Date:
November 19th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
329/05:05:17
749 -1
6 2
0 2
0
N/A 0
5 0
1 190
2
000/00:04:35
497 1
1 0
1 188
9
Coasting Arc #1 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2010/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6384591
58 A = 6735382
81 meter
Y = -2067564
85 meter E =
0015580
Z = 438388
95 I = 51
74783
XDOT = 1850
635742 Wp = 158
60967
YDOT = 4425
208739 meter/sec RA = 165
00825 deg
ZDOT = -6029
075914 TA = 16
62891
MA = 16
57787
Ha = 192
155 n
mi
Hp = 186
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20946822
77 X = 6405107
29
Y = -6783349
23 feet Y = -1996053
79 meter
Z = 1438283
94 Z = 469455
88
XDOT = 6071
639573 XDOT = 1830
303570
YDOT = 14518
401375 feet/sec YDOT = 4445
790009 meter/sec
ZDOT = -19780
432789 ZDOT = -6020
134671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6211038
69 X = -1893124
59
Y = 21114728
89 feet Y = 6435769
37 meter
Z = 1563039
95 Z = 476414
58
XDOT = -13938
766771 XDOT = -4248
536112
YDOT = -2626
812969 feet/sec YDOT = -800
652593 meter/sec
ZDOT = -19744
526381 ZDOT = -6018
131641
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 10321
53270299
00016717 00000-0 10270-3 0 9001
2 25544 51
6426 165
8857 0007385 215
0546 145
0132 15
72841513 7596
Satellite: ISS
Catalog Number: 25544
Epoch time: 10321
53270299 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 165
8857 deg
Eccentricity:
0007385
Arg of perigee: 215
0546 deg
Mean anomaly: 145
0132 deg
Mean motion: 15
72841513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 301
Coasting Arc #2 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2010/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2377180
36 A = 6723686
51 meter
Y = -3513410
16 meter E =
0007778
Z = 5219030
88 I = 51
73641
XDOT = 6896
456653 Wp = 192
41173
YDOT = -3293
669631 meter/sec RA = 159
90022 deg
ZDOT = 916
751440 TA = 248
82209
MA = 248
90521
Ha = 192
052 n
mi
Hp = 186
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7799148
16 X = -2363069
88
Y = -11526936
22 feet Y = -3539914
42 meter
Z = 17122804
73 Z = 5207516
43
XDOT = 22626
170120 XDOT = 6928
320977
YDOT = -10806
002726 feet/sec YDOT = -3216
371157 meter/sec
ZDOT = 3007
714698 ZDOT = 950
332693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13971755
09 X = 4258590
95
Y = -261489
70 feet Y = -79702
06 meter
Z = 17076565
68 Z = 5204937
22
XDOT = -3424
311178 XDOT = -1043
730047
YDOT = 23806
314404 feet/sec YDOT = 7256
164630 meter/sec
ZDOT = 3142
581869 ZDOT = 957
858954
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 10322
54926920
00016717 00000-0 10270-3 0 9013
2 25544 51
6414 160
6731 0007348 218
9377 141
1257 15
72849003 7755
Satellite: ISS
Catalog Number: 25544
Epoch time: 10322
54926920 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 160
6731 deg
Eccentricity:
0007348
Arg of perigee: 218
9377 deg
Mean anomaly: 141
1257 deg
Mean motion: 15
72849003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 302
Coasting Arc #3 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2010/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5564563
55 A = 6734655
47 meter
Y = 3615642
14 meter E =
0002065
Z = -1141078
78 I = 51
80107
XDOT = -3481
351430 Wp = 17
12623
YDOT = -3495
804401 meter/sec RA = 154
76210 deg
ZDOT = 5904
853722 TA = 330
42072
MA = 330
43240
Ha = 191
720 n
mi
Hp = 186
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18256442
10 X = -5599037
44
Y = 11862342
98 feet Y = 3553223
13 meter
Z = -3743696
78 Z = -1168195
83
XDOT = -11421
756660 XDOT = -3470
687508
YDOT = -11469
174544 feet/sec YDOT = -3534
675567 meter/sec
ZDOT = 19372
