Date:
July 28th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8880 23 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 2979)
---------------------------------------
Vector Time (GMT): 2010/208/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5593976
34 A = 6734057
59 meter
Y = 646179
01 meter E =
0015774
Z = 3675431
36 I = 51
78783
XDOT = -3477
261292 Wp = 109
99564
YDOT = -5327
330457 meter/sec RA = 24
33098 deg
ZDOT = -4346
054904 TA = 25
92703
MA = 25
84808
Ha = 196
274 n
mi
Hp = 186
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18352940
75 X = -5618640
45
Y = 2120009
87 feet Y = 583485
61 meter
Z = 12058501
84 Z = 3648196
59
XDOT = -11408
337572 XDOT = -3396
319810
YDOT = -17478
118298 feet/sec YDOT = -5365
762334 meter/sec
ZDOT = -14258
710314 ZDOT = -4362
750903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -588585
71 X = -179400
92
Y = 18536274
98 feet Y = 5649856
61 meter
Z = 11949578
21 Z = 3642231
44
XDOT = -17591
172354 XDOT = -5361
789334
YDOT = 8697
160616 feet/sec YDOT = 2650
894556 meter/sec
ZDOT = -14325
425943 ZDOT = -4366
389827
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 10208
42135606
00016717 00000-0 10270-3 0 9005
2 25544 51
6461 24
6869 0007109 156
0301 204
1193 15
71318315 29807
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208
42135606 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 24
6869 deg
Eccentricity:
0007109
Arg of perigee: 156
0301 deg
Mean anomaly: 204
1193 deg
Mean motion: 15
71318315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 276
Coasting Arc #2 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2010/209/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4323530
30 A = 6735628
52 meter
Y = 4113538
89 meter E =
0016416
Z = 3116620
96 I = 51
76403
XDOT = -5559
592175 Wp = 110
12131
YDOT = 2127
643949 meter/sec RA = 19
27540 deg
ZDOT = 4878
099003 TA = 285
98971
MA = 286
17049
Ha = 196
088 n
mi
Hp = 186
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14184810
69 X = 4262070
96
Y = 13495862
51 feet Y = 4161543
35 meter
Z = 10225134
38 Z = 3137475
22
XDOT = -18240
131807 XDOT = -5606
667103
YDOT = 6980
459149 feet/sec YDOT = 2065
209731 meter/sec
ZDOT = 16004
261820 ZDOT = 4850
976866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15202542
06 X = 4633734
82
Y = -12268588
04 feet Y = -3739465
64 meter
Z = 10308491
39 Z = 3142028
17
XDOT = 3667
337869 XDOT = 1117
804583
YDOT = 17972
248025 feet/sec YDOT = 5477
941198 meter/sec
ZDOT = 15895
776677 ZDOT = 4845
032731
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 10209
43894824
00016717 00000-0 10270-3 0 9012
2 25544 51
6451 19
4817 0007132 160
5853 199
5582 15
71289510 29969
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209
43894824 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 19
4817 deg
Eccentricity:
0007132
Arg of perigee: 160
5853 deg
Mean anomaly: 199
5582 deg
Mean motion: 15
71289510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 325
Coasting Arc #3 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2010/210/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3852262
72 A = 6730298
20 meter
Y = -2876537
27 meter E =
0016302
Z = -4725089
92 I = 51
71634
XDOT = 6132
831492 Wp = 129
83370
YDOT = 3750
621062 meter/sec RA = 14
12118 deg
ZDOT = 2712
611111 TA = 166
91581
MA = 166
87347
Ha = 196
032 n
mi
Hp = 186
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12638657
22 X = 3907095
60
Y = -9437458
24 feet Y = -2833152
13 meter
Z = -15502263
53 Z = -4706242
93
XDOT = 20120
838229 XDOT = 6077
258418
YDOT = 12305
187210 feet/sec YDOT = 3818
891184 meter/sec
ZDOT = 8899
