Date:
August 25th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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 3405)
---------------------------------------
Vector Time (GMT): 2010/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4709953
66 A = 6731006
27 meter
Y = -1442551
31 meter E =
0002447
Z = -4589528
20 I = 51
32338
XDOT = -683
660493 Wp = 127
46622
YDOT = -7081
967131 meter/sec RA = 245
25799 deg
ZDOT = 2927
159447 TA = 171
70276
MA = 171
69871
Ha = 192
922 n
mi
Hp = 191
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15452603
86 X = -4671178
08
Y = -4732779
88 feet Y = -1495004
07 meter
Z = -15057507
21 Z = -4612314
49
XDOT = -2242
980619 XDOT = -618
637150
YDOT = -23234
800299 feet/sec YDOT = -7089
248636 meter/sec
ZDOT = 9603
541494 ZDOT = 2923
996306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11120852
76 X = 3389635
92
Y = 11608395
17 feet Y = 3538238
85 meter
Z = -15148679
49 Z = -4617317
51
XDOT = -8445
621985 XDOT = -2574
225581
YDOT = 20608
387263 feet/sec YDOT = 6281
436438 meter/sec
ZDOT = 9590
809124 ZDOT = 2923
278621
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
51078085
00016717 00000-0 10270-3 0 9002
2 25544 51
6435 246
1134 0008277 284
7380 75
2864 15
71168758 34067
Satellite: ISS
Catalog Number: 25544
Epoch time: 10235
51078085 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 246
1134 deg
Eccentricity:
0008277
Arg of perigee: 284
7380 deg
Mean anomaly: 75
2864 deg
Mean motion: 15
71168758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3406
Checksum: 313
Coasting Arc #2 (Orbit 3421)
---------------------------------------
Vector Time (GMT): 2010/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1955473
61 A = 6738880
55 meter
Y = 6206298
80 meter E =
0004615
Z = -1741235
97 I = 51
36243
XDOT = -5199
770360 Wp = 222
30673
YDOT = 45
787565 meter/sec RA = 240
16030 deg
ZDOT = -5670
975879 TA = 337
01876
MA = 337
03940
Ha = 193
218 n
mi
Hp = 191
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6415595
84 X = 1894386
76
Y = 20361872
69 feet Y = 6227824
47 meter
Z = -5712716
44 Z = -1731885
01
XDOT = -17059
614041 XDOT = -5172
347823
YDOT = 150
221669 feet/sec YDOT = -12
206218 meter/sec
ZDOT = -18605
563906 ZDOT = -5696
169302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3908612
23 X = 1191345
01
Y = -20997985
88 feet Y = -6400186
10 meter
Z = -5675226
70 Z = -1729809
10
XDOT = 13487
812488 XDOT = 4111
085246
YDOT = 7571
293425 feet/sec YDOT = 2307
730236 meter/sec
ZDOT = -18706
354060 ZDOT = -5701
696717
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
52842858
00016717 00000-0 10270-3 0 9012
2 25544 51
6422 240
9087 0008180 288
5154 71
5118 15
71192376 34228
Satellite: ISS
Catalog Number: 25544
Epoch time: 10236
52842858 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 240
9087 deg
Eccentricity:
0008180
Arg of perigee: 288
5154 deg
Mean anomaly: 71
5118 deg
Mean motion: 15
71192376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3422
Checksum: 304
Coasting Arc #3 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2010/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4039308
71 A = 6728354
46 meter
Y = -1460503
14 meter E =
0006893
Z = 5183679
29 I = 51
34298
XDOT = 3697
602556 Wp = 318
05233
YDOT = 6671
672607 meter/sec RA = 235
00059 deg
ZDOT = -997
271943 TA = 141
52826
MA = 141
47910
Ha = 193
363 n
mi
Hp = 190
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13252325
15 X = 4030159
09
Y = -4791676
96 feet Y = -1415384
10 meter
Z = 17006821
83 Z = 5203279
81
XDOT = 12131
241981 XDOT = 3627
568372
YDOT = 21888
689657 feet/sec YDOT = 6712