879664 ZDOT = 5887
966586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -256311
47 X = -78123
74
Y = -21751316
26 feet Y = -6629801
20 meter
Z = -3852618
61 Z = -1174278
15
XDOT = 14276
883559 XDOT = 4351
594109
YDOT = -3584
957430 feet/sec YDOT = -1092
695025 meter/sec
ZDOT = 19305
062704 ZDOT = 5884
183112
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 10323
50227372
00016717 00000-0 10270-3 0 9026
2 25544 51
6401 155
7859 0007439 223
3395 136
7183 15
72916972 7903
Satellite: ISS
Catalog Number: 25544
Epoch time: 10323
50227372 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 155
7859 deg
Eccentricity:
0007439
Arg of perigee: 223
3395 deg
Mean anomaly: 136
7183 deg
Mean motion: 15
72916972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 313
Coasting Arc #4 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2010/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3618300
41 A = 6723996
48 meter
Y = 2518853
80 meter E =
0008145
Z = -5083160
09 I = 51
79162
XDOT = -5721
841969 Wp = 105
07271
YDOT = 4866
592628 meter/sec RA = 149
67041 deg
ZDOT = -1665
669924 TA = 148
95874
MA = 148
91058
Ha = 191
549 n
mi
Hp = 187
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11871064
34 X = 3614559
00
Y = 8263956
05 feet Y = 2559295
21 meter
Z = -16677034
40 Z = -5065590
79
XDOT = -18772
447406 XDOT = -5767
744084
YDOT = 15966
511247 feet/sec YDOT = 4802
351002 meter/sec
ZDOT = -5464
796338 ZDOT = -1693
578657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13288175
16 X = -4050235
79
Y = 5915072
99 feet Y = 1802914
25 meter
Z = -16606472
44 Z = -5061652
80
XDOT = -3439
288012 XDOT = -1048
294986
YDOT = -23343
857534 feet/sec YDOT = -7115
207776 meter/sec
ZDOT = -5576
920257 ZDOT = -1699
845294
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 10324
51878774
00016717 00000-0 10270-3 0 9037
2 25544 51
6392 150
5734 0007351 226
4826 133
5727 15
72967304 8065
Satellite: ISS
Catalog Number: 25544
Epoch time: 10324
51878774 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 150
5734 deg
Eccentricity:
0007351
Arg of perigee: 226
4826 deg
Mean anomaly: 133
5727 deg
Mean motion: 15
72967304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 316
Coasting Arc #5 (Orbit 821)
---------------------------------------
Vector Time (GMT): 2010/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4360966
36 A = 6733496
84 meter
Y = -4807132
88 meter E =
0012446
Z = 1761847
41 I = 51
85075
XDOT = 4695
084366 Wp = 146
27613
YDOT = 2162
813025 meter/sec RA = 144
52509 deg
ZDOT = -5711
224724 TA = 14
26537
MA = 14
23026
Ha = 191
076 n
mi
Hp = 187
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14307632
41 X = 4405837
51
Y = -15771433
33 feet Y = -4758115
19 meter
Z = 5780339
28 Z = 1783142
16
XDOT = 15403
820097 XDOT = 4698
295310
YDOT = 7095
843259 feet/sec YDOT = 2215
334731 meter/sec
ZDOT = -18737
613925 ZDOT = -5688
407373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6380252
89 X = 1944701
08
Y = 20291431
75 feet Y = 6184828
40 meter
Z = 5865913
98 Z = 1787930
58
XDOT = -12491
068478 XDOT = -3807
277672
YDOT = 9326
232193 feet/sec YDOT = 2842
635573 meter/sec
ZDOT = -18645
963382 ZDOT = -5683
289639
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 10325
53527280
00016717 00000-0 10270-3 0 9044
2 25544 51
6397 145
3607 0007377 232
8792 127
1697 15
73049504 8229
Satellite: ISS
Catalog Number: 25544
Epoch time: 10325
53527280 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 145
3607 deg
Eccentricity:
0007377
Arg of perigee: 232
8792 deg
Mean anomaly: 127
1697 deg
Mean motion: 15
73049504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 822