642752 ZDOT = 2742
269086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7957073
02 X = -2425315
86
Y = -13704677
99 feet Y = -4177185
85 meter
Z = -15426867
43 Z = -4702109
19
XDOT = 13470
483680 XDOT = 4105
803426
YDOT = -17987
608328 feet/sec YDOT = -5482
623018 meter/sec
ZDOT = 9018
206619 ZDOT = 2748
749377
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 10210
39293210
00016717 00000-0 10270-3 0 9022
2 25544 51
6444 14
6014 0007186 164
0441 196
0948 15
71307656 30117
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210
39293210 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 14
6014 deg
Eccentricity:
0007186
Arg of perigee: 164
0441 deg
Mean anomaly: 196
0948 deg
Mean motion: 15
71307656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 273
Coasting Arc #4 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2010/211/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6149261
14 A = 6738741
61 meter
Y = -2239238
65 meter E =
0014770
Z = -1576435
39 I = 51
71527
XDOT = 2977
419840 Wp = 154
19670
YDOT = -4137
640630 meter/sec RA = 9
04818 deg
ZDOT = -5770
027550 TA = 43
16194
MA = 43
04625
Ha = 195
880 n
mi
Hp = 186
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20174741
26 X = -6116106
60
Y = -7346583
49 feet Y = -2307817
92 meter
Z = -5172032
11 Z = -1606227
64
XDOT = 9768
437795 XDOT = 3051
495761
YDOT = -13574
936450 feet/sec YDOT = -4103
930913 meter/sec
ZDOT = -18930
536581 ZDOT = -5755
383696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9219001
35 X = -2809951
61
Y = 19358621
18 feet Y = 5900507
74 meter
Z = -5291142
64 Z = -1612740
28
XDOT = -11168
560027 XDOT = -3404
177096
YDOT = -10447
750805 feet/sec YDOT = -3184
474445 meter/sec
ZDOT = -18871
939189 ZDOT = -5752
167065
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 10211
41050696
00016717 00000-0 10270-3 0 9036
2 25544 51
6443 9
3977 0007166 168
2313 191
9018 15
71300350 30270
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211
41050696 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 9
3977 deg
Eccentricity:
0007166
Arg of perigee: 168
2313 deg
Mean anomaly: 191
9018 deg
Mean motion: 15
71300350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 280
Coasting Arc #5 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2010/212/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1184044
76 A = 6728017
60 meter
Y = 4063459
05 meter E =
0006664
Z = 5225971
16 I = 51
64887
XDOT = -7568
456691 Wp = 143
90256
YDOT = -1163
824886 meter/sec RA = 3
91381 deg
ZDOT = -814
609073 TA = 313
82223
MA = 313
87731
Ha = 195
858 n
mi
Hp = 187
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3884661
28 X = -1254781
66
Y = 13331558
55 feet Y = 4049822
62 meter
Z = 17145574
66 Z = 5220047
47
XDOT = -24830
894657 XDOT = -7550
922900
YDOT = -3818
323116 feet/sec YDOT = -1248
361824 meter/sec
ZDOT = -2672
601945 ZDOT = -851
333721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12983383
03 X = 3957335
15
Y = 5006579
44 feet Y = 1526005
41 meter
Z = 17121848
74 Z = 5218739
50
XDOT = -5363
530457 XDOT = -1634
804083
YDOT = 23497
652406 feet/sec YDOT = 7162
084453 meter/sec
ZDOT = -2819
436920 ZDOT = -859
364373
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 10212
42807305
00016717 00000-0 10270-3 0 9046
2 25544 51
6442 4
1925 0007175 171
9126 188
2153 15
71307487 30433
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212
42807305 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 4
1925 deg
Eccentricity:
0007175
Arg of perigee: 171
9126 deg
Mean anomaly: 188
2153 deg
Mean motion: 15
71307487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 283