629790 meter/sec
ZDOT = -3271
889576 ZDOT = -979
479650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13889006
98 X = -4233369
33
Y = -1734081
55 feet Y = -528548
06 meter
Z = 17085219
49 Z = 5207574
90
XDOT = -956
873828 XDOT = -291
655143
YDOT = -24008
259251 feet/sec YDOT = -7317
717420 meter/sec
ZDOT = -3200
609534 ZDOT = -975
545786
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
54606501
00016717 00000-0 10270-3 0 9029
2 25544 51
6417 235
7038 0008280 292
9446 67
0841 15
71219063 34387
Satellite: ISS
Catalog Number: 25544
Epoch time: 10237
54606501 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 235
7038 deg
Eccentricity:
0008280
Arg of perigee: 292
9446 deg
Mean anomaly: 67
0841 deg
Mean motion: 15
71219063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 300
Coasting Arc #4 (Orbit 3452)
---------------------------------------
Vector Time (GMT): 2010/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4350216
07 A = 6739915
44 meter
Y = -5137265
62 meter E =
0012209
Z = -19662
74 I = 51
40101
XDOT = 3655
101227 Wp = 6
03128
YDOT = -3116
818392 meter/sec RA = 229
87580 deg
ZDOT = 6017
450049 TA = 353
75458
MA = 353
76978
Ha = 193
405 n
mi
Hp = 190
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14272362
45 X = -4292351
39
Y = -16854546
01 feet Y = -5185588
81 meter
Z = -64510
30 Z = -40655
04
XDOT = 11991
801925 XDOT = 3660
451017
YDOT = -10225
782125 feet/sec YDOT = -3075
914626 meter/sec
ZDOT = 19742
290188 ZDOT = 6035
219509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5383381
14 X = 1640854
57
Y = 21419088
30 feet Y = 6528538
11 meter
Z = -148580
76 Z = -45287
42
XDOT = -13603
574963 XDOT = -4146
369649
YDOT = 3553
050405 feet/sec YDOT = 1082
969764 meter/sec
ZDOT = 19813
337061 ZDOT = 6039
105136
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
50008969
00016717 00000-0 10270-3 0 9031
2 25544 51
6419 230
8253 0008170 295
7210 64
3108 15
71284546 34533
Satellite: ISS
Catalog Number: 25544
Epoch time: 10238
50008969 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 230
8253 deg
Eccentricity:
0008170
Arg of perigee: 295
7210 deg
Mean anomaly: 64
3108 deg
Mean motion: 15
71284546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3453
Checksum: 298
Coasting Arc #5 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2010/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2090128
81 A = 6728352
81 meter
Y = 3757357
02 meter E =
0009585
Z = -5182518
85 I = 51
38172
XDOT = -5961
199790 Wp = 48
74684
YDOT = -4747
834780 meter/sec RA = 224
75215 deg
ZDOT = -1033
051287 TA = 211
32496
MA = 211
38210
Ha = 193
772 n
mi
Hp = 190
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6857377
99 X = -2106813
33
Y = 12327286
80 feet Y = 3733890
36 meter
Z = -17003014
60 Z = -5192713
38
XDOT = -19557
742092 XDOT = -5902
647231
YDOT = -15576
885760 feet/sec YDOT = -4814
169163 meter/sec
ZDOT = -3389
275877 ZDOT = -1061
868131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11356528
18 X = 3461469
79
Y = -8284216
81 feet Y = -2525029
28 meter
Z = -17043742
48 Z = -5194932
71
XDOT = 10456
029885 XDOT = 3186
997909
YDOT = 21577
735830 feet/sec YDOT = 6576
893881 meter/sec
ZDOT = -3504
655333 ZDOT = -1068
218945
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
51770579
00016717 00000-0 10270-3 0 9047
2 25544 51
6415 225
6200 0008307 301
1736 58
8610 15
71241861 34696
Satellite: ISS
Catalog Number: 25544
Epoch time: 10239
51770579 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 225
6200 deg
Eccentricity:
0008307
Arg of perigee: 301
1736 deg
Mean anomaly: 58
8610 deg
Mean motion: 15