Checksum: 317
Coasting Arc #6 (Orbit 837)
---------------------------------------
Vector Time (GMT): 2010/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4474864
32 A = 6724740
44 meter
Y = -1211170
01 meter E =
0007763
Z = 4874352
64 I = 51
84424
XDOT = 4191
715842 Wp = 181
15232
YDOT = -6013
321005 meter/sec RA = 139
44578 deg
ZDOT = 2346
460912 TA = 245
99468
MA = 246
07596
Ha = 191
071 n
mi
Hp = 187
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14681313
38 X = -4484667
51
Y = -3973654
88 feet Y = -1261265
96 meter
Z = 15991970
61 Z = 4852589
27
XDOT = 13752
348564 XDOT = 4247
247411
YDOT = -19728
743456 feet/sec YDOT = -5966
136473 meter/sec
ZDOT = 7698
362572 ZDOT = 2366
959028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10717781
22 X = 3266779
71
Y = -10920109
98 feet Y = -3328449
52 meter
Z = 15904539
71 Z = 4847703
70
XDOT = 9657
461068 XDOT = 2943
594133
YDOT = 20846
984558 feet/sec YDOT = 6354
160893 meter/sec
ZDOT = 7780
764380 ZDOT = 2371
576983
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 10326
55173502
00016717 00000-0 10270-3 0 9052
2 25544 51
6389 140
1473 0007303 235
1725 124
8751 15
73028047 8386
Satellite: ISS
Catalog Number: 25544
Epoch time: 10326
55173502 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 140
1473 deg
Eccentricity:
0007303
Arg of perigee: 235
1725 deg
Mean anomaly: 124
8751 deg
Mean motion: 15
73028047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 838
Checksum: 292
Coasting Arc #7 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2010/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2926212
24 A = 6732402
48 meter
Y = 5601967
49 meter E =
0002093
Z = -2317546
46 I = 51
89387
XDOT = -5408
388485 Wp = 273
96769
YDOT = -571
041764 meter/sec RA = 134
29392 deg
ZDOT = 5444
438361 TA = 60
08634
MA = 60
06555
Ha = 190
800 n
mi
Hp = 187
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9600433
84 X = -2977378
55
Y = 18379158
45 feet Y = 5568959
01 meter
Z = -7603498
89 Z = -2331885
93
XDOT = -17744
056708 XDOT = -5428
049651
YDOT = -1873
496601 feet/sec YDOT = -631
632176 meter/sec
ZDOT = 17862
330580 ZDOT = 5418
116051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11613710
40 X = -3539858
93
Y = -17152352
70 feet Y = -5228037
10 meter
Z = -7661169
49 Z = -2335124
46
XDOT = 8893
962580 XDOT = 2710
879794
YDOT = -13958
965477 feet/sec YDOT = -4254
692677 meter/sec
ZDOT = 17756
564821 ZDOT = 5412
200958
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 10327
50464098
00016717 00000-0 10270-3 0 9062
2 25544 51
6395 135
2597 0007299 237
5562 122
4896 15
73087851 8533
Satellite: ISS
Catalog Number: 25544
Epoch time: 10327
50464098 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 135
2597 deg
Eccentricity:
0007299
Arg of perigee: 237
5562 deg
Mean anomaly: 122
4896 deg
Mean motion: 15
73087851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 853
Checksum: 339
Coasting Arc #8 (Orbit 868)
---------------------------------------
Vector Time (GMT): 2010/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4872763
56 A = 6725396
52 meter
Y = -222478
79 meter E =
0003637
Z = -4633274
49 I = 51
89182
XDOT = -2479
392079 Wp = 86
97480
YDOT = 6670
760525 meter/sec RA = 129
22621 deg
ZDOT = -2929
638826 TA = 154
10115
MA = 154
08295
Ha = 190
591 n
mi
Hp = 187
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15986757
08 X = 4897397
15
Y = -729917
30 feet Y = -167850
35 meter
Z = -15201031
80 Z = -4609542
43
XDOT = -8134
488449 XDOT = -2539
569618
YDOT = 21885
697260 feet/sec YDOT = 6642
698338 meter/sec
ZDOT = -9611
675938 ZDOT = -2941
