Date:
September 14th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12260 09 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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
258/09:08:24
308 -0
4 3
8 3
8
N/A 3
4 -0
3 195
8
000/00:08:44
617 -1
8 -0
1 188
2
Coasting Arc #1 (Orbit 3736)
---------------------------------------
Vector Time (GMT): 2010/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5646765
65 A = 6737190
89 meter
Y = 3131948
89 meter E =
0019922
Z = 1878217
21 I = 51
88769
XDOT = -955
781861 Wp = 43
29614
YDOT = -5134
062665 meter/sec RA = 137
79567 deg
ZDOT = 5666
599554 TA = 337
49597
MA = 337
58322
Ha = 195
717 n
mi
Hp = 186
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18526134
01 X = -5690492
09
Y = 10275422
86 feet Y = 3068558
93 meter
Z = 6162129
94 Z = 1850678
77
XDOT = -3135
767262 XDOT = -925
828265
YDOT = -16844
037616 feet/sec YDOT = -5144
583169 meter/sec
ZDOT = 18591
205887 ZDOT = 5662
029227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19865260
18 X = 6054931
30
Y = -7451217
54 feet Y = -2271131
10 meter
Z = 6051825
94 Z = 1844596
55
XDOT = 205
081496 XDOT = 62
508840
YDOT = 15688
438839 feet/sec YDOT = 4781
836158 meter/sec
ZDOT = 18572
813589 ZDOT = 5660
993582
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
55997547
00016717 00000-0 10270-3 0 9002
2 25544 51
6458 138
4489 0008935 4
4822 355
6418 15
71724890 37379
Satellite: ISS
Catalog Number: 25544
Epoch time: 10256
55997547 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 138
4489 deg
Eccentricity:
0008935
Arg of perigee: 4
4822 deg
Mean anomaly: 355
6418 deg
Mean motion: 15
71724890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3737
Checksum: 345
Coasting Arc #2 (Orbit 3751)
---------------------------------------
Vector Time (GMT): 2010/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1968481
92 A = 6727015
45 meter
Y = 3847314
26 meter E =
0016339
Z = -5166862
86 I = 51
87568
XDOT = -5856
649544 Wp = 67
38447
YDOT = 4793
710233 meter/sec RA = 132
66628 deg
ZDOT = 1347
688913 TA = 215
43774
MA = 215
54641
Ha = 195
674 n
mi
Hp = 186
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6458274
00 X = 1950413
99
Y = 12622422
11 feet Y = 3869225
90 meter
Z = -16951649
80 Z = -5157343
90
XDOT = -19214
729475 XDOT = -5916
365259
YDOT = 15727
395777 feet/sec YDOT = 4727
883799 meter/sec
ZDOT = 4421
551551 ZDOT = 1319
092107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4873380
81 X = -1485406
47
Y = -13363334
33 feet Y = -4073144
30 meter
Z = -16913448
17 Z = -5155219
00
XDOT = 20136
486436 XDOT = 6137
601066
YDOT = -12755
084740 feet/sec YDOT = -3887
749829 meter/sec
ZDOT = 4307
013426 ZDOT = 1312
777692
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 10257
51368447
00016717 00000-0 10270-3 0 9011
2 25544 51
6457 133
5678 0008890 7
2912 352
8378 15
71774872 37521
Satellite: ISS
Catalog Number: 25544
Epoch time: 10257
51368447 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 133
5678 deg
Eccentricity:
0008890
Arg of perigee: 7
2912 deg
Mean anomaly: 352
8378 deg
Mean motion: 15
71774872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 336
Coasting Arc #3 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2010/258/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4614482
64 A = 6730306
63 meter
Y = 348892
06 meter E =
0015136
Z = -4900079
49 I = 51
89630
XDOT = -2966
227550 Wp = 47
51339
YDOT = 6702
152956 meter/sec RA = 128
18705 deg
ZDOT = -2310
663663 TA = 199
99261
MA = 200
05197
Ha = 195
764 n
mi
Hp = 188
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15139378
73 X = 4634041
99
Y = 1144658
98 feet Y = 400603
26 meter
Z = -16076376
28 Z = -4877614
84
XDOT = -9731
717683 XDOT = -3029
727020
YDOT = 21988
690799 feet/sec YDOT = 6668
627740 meter/sec
ZDOT = -7580
917530 ZDOT = -2325
227931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9268241
82 X = -2824960
11
Y = -12144864
09 feet Y = -3701754