71241861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 297
Coasting Arc #6 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2010/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5785993
03 A = 6738513
84 meter
Y = 2970876
54 meter E =
0005991
Z = 1754418
33 I = 51
43906
XDOT = -904
167494 Wp = 98
78379
YDOT = 5119
197496 meter/sec RA = 219
59590 deg
ZDOT = -5671
197138 TA = 61
76191
MA = 61
70144
Ha = 193
985 n
mi
Hp = 190
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18982916
76 X = 5743819
48
Y = 9746970
29 feet Y = 3035343
27 meter
Z = 5755965
65 Z = 1782424
03
XDOT = -2966
428787 XDOT = -933
794501
YDOT = 16795
267374 feet/sec YDOT = 5108
920600 meter/sec
ZDOT = -18606
289824 ZDOT = -5675
661809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13294363
76 X = -4052122
07
Y = -16652665
24 feet Y = -5075732
36 meter
Z = 5868077
36 Z = 1788589
98
XDOT = 8269
633542 XDOT = 2520
584304
YDOT = -13182
353396 feet/sec YDOT = -4017
981315 meter/sec
ZDOT = -18624
066913 ZDOT = -5676
615595
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
53530990
00016717 00000-0 10270-3 0 9053
2 25544 51
6417 220
4153 0008501 305
8092 54
2279 15
71289758 34856
Satellite: ISS
Catalog Number: 25544
Epoch time: 10240
53530990 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 220
4153 deg
Eccentricity:
0008501
Arg of perigee: 305
8092 deg
Mean anomaly: 54
2279 deg
Mean motion: 15
71289758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 303
Coasting Arc #7 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2010/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -613316
39 A = 6730683
65 meter
Y = -4872684
36 meter E =
0001954
Z = 4600889
41 I = 51
43691
XDOT = 6864
709480 Wp = 27
14259
YDOT = 1892
988006 meter/sec RA = 214
50576 deg
ZDOT = 2921
132128 TA = 33
82657
MA = 33
81410
Ha = 194
077 n
mi
Hp = 189
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2012192
88 X = -581133
87
Y = -15986497
25 feet Y = -4879362
70 meter
Z = 15094781
54 Z = 4597988
29
XDOT = 22522
012731 XDOT = 6828
841190
YDOT = 6210
590570 feet/sec YDOT = 1969
552873 meter/sec
ZDOT = 9583
766823 ZDOT = 2954
393716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4363568
11 X = -1330015
56
Y = 15521893
65 feet Y = 4731073
19 meter
Z = 15083087
71 Z = 4597325
13
XDOT = -17071
769431 XDOT = -5203
475323
YDOT = -14237
568791 feet/sec YDOT = -4339
610968 meter/sec
ZDOT = 9716
899268 ZDOT = 2961
710897
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
55290298
00016717 00000-0 10270-3 0 9061
2 25544 51
6419 215
2112 0008546 308
6408 51
3988 15
71307026 35019
Satellite: ISS
Catalog Number: 25544
Epoch time: 10241
55290298 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 215
2112 deg
Eccentricity:
0008546
Arg of perigee: 308
6408 deg
Mean anomaly: 51
3988 deg
Mean motion: 15
71307026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 294
Coasting Arc #8 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2010/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5867010
15 A = 6735127
28 meter
Y = -295447
75 meter E =
0006264
Z = -3286597
75 I = 51
47754
XDOT = -2351
142753 Wp = 347
26986
YDOT = -5618
724467 meter/sec RA = 209
33073 deg
ZDOT = 4706
501640 TA = 334
11582
MA = 334
14714
Ha = 194
231 n
mi
Hp = 189
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19248720
96 X = -5847304
61
Y = -969316
76 feet Y = -360946
08 meter
Z = -10782801
03 Z = -3315051
89
XDOT = -7713
722944 XDOT = -2311
001797
YDOT = -18434
135390 feet/sec YDOT = -5644
791792 meter/sec
ZDOT = 15441
278345 ZDOT = 4695
177408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17395128
87 X = 5302035
28
Y = 8148224
