0 10270-3 0 9096
2 25544 51
6456 254
2369 0008310 280
4876 79
5349 15
71176472 33810
Satellite: ISS
Catalog Number: 25544
Epoch time: 10233
92062471 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 254
2369 deg
Eccentricity:
0008310
Arg of perigee: 280
4876 deg
Mean anomaly: 79
5349 deg
Mean motion: 15
71176472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3381
Checksum: 320
Coasting Arc #11 (Orbit 3395)
---------------------------------------
Vector Time (GMT): 2010/234/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4474769
27 A = 6729067
40 meter
Y = -408954
73 meter E =
0004935
Z = -5013393
72 I = 51
31200
XDOT = -1343
949137 Wp = 103
04052
YDOT = -7357
362758 meter/sec RA = 248
53520 deg
ZDOT = 1800
108663 TA = 184
40216
MA = 184
40651
Ha = 192
828 n
mi
Hp = 191
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14681001
55 X = -4445510
04
Y = -1341715
01 feet Y = -458830
68 meter
Z = -16448142
11 Z = -5035060
62
XDOT = -4409
281944 XDOT = -1270
322291
YDOT = -24138
329257 feet/sec YDOT = -7371
979936 meter/sec
ZDOT = 5905
868316 ZDOT = 1793
758716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1342881
04 X = -409310
14
Y = -14583200
48 feet Y = -4444959
51 meter
Z = -16534821
40 Z = -5039813
56
XDOT = 21857
591774 XDOT = 6662
193973
YDOT = -8678
635371 feet/sec YDOT = -2645
248061 meter/sec
ZDOT = 5880
393825 ZDOT = 1792
344038
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
87466396
00016717 00000-0 10270-3 0 9107
2 25544 51
6455 249
3582 0008423 283
8246 76
1978 15
71229262 33967
Satellite: ISS
Catalog Number: 25544
Epoch time: 10234
87466396 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 249
3582 deg
Eccentricity:
0008423
Arg of perigee: 283
8246 deg
Mean anomaly: 76
1978 deg
Mean motion: 15
71229262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3396
Checksum: 338
Coasting Arc #12 (Orbit 3411)
---------------------------------------
Vector Time (GMT): 2010/235/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2480977
49 A = 6739935
23 meter
Y = 6222368
77 meter E =
0005914
Z = -707141
64 I = 51
36036
XDOT = -4720
881674 Wp = 192
14723
YDOT = 1205
084391 meter/sec RA = 243
42095 deg
ZDOT = -5955
750262 TA = 355
57682
MA = 355
58205
Ha = 193
152 n
mi
Hp = 191
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8139689
92 X = 2414648
53
Y = 20414595
69 feet Y = 6249741
67 meter
Z = -2320018
51 Z = -695250
51
XDOT = -15488
456936 XDOT = -4705
074890
YDOT = 3953
688947 feet/sec YDOT = 1152
380940 meter/sec
ZDOT = -19539
863063 ZDOT = -5978
645482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18378039
60 X = -5601626
47
Y = 12061373
47 feet Y = 3676306
63 meter
Z = -2272374
45 Z = -692619
73
XDOT = -6060
306128 XDOT = -1847
181308
YDOT = -12934
842501 feet/sec YDOT = -3942
539994 meter/sec
ZDOT = -19631
442631 ZDOT = -5983
663714
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
89229146
00016717 00000-0 10270-3 0 9111
2 25544 51
6454 244
1542 0008413 286
5814 73
4423 15
71204225 34121
Satellite: ISS
Catalog Number: 25544
Epoch time: 10235
89229146 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 244
1542 deg
Eccentricity:
0008413
Arg of perigee: 286
5814 deg
Mean anomaly: 73
4423 deg
Mean motion: 15
71204225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 286
Coasting Arc #13 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2010/236/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3459073
60 A = 6727893
03 meter
Y = -2398269
23 meter E =
0006048
Z = 5253188
64 I = 51
33509
XDOT = 4178
142749 Wp = 296
16039
YDOT = 6456
485273 meter/sec RA = 238
27993 deg
ZDOT = 199
235359 TA = 151
95517
MA = 151
92257
Ha = 193
239 n
mi
Hp = 190
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11348666
67 X = 3460115
79
Y = -7868337
37 feet Y = -2359581
79 meter
Z = 17234870
86 Z = 5269995
15
XDOT = 13707
817419 XDOT = 4104
666784
YDOT = 21182
694466 feet/sec YDOT = 6502
796950 meter/sec
ZDOT = 653
659314 ZDOT = 219
353742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10114003
98 X = 3082748
41
Y = 9278404
45 feet Y = 2828057
68 meter
Z = 17302077
22 Z = 5273673
14
XDOT = -17040
782453 XDOT = -5194
030492
YDOT = 17223
366545 feet/sec YDOT = 5249
682123 meter/sec
ZDOT = 734
234321 ZDOT = 223
794621
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
90989998
00016717 00000-0 10270-3 0 9123
2 25544 51
6453 238
9492 0008439 291
7299 68
2964 15
71274739 34284
Satellite: ISS
Catalog Number: 25544
Epoch time: 10236
90989998 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 238
9492 deg
Eccentricity:
0008439
Arg of perigee: 291
7299 deg
Mean anomaly: 68
2964 deg
Mean motion: 15
71274739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3428
Checksum: 371
Coasting Arc #14 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2010/237/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4626968
12 A = 6739380
07 meter
Y = -4775994
41 meter E =
0011428
Z = -1047212
43 I = 51
39051
XDOT = 2847
425871 Wp = 351
21055
YDOT = -4050
797047 meter/sec RA = 233
13258 deg
ZDOT = 5896
048917 TA = 357
30627
MA = 357
31242
Ha = 193
442 n
mi
Hp = 190
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15180341
60 X = -4568131
08
Y = -15669272
98 feet Y = -4827407
01 meter
Z = -3435736
32 Z = -1069546
81
XDOT = 9341
948396 XDOT = 2863
869428
YDOT = -13290
016558 feet/sec YDOT = -4018
863203 meter/sec
ZDOT = 19343
992509 ZDOT = 5909
921665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11704955
08 X = 3567670
31
Y = -18394031
91 feet Y = -5606500
93 meter
Z = -3525164
92 Z = -1074470
27
XDOT = 13732
554851 XDOT = 4185
682719
YDOT = 5022
425524 feet/sec YDOT = 1530
835300 meter/sec
ZDOT = 19399
435755 ZDOT = 5912
948018
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
86389305
00016717 00000-0 10270-3 0 9136
2 25544 51
6449 234
0693 0008562 295
6897 64
3380 15
71296789 34438
Satellite: ISS
Catalog Number: 25544
Epoch time: 10237
86389305 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 234
0693 deg
Eccentricity:
0008562
Arg of perigee: 295
6897 deg
Mean anomaly: 64
3380 deg
Mean motion: 15
71296789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 348
Coasting Arc #15 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2010/238/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1306241
64 A = 6729310
35 meter
Y = 4416843
78 meter E =
0008920
Z = -4912458
72 I = 51
37512
XDOT = -6079
485596 Wp = 30
74949
YDOT = -4192
766852 meter/sec RA = 228
02650 deg
ZDOT = -2147
372974 TA = 218
27906
MA = 218
34241
Ha = 193
640 n
mi
Hp = 190
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4285569
70 X = -1331670
89
Y = 14490957
29 feet Y = 4402094
15 meter
Z = -16116990
54 Z = -4918866
40
XDOT = -19945
818883 XDOT = -6021
718004
YDOT = -13755
796759 feet/sec YDOT = -4260
428427 meter/sec
ZDOT = -7045
186923 ZDOT = -2176
766310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15077700
86 X = -4595683
22
Y = -438305
48 feet Y = -133595
51 meter
Z = -16142557
42 Z = -4920251
50
XDOT = 8317
345525 XDOT = 2535
126916
YDOT = -21608
991363 feet/sec YDOT = -6586
420568 meter/sec
ZDOT = -7162
858400 ZDOT = -2183
239240
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
88146849
00016717 00000-0 10270-3 0 9144
2 25544 51
6441 228
8643 0008630 299
3869 60
6431 15
71327568 34595
Satellite: ISS
Catalog Number: 25544
Epoch time: 10238
88146849 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 228
8643 deg
Eccentricity:
0008630
Arg of perigee: 299
3869 deg
Mean anomaly: 60
6431 deg
Mean motion: 15
71327568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 343
Coasting Arc #16 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2010/239/20:41:00
955
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5704542
54 A = 6736506
65 meter
Y = 2407770
72 meter E =
0006486
Z = 2651215
64 I = 51
42200
XDOT = 24
651519 Wp = 71
90418
YDOT = 5674
848370 meter/sec RA = 222
85436 deg
ZDOT = -5194
410858 TA = 77
86423
MA = 77
79157
Ha = 193
775 n
mi
Hp = 190
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18715690
75 X = 5664315
36
Y = 7899510
22 feet Y = 2471337
56 meter
Z = 8698214
03 Z = 2678830
33
XDOT = 80
877688 XDOT = -13
574108
YDOT = 18618
268929 feet/sec YDOT = 5674
910015 meter/sec
ZDOT = -17042
030375 ZDOT = -5194
384270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2643052
76 X = -805602
48
Y = 20093743
14 feet Y = 6124572
91 meter
Z = 8808747
25 Z = 2684906
16
XDOT = -16431
430421 XDOT = -5008
299992
YDOT = 5327
115167 feet/sec YDOT = 1623
704703 meter/sec
ZDOT = -17041
828684 ZDOT = -5194
349383
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
89902590
00016717 00000-0 10270-3 0 9150
2 25544 51
6449 223
6597 0008669 303
7864 56
2472 15
71384928 34758
Satellite: ISS
Catalog Number: 25544
Epoch time: 10239
89902590 = yrday
fracday
Element set: 915
Inclination: 51
6449 deg
RA of node: 223
6597 deg
Eccentricity:
0008669
Arg of perigee: 303
7864 deg
Mean anomaly: 56
2472 deg
Mean motion: 15
71384928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 352
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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