58 meter
Z = -15986334
06 Z = -4872634
62
XDOT = 21982
855847 XDOT = 6700
374462
YDOT = -6696
709855 feet/sec YDOT = -2041
157164 meter/sec
ZDOT = -7639
204089 ZDOT = -2328
429406
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 10258
40380897
00016717 00000-0 10270-3 0 9024
2 25544 51
6448 129
0113 0006749 355
4649 4
6450 15
71057295 37662
Satellite: ISS
Catalog Number: 25544
Epoch time: 10258
40380897 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 129
0113 deg
Eccentricity:
0006749
Arg of perigee: 355
4649 deg
Mean anomaly: 4
6450 deg
Mean motion: 15
71057295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 320
Coasting Arc #4 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2010/259/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1205963
10 A = 6737004
81 meter
Y = -5972628
62 meter E =
0013941
Z = 2869038
91 I = 51
93650
XDOT = 5616
374164 Wp = 70
51318
YDOT = -1322
895390 meter/sec RA = 123
05202 deg
ZDOT = -5090
210060 TA = 76
73029
MA = 76
57484
Ha = 195
843 n
mi
Hp = 187
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3956571
86 X = 1258723
29
Y = -19595238
25 feet Y = -5958847
76 meter
Z = 9412857
32 Z = 2875025
74
XDOT = 18426
424422 XDOT = 5655
476825
YDOT = -4340
207971 feet/sec YDOT = -1259
871198 meter/sec
ZDOT = -16700
164240 ZDOT = -5062
830816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17058719
71 X = -5199497
77
Y = 10400813
47 feet Y = 3170167
95 meter
Z = 9436782
64 Z = 2876331
35
XDOT = -14981
477054 XDOT = -4566
354206
YDOT = -9446
172641 feet/sec YDOT = -2879
193421 meter/sec
ZDOT = -16590
434027 ZDOT = -5056
764291
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 10259
42155136
00016717 00000-0 10270-3 0 9034
2 25544 51
6445 123
8081 0006719 358
9075 1
2071 15
71050049 37823
Satellite: ISS
Catalog Number: 25544
Epoch time: 10259
42155136 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 123
8081 deg
Eccentricity:
0006719
Arg of perigee: 358
9075 deg
Mean anomaly: 1
2071 deg
Mean motion: 15
71050049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3782
Checksum: 291
Coasting Arc #5 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2010/260/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4830429
37 A = 6734151
55 meter
Y = 2653399
40 meter E =
0012673
Z = 3855758
83 I = 51
94316
XDOT = -238
085067 Wp = 66
15539
YDOT = -6480
979490 meter/sec RA = 118
00878 deg
ZDOT = 4156
057248 TA = 340
56637
MA = 340
61465
Ha = 196
065 n
mi
Hp = 187
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15847865
38 X = -4878471
62
Y = 8705378
61 feet Y = 2599114
15 meter
Z = 12650127
40 Z = 3832175
98
XDOT = -781
118985 XDOT = -185
785109
YDOT = -21263
056068 feet/sec YDOT = -6483
349335 meter/sec
ZDOT = 13635
358425 ZDOT = 4155
027892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17286475
56 X = 5268917
75
Y = 5522529
15 feet Y = 1683266
88 meter
Z = 12555620
73 Z = 3826953
20
XDOT = -14396
646599 XDOT = -4388
097883
YDOT = 14030
666712 feet/sec YDOT = 4276
547214 meter/sec
ZDOT = 13631
158006 ZDOT = 4154
776960
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 10260
43927843
00016717 00000-0 10270-3 0 9040
2 25544 51
6452 118
6044 0006827 2
5726 357
5470 15
71076505 37989
Satellite: ISS
Catalog Number: 25544
Epoch time: 10260
43927843 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 118
6044 deg
Eccentricity:
0006827
Arg of perigee: 2
5726 deg
Mean anomaly: 357
5470 deg
Mean motion: 15
71076505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3798
Checksum: 313
Coasting Arc #6 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2010/261/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1529356
65 A = 6732542
84 meter
Y = 4977836
63 meter E =
0009382
Z = -4272110
12 I = 51
95183
XDOT = -4997
275695 Wp = 65
65733
YDOT = 4611
124078 meter/sec RA = 112
86713 deg
ZDOT = 3593
822650 TA = 240
69270
MA = 240
78648
Ha = 196
007 n
mi
Hp = 187
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5017574