12 feet Y = 2483578
71 meter
Z = -10896676
87 Z = -3321307
11
XDOT = 853
679423 XDOT = 260
201488
YDOT = 18747
821644 feet/sec YDOT = 5714
336037 meter/sec
ZDOT = 15395
861806 ZDOT = 4692
658679
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
50688694
00016717 00000-0 10270-3 0 9079
2 25544 51
6419 210
3318 0008501 313
5011 46
5443 15
71284824 35167
Satellite: ISS
Catalog Number: 25544
Epoch time: 10242
50688694 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 210
3318 deg
Eccentricity:
0008501
Arg of perigee: 313
5011 deg
Mean anomaly: 46
5443 deg
Mean motion: 15
71284824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 290
Coasting Arc #9 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2010/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3415370
36 A = 6734460
15 meter
Y = 4614910
43 meter E =
0006788
Z = -3526005
68 I = 51
50306
XDOT = -6152
177474 Wp = 354
88627
YDOT = 1129
912315 meter/sec RA = 204
25616 deg
ZDOT = -4472
980653 TA = 227
07882
MA = 227
13580
Ha = 194
469 n
mi
Hp = 189
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11205283
34 X = 3380640
49
Y = 15140782
25 feet Y = 4652908
93 meter
Z = -11568260
12 Z = -3509498
18
XDOT = -20184
309299 XDOT = -6142
626130
YDOT = 3707
061401 feet/sec YDOT = 1061
168342 meter/sec
ZDOT = -14675
133377 ZDOT = -4502
844813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5029131
52 X = -1532879
29
Y = -18194382
46 feet Y = -5545647
77 meter
Z = -11502112
29 Z = -3505843
82
XDOT = 18749
173122 XDOT = 5714
747968
YDOT = 4185
625339 feet/sec YDOT = 1275
778603 meter/sec
ZDOT = -14794
638279 ZDOT = -4509
405747
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10243
52445748
00016717 00000-0 10270-3 0 9084
2 25544 51
6425 205
1271 0008562 317
4899 42
5599 15
71331800 35321
Satellite: ISS
Catalog Number: 25544
Epoch time: 10243
52445748 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 205
1271 deg
Eccentricity:
0008562
Arg of perigee: 317
4899 deg
Mean anomaly: 42
5599 deg
Mean motion: 15
71331800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 309
Coasting Arc #10 (Orbit 3547)
---------------------------------------
Vector Time (GMT): 2010/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4591885
04 A = 6731118
10 meter
Y = -2141137
22 meter E =
0010491
Z = 4434450
10 I = 51
52027
XDOT = 5275
928626 Wp = 16
62035
YDOT = 4558
942359 meter/sec RA = 199
08344 deg
ZDOT = -3250
214465 TA = 106
10009
MA = 105
98457
Ha = 194
557 n
mi
Hp = 189
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15065239
64 X = 4593944
58
Y = -7024728
42 feet Y = -2089776
52 meter
Z = 14548720
79 Z = 4456762
48
XDOT = 17309
477121 XDOT = 5240
346537
YDOT = 14957
159969 feet/sec YDOT = 4617
742019 meter/sec
ZDOT = -10663
433283 ZDOT = -3224
670399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16483754
93 X = -5024248
50
Y = 1410138
59 feet Y = 429810
24 meter
Z = 14637993
85 Z = 4461660
52
XDOT = -11024
363866 XDOT = -3360
226106
YDOT = -18840
241249 feet/sec YDOT = -5742
505533 meter/sec
ZDOT = -10561
108432 ZDOT = -3219
025850
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10244
54201585
00016717 00000-0 10270-3 0 9097
2 25544 51
6424 199
9228 0008646 320
8749 39
1786 15
71346280 35482
Satellite: ISS
Catalog Number: 25544
Epoch time: 10244
54201585 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 199
9228 deg
Eccentricity:
0008646
Arg of perigee: 320
8749 deg
Mean anomaly: 39
1786 deg
Mean motion: 15
71346280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3548
Checksum: 333
Coasting Arc #11 (Orbit 3563)
---------------------------------------