Coasting Arc #6 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2010/213/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6731837
90 A = 6739769
80 meter
Y = -265371
59 meter E =
0009054
Z = -157855
97 I = 51
65758
XDOT = 322
280996 Wp = 80
29205
YDOT = 4763
703897 meter/sec RA = 358
80446 deg
ZDOT = 6029
911767 TA = 277
99649
MA = 278
09922
Ha = 195
703 n
mi
Hp = 187
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22086082
34 X = 6735071
83
Y = -870641
69 feet Y = -190074
06 meter
Z = -517900
17 Z = -125145
08
XDOT = 1057
352350 XDOT = 239
696414
YDOT = 15628
949793 feet/sec YDOT = 4766
845799 meter/sec
ZDOT = 19783
175087 ZDOT = 6031
277023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 462435
97 X = 140950
48
Y = -22101076
27 feet Y = -6736408
05 meter
Z = -387106
09 Z = -117989
94
XDOT = 14046
203067 XDOT = 4281
282695
YDOT = -30
073606 feet/sec YDOT = -9
166435 meter/sec
ZDOT = 19788
586276 ZDOT = 6031
561097
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 10213
38203262
00016717 00000-0 10270-3 0 9055
2 25544 51
6433 359
3122 0007151 175
6075 184
5151 15
71330643 30588
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213
38203262 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 359
3122 deg
Eccentricity:
0007151
Arg of perigee: 175
6075 deg
Mean anomaly: 184
5151 deg
Mean motion: 15
71330643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 277
Coasting Arc #7 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2010/214/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1712233
94 A = 6728046
28 meter
Y = -3946824
50 meter E =
0015346
Z = -5184402
89 I = 51
58777
XDOT = 7403
464701 Wp = 108
94118
YDOT = -1725
985859 meter/sec RA = 353
69868 deg
ZDOT = -1138
770211 TA = 150
20420
MA = 150
11673
Ha = 195
593 n
mi
Hp = 187
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5617565
44 X = -1642787
79
Y = -12948899
29 feet Y = -3965583
13 meter
Z = -17009195
85 Z = -5192552
44
XDOT = 24289
582354 XDOT = 7427
746662
YDOT = -5662
683266 feet/sec YDOT = -1643
060056 meter/sec
ZDOT = -3736
122739 ZDOT = -1102
745455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13175192
30 X = -4015798
61
Y = 4953504
95 feet Y = 1509828
31 meter
Z = -17041739
17 Z = -5194322
10
XDOT = -4248
484509 XDOT = -1294
938078
YDOT = -23572
005877 feet/sec YDOT = -7184
747391 meter/sec
ZDOT = -3592
068103 ZDOT = -1094
862358
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 10214
39958184
00016717 00000-0 10270-3 0 9068
2 25544 51
6429 354
1072 0007200 178
3150 181
8037 15
71354547 30749
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214
39958184 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 354
1072 deg
Eccentricity:
0007200
Arg of perigee: 178
3150 deg
Mean anomaly: 181
8037 deg
Mean motion: 15
71354547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 301
Coasting Arc #8 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2010/215/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5903272
77 A = 6738203
55 meter
Y = 2665364
26 meter E =
0017808
Z = 1817445
51 I = 51
59266
XDOT = -3499
597939 Wp = 135
68222
YDOT = -3873
878546 meter/sec RA = 348
55385 deg
ZDOT = -5665
141610 TA = 24
15040
MA = 24
06701
Ha = 195
343 n
mi
Hp = 187
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19367692
82 X = -5941467
41
Y = 8744633
38 feet Y = 2599136
64 meter
Z = 5962747
75 Z = 1788674
94
XDOT = -11481
620536 XDOT = -3428
499288
YDOT = -12709
575282 feet/sec YDOT = -3912
615189 meter/sec
ZDOT = -18586
422606 ZDOT = -5681
970187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8239180
98 X = 2511302
36
Y = 19622714