32 X = 1494332
88
Y = 16331485
00 feet Y = 4994742
77 meter
Z = -14016109
31 Z = -4264765
88
XDOT = -16395
261465 XDOT = -5065
924733
YDOT = 15128
359835 feet/sec YDOT = 4554
857886 meter/sec
ZDOT = 11790
756727 ZDOT = 3569
379092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8046551
60 X = 2452588
93
Y = -15098756
96 feet Y = -4602101
12 meter
Z = -13986612
16 Z = -4263119
39
XDOT = 21231
933470 XDOT = 6471
493322
YDOT = 513
778001 feet/sec YDOT = 156
599535 meter/sec
ZDOT = 11692
812628 ZDOT = 3563
969289
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 10261
39338353
00016717 00000-0 10270-3 0 9059
2 25544 51
6456 113
7263 0006884 4
9926 355
1303 15
71109108 38136
Satellite: ISS
Catalog Number: 25544
Epoch time: 10261
39338353 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 113
7263 deg
Eccentricity:
0006884
Arg of perigee: 4
9926 deg
Mean anomaly: 355
1303 deg
Mean motion: 15
71109108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3813
Checksum: 299
Coasting Arc #7 (Orbit 3828)
---------------------------------------
Vector Time (GMT): 2010/262/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3601824
59 A = 6738064
41 meter
Y = -5188984
13 meter E =
0005649
Z = -2354658
62 I = 51
98106
XDOT = 2998
730763 Wp = 62
11481
YDOT = 4542
026623 meter/sec RA = 107
82124 deg
ZDOT = -5429
547755 TA = 144
20479
MA = 144
16691
Ha = 196
014 n
mi
Hp = 187
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11817009
80 X = 3671019
49
Y = -17024226
15 feet Y = -5148319
64 meter
Z = -7725257
92 Z = -2336992
65
XDOT = 9838
355521 XDOT = 2974
093689
YDOT = 14901
662149 feet/sec YDOT = 4575
422103 meter/sec
ZDOT = -17813
476886 ZDOT = -5415
040181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20387851
21 X = -6214217
05
Y = 3858754
60 feet Y = 1176148
40 meter
Z = -7654485
12 Z = -2333087
07
XDOT = 3606
769020 XDOT = 1099
343197
YDOT = -16116
279553 feet/sec YDOT = -4912
242008 meter/sec
ZDOT = -17755
265897 ZDOT = -5411
805045
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 10262
41108197
00016717 00000-0 10270-3 0 9065
2 25544 51
6457 108
5226 0006776 7
8516 352
2751 15
71105833 38298
Satellite: ISS
Catalog Number: 25544
Epoch time: 10262
41108197 = yrday
fracday
Element set: 906
Inclination: 51
6457 deg
RA of node: 108
5226 deg
Eccentricity:
0006776
Arg of perigee: 7
8516 deg
Mean anomaly: 352
2751 deg
Mean motion: 15
71105833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3829
Checksum: 307
Coasting Arc #8 (Orbit 3844)
---------------------------------------
Vector Time (GMT): 2010/263/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3468515
82 A = 6729030
40 meter
Y = -2711904
19 meter E =
0011233
Z = 5086420
50 I = 51
95952
XDOT = 2915
561977 Wp = 29
35040
YDOT = -6921
444446 meter/sec RA = 102
69631 deg
ZDOT = -1690
967768 TA = 76
90648
MA = 76
78113
Ha = 196
091 n
mi
Hp = 187
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11379645
08 X = -3462641
81
Y = -8897323
46 feet Y = -2750657
94 meter
Z = 16687731
30 Z = 5069585
03
XDOT = 9565
492049 XDOT = 3000
956529
YDOT = -22708
151068 feet/sec YDOT = -6888
363560 meter/sec
ZDOT = -5547
794515 ZDOT = -1676
596022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2220001
31 X = 676656
40
Y = 14351983
13 feet Y = 4374484
46 meter
Z = 16620205
69 Z = 5065838
69
XDOT = -21534
748151 XDOT = -6563
791236
YDOT = 9731
467458 feet/sec YDOT = 2966
151281 meter/sec
ZDOT = -5490
240773 ZDOT = -1673
425388
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 10263
42876342
00016717 00000-0 10270-3 0 9072
2 25544 51
6455 103
3185 0006957 11
0297 349
1016 15
71196443 38451
Satellite: ISS
Catalog Number: 25544
Epoch time: 10263
42876342 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 103
3185 deg
Eccentricity:
0006957
Arg of perigee: 11
0297 deg
Mean anomaly: 349
1016 deg
Mean motion: 15
71196443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3845