Vector Time (GMT): 2010/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5595654
10 A = 6737842
65 meter
Y = -3100279
65 meter E =
0014488
Z = 2084828
67 I = 51
57205
XDOT = 4021
833115 Wp = 34
54296
YDOT = -3527
955459 meter/sec RA = 194
00376 deg
ZDOT = 5541
232453 TA = 348
75661
MA = 348
78894
Ha = 194
742 n
mi
Hp = 188
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18358445
21 X = -5570698
01
Y = -10171521
17 feet Y = -3162714
10 meter
Z = 6839989
06 Z = 2057705
64
XDOT = 13194
990535 XDOT = 4034
066222
YDOT = -11574
657019 feet/sec YDOT = -3482
912586 meter/sec
ZDOT = 18179
896499 ZDOT = 5560
800128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14016873
65 X = 4272343
09
Y = 15668245
27 feet Y = 4775681
16 meter
Z = 6731355
50 Z = 2051717
16
XDOT = -15028
478830 XDOT = -4580
680347
YDOT = 5590
461152 feet/sec YDOT = 1703
972559 meter/sec
ZDOT = 18258
168608 ZDOT = 5565
089792
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10245
55956153
00016717 00000-0 10270-3 0 9109
2 25544 51
6426 194
7179 0008598 324
5036 35
5553 15
71372842 35641
Satellite: ISS
Catalog Number: 25544
Epoch time: 10245
55956153 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 194
7179 deg
Eccentricity:
0008598
Arg of perigee: 324
5036 deg
Mean anomaly: 35
5553 deg
Mean motion: 15
71372842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3564
Checksum: 324
Coasting Arc #12 (Orbit 3578)
---------------------------------------
Vector Time (GMT): 2010/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2232654
14 A = 6728250
14 meter
Y = 3762456
88 meter E =
0010342
Z = -5118488
25 I = 51
56994
XDOT = -7194
640539 Wp = 62
74762
YDOT = -2292
820387 meter/sec RA = 188
85300 deg
ZDOT = 1459
773940 TA = 221
23517
MA = 221
31333
Ha = 194
862 n
mi
Hp = 188
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7324980
79 X = -2249696
18
Y = 12344018
63 feet Y = 3737394
78 meter
Z = -16792940
47 Z = -5129375
76
XDOT = -23604
463711 XDOT = -7175
558345
YDOT = -7522
376597 feet/sec YDOT = -2373
168493 meter/sec
ZDOT = 4789
284580 ZDOT = 1424
868946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10729594
55 X = 3270380
42
Y = -9457391
47 feet Y = -2882612
92 meter
Z = -16836464
49 Z = -5131754
38
XDOT = 19394
978469 XDOT = 5911
589437
YDOT = 13766
959009 feet/sec YDOT = 4196
169106 meter/sec
ZDOT = 4649
492720 ZDOT = 1417
165381
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10246
51350000
00016717 00000-0 10270-3 0 9116
2 25544 51
6428 189
8384 0008723 328
3269 31
7367 15
71375156 35794
Satellite: ISS
Catalog Number: 25544
Epoch time: 10246
51350000 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 189
8384 deg
Eccentricity:
0008723
Arg of perigee: 328
3269 deg
Mean anomaly: 31
7367 deg
Mean motion: 15
71375156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 314
Coasting Arc #13 (Orbit 3594)
---------------------------------------
Vector Time (GMT): 2010/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6676286
94 A = 6739517
69 meter
Y = 798364
85 meter E =
0003575
Z = -454644
00 I = 51
63889
XDOT = -968
705798 Wp = 102
35261
YDOT = 4702
207727 meter/sec RA = 183
75138 deg
ZDOT = -6008
337451 TA = 82
58303
MA = 82
54240
Ha = 195
012 n
mi
Hp = 188
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21903828
54 X = 6669071
83
Y = 2619307
25 feet Y = 872982
75 meter
Z = -1491614
16 Z = -422228
48
XDOT = -3178
168627 XDOT = -992
027662
YDOT = 15427
190705 feet/sec YDOT = 4691
244683 meter/sec
ZDOT = -19712
393211 ZDOT = -6013
100015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20145586
18 X = -6140374
67
Y = -9009120
42 feet Y = -2745979
90 meter
Z = -1361798