829304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6761032
65 X = -2060762
75
Y = 14604389
45 feet Y = 4451417
90 meter
Z = -15105654
41 Z = -4604203
46
XDOT = -14635
041720 XDOT = -4460
760716
YDOT = -16761
479245 feet/sec YDOT = -5108
898874 meter/sec
ZDOT = -9660
735211 ZDOT = -2944
592092
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 10328
52104813
00016717 00000-0 10270-3 0 9072
2 25544 51
6402 130
0476 0007118 241
8034 118
2410 15
73147166 8691
Satellite: ISS
Catalog Number: 25544
Epoch time: 10328
52104813 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 130
0476 deg
Eccentricity:
0007118
Arg of perigee: 241
8034 deg
Mean anomaly: 118
2410 deg
Mean motion: 15
73147166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 869
Checksum: 277
Coasting Arc #9 (Orbit 879)
---------------------------------------
Vector Time (GMT): 2010/329/05:07:35
497
Vector Time (MET): N/A
Weight (LBS) : 829753
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1278522
69 A = 6731603
88 meter
Y = 5872572
26 meter E =
0003353
Z = -3029255
12 I = 51
92632
XDOT = -5726
689385 Wp = 267
73340
YDOT = 1319
318434 meter/sec RA = 125
53775 deg
ZDOT = 4969
824931 TA = 57
39477
MA = 57
36241
Ha = 190
189 n
mi
Hp = 188
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4194628
25 X = -1329380
12
Y = 19266969
37 feet Y = 5857991
02 meter
Z = -9938501
05 Z = -3035589
16
XDOT = -18788
351002 XDOT = -5765
159425
YDOT = 4328
472554 feet/sec YDOT = 1255
063513 meter/sec
ZDOT = 16305
199906 ZDOT = 4941
911035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15518810
58 X = 4730133
46
Y = -12143705
93 feet Y = -3701401
57 meter
Z = -9964022
40 Z = -3037034
03
XDOT = 16388
182004 XDOT = 4995
117875
YDOT = 7643
489260 feet/sec YDOT = 2329
735527 meter/sec
ZDOT = 16192
994176 ZDOT = 4935
624625
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 10329
21981200
00016717 00000-0 10270-3 0 9083
2 25544 51
6437 126
4680 0007805 258
7848 101
2437 15
72794225 8805
Satellite: ISS
Catalog Number: 25544
Epoch time: 10329
21981200 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 126
4680 deg
Eccentricity:
0007805
Arg of perigee: 258
7848 deg
Mean anomaly: 101
2437 deg
Mean motion: 15
72794225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 880
Checksum: 312
Coasting Arc #10 (Orbit 895)
---------------------------------------
Vector Time (GMT): 2010/330/05:07:35
497
Vector Time (MET): N/A
Weight (LBS) : 829753
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4926600
05 A = 6728245
18 meter
Y = -2014383
56 meter E =
0001776
Z = -4116395
03 I = 51
93266
XDOT = -460
661228 Wp = 337
45506
YDOT = 6669
728720 meter/sec RA = 120
48170 deg
ZDOT = -3813
060897 TA = 253
53808
MA = 253
55760
Ha = 189
941 n
mi
Hp = 189
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16163386
00 X = 4968755
98
Y = -6608869
96 feet Y = -1959055
27 meter
Z = -13505233
04 Z = -4092359
19
XDOT = -1511
355734 XDOT = -516
685821
YDOT = 21882
312075 feet/sec YDOT = 6664
264431 meter/sec
ZDOT = -12510
042312 ZDOT = -3815
434278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16795642
50 X = -5119311
83
Y = -5043761
29 feet Y = -1537338
44 meter
Z = -13408594
03 Z = -4086939
46
XDOT = 14479
154169 XDOT = 4413
246191
YDOT = -14913
616034 feet/sec YDOT = -4545
670167 meter/sec
ZDOT = -12519
659652 ZDOT = -3815
992262
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 10330
23641828
00016717 00000-0 10270-3 0 9097
2 25544 51
6444 121
2572 0007875 263
8053 96
2212 15
72833405 8963
Satellite: ISS
Catalog Number: 25544
Epoch time: 10330
23641828 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 121
2572 deg
Eccentricity:
0007875