Checksum: 307
Coasting Arc #9 (Orbit 3860)
---------------------------------------
Vector Time (GMT): 2010/264/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1316779
13 A = 6740066
08 meter
Y = 6575741
69 meter E =
0019254
Z = 553756
42 I = 52
00176
XDOT = -4566
149515 Wp = 38
46731
YDOT = -1430
810191 meter/sec RA = 97
62494 deg
ZDOT = 6036
108287 TA = 327
52692
MA = 327
64523
Ha = 196
137 n
mi
Hp = 187
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4320141
51 X = -1392902
47
Y = 21573955
69 feet Y = 6560591
10 meter
Z = 1816786
14 Z = 547173
96
XDOT = -14980
805497 XDOT = -4579
132849
YDOT = -4694
259156 feet/sec YDOT = -1481
943610 meter/sec
ZDOT = 19803
504878 ZDOT = 6013
894573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17755207
35 X = 5411787
20
Y = -12997953
18 feet Y = -3961776
13 meter
Z = 1790453
47 Z = 545730
22
XDOT = 7026
311774 XDOT = 2141
619829
YDOT = 12357
883757 feet/sec YDOT = 3766
682969 meter/sec
ZDOT = 19714
428023 ZDOT = 6008
957662
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 10264
44643173
00016717 00000-0 10270-3 0 9080
2 25544 51
6452 98
1142 0006980 14
8777 345
2589 15
71189880 38619
Satellite: ISS
Catalog Number: 25544
Epoch time: 10264
44643173 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 98
1142 deg
Eccentricity:
0006980
Arg of perigee: 14
8777 deg
Mean anomaly: 345
2589 deg
Mean motion: 15
71189880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3861
Checksum: 333
Coasting Arc #10 (Orbit 3875)
---------------------------------------
Vector Time (GMT): 2010/265/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4159431
91 A = 6728095
70 meter
Y = -276403
72 meter E =
0018661
Z = -5296126
89 I = 51
96395
XDOT = -18
982650 Wp = 66
18647
YDOT = 7672
611322 meter/sec RA = 92
53246 deg
ZDOT = -409
118322 TA = 199
90072
MA = 199
97360
Ha = 196
172 n
mi
Hp = 187
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13646430
14 X = 4187941
27
Y = -906836
35 feet Y = -229731
62 meter
Z = -17375744
38 Z = -5275851
03
XDOT = -62
279035 XDOT = -102
790365
YDOT = 25172
609324 feet/sec YDOT = 7671
930408 meter/sec
ZDOT = -1342
251712 ZDOT = -409
414939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10905169
00 X = -3323895
51
Y = -8422773
74 feet Y = -2567261
44 meter
Z = -17294452
07 Z = -5271348
99
XDOT = 16092
192860 XDOT = 4904
900384
YDOT = -18034
482514 feet/sec YDOT = -5496
910270 meter/sec
ZDOT = -1343
379706 ZDOT = -409
462134
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 10265
40048100
00016717 00000-0 10270-3 0 9097
2 25544 51
6446 93
2349 0007042 17
8406 342
3002 15
71220760 38766
Satellite: ISS
Catalog Number: 25544
Epoch time: 10265
40048100 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 93
2349 deg
Eccentricity:
0007042
Arg of perigee: 17
8406 deg
Mean anomaly: 342
3002 deg
Mean motion: 15
71220760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3876
Checksum: 277
Coasting Arc #11 (Orbit 3891)
---------------------------------------
Vector Time (GMT): 2010/266/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1265514
88 A = 6739474
49 meter
Y = -6498575
75 meter E =
0014527
Z = 1244872
80 I = 52
00237
XDOT = 4516
768760 Wp = 93
00375
YDOT = -2019
341289 meter/sec RA = 87
42713 deg
ZDOT = -5891
899207 TA = 73
43440
MA = 73
27489
Ha = 196
263 n
mi
Hp = 186
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4151951
70 X = -1198799
96
Y = -21320786
59 feet Y = -6512354
34 meter
Z = 4084228
35 Z = 1238887
66
XDOT = 14818
795143 XDOT = 4567
635708
YDOT = -6625
135464 feet/sec YDOT = -1968
548311 meter/sec
ZDOT = -19330
377976 ZDOT = -5869
832802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10661662
07 X = -3249674
60
Y = 18929854
75 feet Y = 5769819
73 meter
Z = 4060187
90 Z = 1237545
27
XDOT = -14280
315002 XDOT = -4352
640013
YDOT = -3874
809930 feet/sec YDOT = -1181
042067 meter/sec
ZDOT = -19241
918283 ZDOT = -5864
936693