67 feet Y = 5981003
43 meter
Z = 5847688
85 Z = 1782375
56
XDOT = -11569
624076 XDOT = -3526
421418
YDOT = 10437
436060 feet/sec YDOT = 3181
330511 meter/sec
ZDOT = -18653
665050 ZDOT = -5685
637107
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 10215
41712003
00016717 00000-0 10270-3 0 9071
2 25544 51
6433 348
9021 0006997 184
0724 176
0382 15
71403577 30907
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215
41712003 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 348
9021 deg
Eccentricity:
0006997
Arg of perigee: 184
0724 deg
Mean anomaly: 176
0382 deg
Mean motion: 15
71403577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 292
Coasting Arc #9 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2010/216/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222549
98 A = 6730429
50 meter
Y = 2543591
15 meter E =
0012606
Z = 4581813
69 I = 51
53649
XDOT = -5748
476504 Wp = 147
51871
YDOT = 4167
082658 meter/sec RA = 343
47134 deg
ZDOT = 2970
148885 TA = 272
87933
MA = 273
02360
Ha = 195
237 n
mi
Hp = 187
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13853510
44 X = 4171535
73
Y = 8345115
33 feet Y = 2590524
58 meter
Z = 15032197
15 Z = 4602203
07
XDOT = -18859
831051 XDOT = -5809
074723
YDOT = 13671
531031 feet/sec YDOT = 4102
460665 meter/sec
ZDOT = 9744
582956 ZDOT = 2942
076097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8465173
65 X = 2580184
93
Y = -13691050
62 feet Y = -4173032
23 meter
Z = 15113689
84 Z = 4606652
66
XDOT = 12508
194554 XDOT = 3812
497700
YDOT = 18418
269414 feet/sec YDOT = 5613
888517 meter/sec
ZDOT = 9632
296976 ZDOT = 2935
924118
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 10216
43465247
00016717 00000-0 10270-3 0 9080
2 25544 51
6426 343
6967 0007157 186
8343 173
2723 15
71385075 31064
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216
43465247 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 343
6967 deg
Eccentricity:
0007157
Arg of perigee: 186
8343 deg
Mean anomaly: 173
2723 deg
Mean motion: 15
71385075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3106
Checksum: 318
Coasting Arc #10 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2010/217/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3920692
73 A = 6734961
48 meter
Y = -4380230
15 meter E =
0007570
Z = -3296820
05 I = 51
52370
XDOT = 5844
185912 Wp = 151
74716
YDOT = 1693
201433 meter/sec RA = 338
30035 deg
ZDOT = 4698
330260 TA = 169
58441
MA = 169
56872
Ha = 195
249 n
mi
Hp = 187
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12863165
12 X = 3985397
10
Y = -14370833
81 feet Y = -4336024
49 meter
Z = -10816338
73 Z = -3277616
75
XDOT = 19173
838294 XDOT = 5801
994402
YDOT = 5555
122812 feet/sec YDOT = 1758
318214 meter/sec
ZDOT = 15414
469356 ZDOT = 4726
618804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14480444
91 X = -4413639
61
Y = -12804479
00 feet Y = -3902805
20 meter
Z = -10739511
06 Z = -3273402
97
XDOT = 4459
661443 XDOT = 1359
304808
YDOT = -18072
786406 feet/sec YDOT = -5508
585296 meter/sec
ZDOT = 15527
555388 ZDOT = 4732
798882
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 10217
38858027
00016717 00000-0 10270-3 0 9098
2 25544 51
6434 338
8166 0007234 188
8703 171
2332 15
71394693 31215
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217
38858027 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 338
8166 deg
Eccentricity:
0007234
Arg of perigee: 188
8703 deg
Mean anomaly: 171
2332 deg
Mean motion: 15
71394693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 317
Coasting Arc #11 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2010/218/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5716327