Arg of perigee: 263
8053 deg
Mean anomaly: 96
2212 deg
Mean motion: 15
72833405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 896
Checksum: 304
Coasting Arc #11 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2010/331/05:07:35
497
Vector Time (MET): N/A
Weight (LBS) : 829753
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -449223
04 A = 6729742
24 meter
Y = -5658708
47 meter E =
0004247
Z = 3611725
40 I = 51
95237
XDOT = 5382
141176 Wp = 82
05454
YDOT = -3260
492257 meter/sec RA = 115
32559 deg
ZDOT = -4433
998992 TA = 54
97141
MA = 54
93156
Ha = 189
175 n
mi
Hp = 188
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1473828
86 X = -403458
15
Y = -18565316
49 feet Y = -5663476
32 meter
Z = 11849492
79 Z = 3609653
82
XDOT = 17657
943490 XDOT = 5439
740311
YDOT = -10697
153074 feet/sec YDOT = -3199
983548 meter/sec
ZDOT = -14547
240787 ZDOT = -4407
712682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10177567
79 X = -3102122
66
Y = 15603073
84 feet Y = 4755816
91 meter
Z = 11841234
22 Z = 3609208
19
XDOT = -19436
545792 XDOT = -5924
259157
YDOT = -1705
908186 feet/sec YDOT = -519
960815 meter/sec
ZDOT = -14441
529233 ZDOT = -4401
778110
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 10331
25299841
00016717 00000-0 10270-3 0 9106
2 25544 51
6441 116
0460 0007793 268
2118 91
8152 15
72868340 9127
Satellite: ISS
Catalog Number: 25544
Epoch time: 10331
25299841 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 116
0460 deg
Eccentricity:
0007793
Arg of perigee: 268
2118 deg
Mean anomaly: 91
8152 deg
Mean motion: 15
72868340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 297
Coasting Arc #12 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2010/332/05:07:35
497
Vector Time (MET): N/A
Weight (LBS) : 829753
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4360466
06 A = 6729707
47 meter
Y = 3620900
00 meter E =
0004229
Z = 3625090
81 I = 51
96470
XDOT = -1419
099681 Wp = 96
09335
YDOT = -6140
027970 meter/sec RA = 110
27179 deg
ZDOT = 4421
135875 TA = 307
07040
MA = 307
10906
Ha = 189
339 n
mi
Hp = 188
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14305991
02 X = -4418241
74
Y = 11879593
16 feet Y = 3571815
42 meter
Z = 11893342
54 Z = 3603767
33
XDOT = -4655
838848 XDOT = -1371
812526
YDOT = -20144
448721 feet/sec YDOT = -6155
633020 meter/sec
ZDOT = 14505
038961 ZDOT = 4414
356389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18629453
80 X = 5678257
52
Y = -873202
47 feet Y = -266152
11 meter
Z = 11807568
69 Z = 3598946
94
XDOT = -8361
402795 XDOT = -2548
555572
YDOT = 17599
656910 feet/sec YDOT = 5364
375426 meter/sec
ZDOT = 14477
862956 ZDOT = 4412
852629
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 10332
26955082
00016717 00000-0 10270-3 0 9115
2 25544 51
6445 110
8337 0007826 273
0705 86
9562 15
72892191 9287
Satellite: ISS
Catalog Number: 25544
Epoch time: 10332
26955082 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 110
8337 deg
Eccentricity:
0007826
Arg of perigee: 273
0705 deg
Mean anomaly: 86
9562 deg
Mean motion: 15
72892191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 316
Coasting Arc #13 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2010/333/05:07:35
497
Vector Time (MET): N/A
Weight (LBS) : 829753
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1972050
25 A = 6727934
54 meter
Y = 4965343
58 meter E =
0001725
Z = -4089499
63 I = 51
96867
XDOT = -4460
178551 Wp = 210
18984
YDOT = 4948
379362 meter/sec RA = 105
11627 deg
ZDOT = 3855
212683 TA = 99
30636
MA = 99
28685
Ha = 189
815 n
mi
Hp = 188
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6469981
14 X = 1936246