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 10266
41811948
00016717 00000-0 10270-3 0 9109
2 25544 51
6446 88
0308 0007001 22
3657 337
7810 15
71206701 38929
Satellite: ISS
Catalog Number: 25544
Epoch time: 10266
41811948 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 88
0308 deg
Eccentricity:
0007001
Arg of perigee: 22
3657 deg
Mean anomaly: 337
7810 deg
Mean motion: 15
71206701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3892
Checksum: 292
Coasting Arc #12 (Orbit 3907)
---------------------------------------
Vector Time (GMT): 2010/267/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3409860
35 A = 6729920
62 meter
Y = 3160093
16 meter E =
0009411
Z = 4857333
93 I = 51
96733
XDOT = -2812
547744 Wp = 72
10184
YDOT = -6751
743902 meter/sec RA = 82
36627 deg
ZDOT = 2417
170913 TA = 354
41594
MA = 354
42643
Ha = 196
462 n
mi
Hp = 186
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11187205
88 X = -3468540
00
Y = 10367759
71 feet Y = 3121634
48 meter
Z = 15936134
95 Z = 4840625
76
XDOT = -9227
518845 XDOT = -2748
581781
YDOT = -22151
390756 feet/sec YDOT = -6782
837589 meter/sec
ZDOT = 7930
350764 ZDOT = 2403
663494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15299937
91 X = 4663421
07
Y = -828257
51 feet Y = -252452
89 meter
Z = 15869162
03 Z = 4836920
59
XDOT = -6988
180636 XDOT = -2129
997458
YDOT = 21877
649283 feet/sec YDOT = 6668
307501 meter/sec
ZDOT = 7876
159653 ZDOT = 2400
653462
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 10267
43574092
00016717 00000-0 10270-3 0 9119
2 25544 51
6441 82
8255 0007138 25
3418 334
8093 15
71223424 39086
Satellite: ISS
Catalog Number: 25544
Epoch time: 10267
43574092 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 82
8255 deg
Eccentricity:
0007138
Arg of perigee: 25
3418 deg
Mean anomaly: 334
8093 deg
Mean motion: 15
71223424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3908
Checksum: 299
Coasting Arc #13 (Orbit 3922)
---------------------------------------
Vector Time (GMT): 2010/268/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3465804
30 A = 6736317
64 meter
Y = 4984532
73 meter E =
0011042
Z = -2914617
84 I = 51
98338
XDOT = -2931
988694 Wp = 41
92889
YDOT = 4991
496410 meter/sec RA = 77
23207 deg
ZDOT = 5068
896009 TA = 284
74878
MA = 284
87112
Ha = 196
327 n
mi
Hp = 186
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11370749
03 X = 3423967
66
Y = 16353453
84 feet Y = 5023055
24 meter
Z = -9562394
50 Z = -2897882
81
XDOT = -9619
385479 XDOT = -3012
210776
YDOT = 16376
300557 feet/sec YDOT = 4958
261091 meter/sec
ZDOT = 16630
236250 ZDOT = 5054
456851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1237043
93 X = 377050
99
Y = -19911758
64 feet Y = -6069104
03 meter
Z = -9495281
19 Z = -2894161
71
XDOT = 16348
127878 XDOT = 4982
909377
YDOT = -6857
277666 feet/sec YDOT = -2090
098232 meter/sec
ZDOT = 16572
361522 ZDOT = 5051
255792
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 10268
38974509
00016717 00000-0 10270-3 0 9122
2 25544 51
6434 77
9456 0007044 27
2739 332
8792 15
71270882 39230
Satellite: ISS
Catalog Number: 25544
Epoch time: 10268
38974509 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 77
9456 deg
Eccentricity:
0007044
Arg of perigee: 27
2739 deg
Mean anomaly: 332
8792 deg
Mean motion: 15
71270882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3923
Checksum: 336
Coasting Arc #14 (Orbit 3938)
---------------------------------------
Vector Time (GMT): 2010/269/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1504627
82 A = 6733341
31 meter
Y = -5289840
28 meter E =
0012715
Z = -3899567
04 I = 51
96513
XDOT = 4785
806140 Wp = 51
49402
YDOT = 4389
079329 meter/sec RA = 72
18974 deg
ZDOT = -4108
545577 TA = 175
75926
MA = 175
74848
Ha = 196
313 n
mi
Hp = 186
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4936442
97 X = 1582611
68
Y = -17355119
03 feet Y = -5272578
90 meter
Z = -12793855
11 Z = -3892067
59
XDOT = 15701