37 Z = -415076
14
XDOT = 6847
903626 XDOT = 2087
241025
YDOT = -12352
221585 feet/sec YDOT = -3764
957139 meter/sec
ZDOT = -19731
377343 ZDOT = -6014
123814
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10247
53102197
00016717 00000-0 10270-3 0 9122
2 25544 51
6436 184
6335 0008719 332
2481 27
8214 15
71395602 35950
Satellite: ISS
Catalog Number: 25544
Epoch time: 10247
53102197 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 184
6335 deg
Eccentricity:
0008719
Arg of perigee: 332
2481 deg
Mean anomaly: 27
8214 deg
Mean motion: 15
71395602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 306
Coasting Arc #14 (Orbit 3610)
---------------------------------------
Vector Time (GMT): 2010/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -584341
76 A = 6727444
40 meter
Y = -4152664
79 meter E =
0007099
Z = 5260975
45 I = 51
62942
XDOT = 7666
028065 Wp = 350
97114
YDOT = -530
698675 meter/sec RA = 178
63555 deg
ZDOT = 439
537116 TA = 94
89241
MA = 94
81135
Ha = 195
051 n
mi
Hp = 188
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1917131
77 X = -563418
98
Y = -13624228
31 feet Y = -4159082
14 meter
Z = 17260418
16 Z = 5258187
68
XDOT = 25151
010713 XDOT = 7669
257517
YDOT = -1741
137386 feet/sec YDOT = -444
954487 meter/sec
ZDOT = 1442
050904 ZDOT = 476
786006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1883575
50 X = -574113
81
Y = 13643136
33 feet Y = 4158427
95 meter
Z = 17249173
91 Z = 5257548
21
XDOT = -23625
970409 XDOT = -7201
195781
YDOT = -5244
701609 feet/sec YDOT = -1598
585050 meter/sec
ZDOT = 1591
214370 ZDOT = 485
002140
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10248
54852975
00016717 00000-0 10270-3 0 9131
2 25544 51
6440 179
4290 0008790 335
3246 24
7494 15
71451438 36114
Satellite: ISS
Catalog Number: 25544
Epoch time: 10248
54852975 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 179
4290 deg
Eccentricity:
0008790
Arg of perigee: 335
3246 deg
Mean anomaly: 24
7494 deg
Mean motion: 15
71451438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3611
Checksum: 319
Coasting Arc #15 (Orbit 3625)
---------------------------------------
Vector Time (GMT): 2010/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6396385
90 A = 6738834
31 meter
Y = 1697216
88 meter E =
0015691
Z = -1219096
38 I = 51
69800
XDOT = -2287
607859 Wp = 9
37191
YDOT = -4415
070908 meter/sec RA = 173
50558 deg
ZDOT = 5881
777411 TA = 337
28039
MA = 337
34976
Ha = 195
233 n
mi
Hp = 187
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20985518
04 X = -6408967
03
Y = 5568296
86 feet Y = 1625618
25 meter
Z = -3999660
03 Z = -1250200
20
XDOT = -7505
275128 XDOT = -2266
639895
YDOT = -14485
140773 feet/sec YDOT = -4440
534763 meter/sec
ZDOT = 19297
169985 ZDOT = 5870
715541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21687775
78 X = 6610434
06
Y = 162817
61 feet Y = 49626
81 meter
Z = -4124202
90 Z = -1257057
04
XDOT = 3537
480079 XDOT = 1078
223928
YDOT = 14400
677769 feet/sec YDOT = 4389
326584 meter/sec
ZDOT = 19252
776217 ZDOT = 5868
246191
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10249
50243410
00016717 00000-0 10270-3 0 9147
2 25544 51
6441 174
5490 0008851 339
6169 20
4639 15
71423538 36262
Satellite: ISS
Catalog Number: 25544
Epoch time: 10249
50243410 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 174
5490 deg
Eccentricity:
0008851
Arg of perigee: 339
6169 deg
Mean anomaly: 20
4639 deg
Mean motion: 15
71423538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3626
Checksum: 303
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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