37 A = 6733965
97 meter
Y = -276100
67 meter E =
0007238
Z = -3546276
52 I = 51
49356
XDOT = 3023
711564 Wp = 147
81110
YDOT = -5496
799273 meter/sec RA = 333
22671 deg
ZDOT = -4456
218989 TA = 74
49577
MA = 74
41585
Ha = 194
952 n
mi
Hp = 187
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18754354
89 X = -5695588
15
Y = -905842
10 feet Y = -339907
70 meter
Z = -11634765
47 Z = -3573995
77
XDOT = 9920
313530 XDOT = 3106
600299
YDOT = -18034
118350 feet/sec YDOT = -5462
522366 meter/sec
ZDOT = -14620
141039 ZDOT = -4441
329253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -425874
49 X = -129806
54
Y = 18702240
17 feet Y = 5700442
80 meter
Z = -11745594
42 Z = -3580057
18
XDOT = -16921
941489 XDOT = -5157
807766
YDOT = -9509
022259 feet/sec YDOT = -2898
349985 meter/sec
ZDOT = -14560
547886 ZDOT = -4438
054996
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 10218
40609386
00016717 00000-0 10270-3 0 9106
2 25544 51
6437 333
6119 0007067 192
6133 167
4853 15
71420869 31370
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218
40609386 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 333
6119 deg
Eccentricity:
0007067
Arg of perigee: 192
6133 deg
Mean anomaly: 167
4853 deg
Mean motion: 15
71420869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 310
Coasting Arc #12 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2010/219/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1259750
03 A = 6731199
22 meter
Y = 4922980
85 meter E =
0007642
Z = 4406516
97 I = 51
45678
XDOT = -6860
617672 Wp = 117
91068
YDOT = 1189
880333 meter/sec RA = 328
04947 deg
ZDOT = -3289
862997 TA = 5
19906
MA = 5
19113
Ha = 195
006 n
mi
Hp = 188
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4133038
16 X = -1336111
77
Y = 16151511
99 feet Y = 4908466
14 meter
Z = 14457076
68 Z = 4400212
26
XDOT = -22508
588164 XDOT = -6857
431949
YDOT = 3903
806867 feet/sec YDOT = 1113
178973 meter/sec
ZDOT = -10793
513770 ZDOT = -3323
183448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16318031
61 X = 4973736
03
Y = 3522052
51 feet Y = 1073521
60 meter
Z = 14431819
04 Z = 4398818
44
XDOT = 5119
181452 XDOT = 1560
326507
YDOT = 21066
298842 feet/sec YDOT = 6421
007887 meter/sec
ZDOT = -10926
758020 ZDOT = -3330
475844
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 10219
42359981
00016717 00000-0 10270-3 0 9113
2 25544 51
6433 328
4063 0007182 196
3063 163
7869 15
71393771 31532
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219
42359981 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 328
4063 deg
Eccentricity:
0007182
Arg of perigee: 196
3063 deg
Mean anomaly: 163
7869 deg
Mean motion: 15
71393771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 319
Coasting Arc #13 (Orbit 3168)
---------------------------------------
Vector Time (GMT): 2010/220/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5940203
61 A = 6737365
17 meter
Y = -2344850
96 meter E =
0010970
Z = 2141388
60 I = 51
45464
XDOT = 134
638995 Wp = 101
16436
YDOT = 5383
033809 meter/sec RA = 322
96383 deg
ZDOT = 5495
129930 TA = 282
81965
MA = 282
94220
Ha = 194
774 n
mi
Hp = 188
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19488856
98 X = 5955580
42
Y = -7693080
56 feet Y = -2278338
26 meter
Z = 7025553
16 Z = 2170282
62
XDOT = 441
728986 XDOT = 47
741160
YDOT = 17660
872078 feet/sec YDOT = 5384
053058 meter/sec
ZDOT = 18028
641502 ZDOT = 5495
573404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8846993
87 X = -2696563
73
Y = -18949740
66 feet Y = -5775880
95 meter
Z = 7141110
58 Z = 2176610
50
XDOT = 16227