463715 XDOT = 4756
329873
YDOT = 14399
866564 feet/sec YDOT = 4442
431953 meter/sec
ZDOT = -13479
480238 ZDOT = -4085
367670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14544580
66 X = -4433188
19
Y = 10714105
95 feet Y = 3265659
49 meter
Z = -12763794
94 Z = -3890404
70
XDOT = -2967
592529 XDOT = -904
522203
YDOT = -19971
149797 feet/sec YDOT = -6087
206458 meter/sec
ZDOT = -13386
545750 ZDOT = -4080
219145
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 10269
40733517
00016717 00000-0 10270-3 0 9139
2 25544 51
6427 72
7409 0007067 31
2344 328
9237 15
71295357 39396
Satellite: ISS
Catalog Number: 25544
Epoch time: 10269
40733517 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 72
7409 deg
Eccentricity:
0007067
Arg of perigee: 31
2344 deg
Mean anomaly: 328
9237 deg
Mean motion: 15
71295357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3939
Checksum: 319
Coasting Arc #15 (Orbit 3954)
---------------------------------------
Vector Time (GMT): 2010/270/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4625179
42 A = 6732245
40 meter
Y = -2526089
10 meter E =
0016295
Z = 4183080
32 I = 51
95226
XDOT = 303
359271 Wp = 58
21165
YDOT = -6737
105740 meter/sec RA = 67
04603 deg
ZDOT = -3714
090545 TA = 69
65258
MA = 69
47758
Ha = 196
353 n
mi
Hp = 186
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15174473
18 X = -4616909
49
Y = -8287693
90 feet Y = -2577764
15 meter
Z = 13724016
80 Z = 4160631
03
XDOT = 995
273198 XDOT = 396
714993
YDOT = -22103
365290 feet/sec YDOT = -6733
191633 meter/sec
ZDOT = -12185
336434 ZDOT = -3712
389639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7325950
30 X = 2232949
65
Y = 15739865
05 feet Y = 4797510
87 meter
Z = 13634010
56 Z = 4155646
42
XDOT = -12866
847530 XDOT = -3921
815127
YDOT = 16591
964511 feet/sec YDOT = 5057
230783 meter/sec
ZDOT = -12178
513339 ZDOT = -3712
010866
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 10270
42490754
00016717 00000-0 10270-3 0 9147
2 25544 51
6436 67
5356 0007039 33
8822 326
2788 15
71347847 39559
Satellite: ISS
Catalog Number: 25544
Epoch time: 10270
42490754 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 67
5356 deg
Eccentricity:
0007039
Arg of perigee: 33
8822 deg
Mean anomaly: 326
2788 deg
Mean motion: 15
71347847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3955
Checksum: 330
Coasting Arc #16 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2010/271/09:12:46
617
Vector Time (MET): N/A
Weight (LBS) : 828502
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1054985
67 A = 6736951
94 meter
Y = 6153730
23 meter E =
0019816
Z = 2501571
36 I = 51
95454
XDOT = -5404
998825 Wp = 63
22142
YDOT = -1255
711782 meter/sec RA = 61
99869 deg
ZDOT = 5344
899136 TA = 324
96047
MA = 325
09069
Ha = 196
301 n
mi
Hp = 186
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3461239
07 X = 973942
72
Y = 20189403
64 feet Y = 6165074
68 meter
Z = 8207255
13 Z = 2506499
47
XDOT = -17732
935779 XDOT = -5416
520505
YDOT = -4119
789312 feet/sec YDOT = -1316
217930 meter/sec
ZDOT = 17535
758320 ZDOT = 5318
613271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8959959
93 X = 2730995
79
Y = -18411594
99 feet Y = -5611854
15 meter
Z = 8226999
46 Z = 2507589
44
XDOT = 10776
097626 XDOT = 3284
554556
YDOT = 13067
125401 feet/sec YDOT = 3982
859822 meter/sec
ZDOT = 17430
369500 ZDOT = 5312
776624
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 10271
44246442
00016717 00000-0 10270-3 0 9154
2 25544 51
6426 62
3303 0006964 38
6564 321
5096 15
71369220 39712
Satellite: ISS
Catalog Number: 25544
Epoch time: 10271
44246442 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 62
3303 deg
Eccentricity:
0006964
Arg of perigee: 38
6564 deg
Mean anomaly: 321
5096 deg
Mean motion: 15
71369220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 300
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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