616144 XDOT = 4946
177401
YDOT = -749
995457 feet/sec YDOT = -228
598615 meter/sec
ZDOT = 18030
369416 ZDOT = 5495
656598
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 10220
44109451
00016717 00000-0 10270-3 0 9123
2 25544 51
6446 323
2014 0007239 200
4868 159
6005 15
71459969 31693
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220
44109451 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 323
2014 deg
Eccentricity:
0007239
Arg of perigee: 200
4868 deg
Mean anomaly: 159
6005 deg
Mean motion: 15
71459969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3169
Checksum: 300
Coasting Arc #14 (Orbit 3183)
---------------------------------------
Vector Time (GMT): 2010/221/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1418836
85 A = 6728221
07 meter
Y = -4189111
30 meter E =
0014095
Z = -5081508
90 I = 51
40065
XDOT = 6338
354010 Wp = 131
38497
YDOT = -4056
965989 meter/sec RA = 317
80152 deg
ZDOT = 1568
373613 TA = 153
78354
MA = 153
71212
Ha = 194
625 n
mi
Hp = 188
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4654976
56 X = -1347203
56
Y = -13743803
48 feet Y = -4204576
75 meter
Z = -16671617
12 Z = -5088227
70
XDOT = 20795
124706 XDOT = 6375
629982
YDOT = -13310
255870 feet/sec YDOT = -3985
878397 meter/sec
ZDOT = 5145
582721 ZDOT = 1599
254866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13351452
19 X = -4069522
63
Y = 5603931
44 feet Y = 1708078
30 meter
Z = -16698456
07 Z = -5089689
41
XDOT = -14465
196792 XDOT = -4408
991982
YDOT = -18700
811340 feet/sec YDOT = -5700
007296 meter/sec
ZDOT = 5269
096759 ZDOT = 1606
020692
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 10221
39499044
00016717 00000-0 10270-3 0 9139
2 25544 51
6450 318
3229 0007091 203
7352 156
3483 15
71456210 31848
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221
39499044 = yrday
fracday
Element set: 913
Inclination: 51
6450 deg
RA of node: 318
3229 deg
Eccentricity:
0007091
Arg of perigee: 203
7352 deg
Mean anomaly: 156
3483 deg
Mean motion: 15
71456210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3184
Checksum: 291
Coasting Arc #15 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2010/222/09:09:47
811
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4871358
78 A = 6739227
99 meter
Y = 4607941
10 meter E =
0014927
Z = -572290
44 I = 51
41592
XDOT = -2944
572606 Wp = 165
12510
YDOT = -3850
145630 meter/sec RA = 312
68732 deg
ZDOT = -5984
746134 TA = 21
12026
MA = 21
05869
Ha = 194
364 n
mi
Hp = 188
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15982148
23 X = -4919743
56
Y = 15117917
00 feet Y = 4553196
14 meter
Z = -1877593
31 Z = -596072
31
XDOT = -9660
671278 XDOT = -2872
228633
YDOT = -12631
711386 feet/sec YDOT = -3882
668940 meter/sec
ZDOT = -19634
993879 ZDOT = -5998
874902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16557438
05 X = 5046707
12
Y = 14472922
23 feet Y = 4411346
70 meter
Z = -1972714
03 Z = -601283
24
XDOT = -10619
974550 XDOT = -3236
968243
YDOT = 9486
237269 feet/sec YDOT = 2891
405120 meter/sec
ZDOT = -19691
473356 ZDOT = -6001
961079
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 10222
41246952
00016717 00000-0 10270-3 0 9142
2 25544 51
6446 313
1171 0007006 208
4305 151
6476 15
71471886 32003
Satellite: ISS
Catalog Number: 25544
Epoch time: 10222
41246952 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 313
1171 deg
Eccentricity:
0007006
Arg of perigee: 208
4305 deg
Mean anomaly: 151
6476 deg
Mean motion: 15
71471886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 279
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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