56
Y = 16290497
31 feet Y = 4987196
19 meter
Z = -13416993
53 Z = -4080006
09
XDOT = -14633
131728 XDOT = -4533
908896
YDOT = 16234
840425 feet/sec YDOT = 4898
090575 meter/sec
ZDOT = 12648
335574 ZDOT = 3833
365974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4246324
12 X = 1294279
59
Y = -17036155
54 feet Y = -5192620
21 meter
Z = -13378894
19 Z = -4077886
95
XDOT = 20191
797903 XDOT = 6154
460001
YDOT = -4836
693809 feet/sec YDOT = -1474
224273 meter/sec
ZDOT = 12560
431584 ZDOT = 3828
419547
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 10333
22254251
00016717 00000-0 10270-3 0 9123
2 25544 51
6443 105
9476 0008029 277
0356 82
9893 15
72952799 9437
Satellite: ISS
Catalog Number: 25544
Epoch time: 10333
22254251 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 105
9476 deg
Eccentricity:
0008029
Arg of perigee: 277
0356 deg
Mean anomaly: 82
9893 deg
Mean motion: 15
72952799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 324
Coasting Arc #14 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2010/334/05:07:35
497
Vector Time (MET): N/A
Weight (LBS) : 829753
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3347804
35 A = 6730958
29 meter
Y = -4938655
01 meter E =
0003629
Z = -3113036
33 I = 51
98546
XDOT = 2987
315817 Wp = 275
45392
YDOT = 5121
761829 meter/sec RA = 100
06220 deg
ZDOT = -4907
579223 TA = 300
50036
MA = 300
53619
Ha = 190
000 n
mi
Hp = 188
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10983610
06 X = 3417903
29
Y = -16202936
38 feet Y = -4900825
80 meter
Z = -10213373
77 Z = -3096602
33
XDOT = 9800
904911 XDOT = 2953
661800
YDOT = 16803
680541 feet/sec YDOT = 5154
979789 meter/sec
ZDOT = -16100
981702 ZDOT = -4893
148189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18330257
88 X = -5587062
60
Y = 6965871
19 feet Y = 2123197
54 meter
Z = -10147222
57 Z = -3092873
44
XDOT = 2009
819921 XDOT = 612
593112
YDOT = -18106
287917 feet/sec YDOT = -5518
796557 meter/sec
ZDOT = -16043
038464 ZDOT = -4889
918124
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 10334
23904156
00016717 00000-0 10270-3 0 9132
2 25544 51
6440 100
7357 0008125 280
6645 79
3603 15
72968898 9596
Satellite: ISS
Catalog Number: 25544
Epoch time: 10334
23904156 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 100
7357 deg
Eccentricity:
0008125
Arg of perigee: 280
6645 deg
Mean anomaly: 79
3603 deg
Mean motion: 15
72968898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 322
Coasting Arc #15 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2010/335/05:07:35
497
Vector Time (MET): N/A
Weight (LBS) : 829753
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3167209
20 A = 6726227
75 meter
Y = -3912779
86 meter E =
0005652
Z = 4463580
50 I = 51
97503
XDOT = 3099
584893 Wp = 6
53510
YDOT = -6241
520631 meter/sec RA = 94
90970 deg
ZDOT = -3266
071334 TA = 116
09079
MA = 116
03261
Ha = 190
172 n
mi
Hp = 188
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10391106
31 X = -3144904
07
Y = -12837204
27 feet Y = -3948072
99 meter
Z = 14644292
97 Z = 4448247
89
XDOT = 10169
241774 XDOT = 3185
014670
YDOT = -20477
429892 feet/sec YDOT = -6206
381394 meter/sec
ZDOT = -10715
457131 ZDOT = -3250
806023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1529197
19 X = 466099
30
Y = 16499402
92 feet Y = 5029018
01 meter
Z = 14582711
66 Z = 4444810
51
XDOT = -18717
187974 XDOT = -5704
998895
YDOT = 11168
225262 feet/sec YDOT = 3404
075060 meter/sec
ZDOT = -10653
971379 ZDOT = -3247
330476
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 10335
25551157
00016717 00000-0 10270-3 0 9145
2 25544 51
6442 95
5230 0008162 286
1669 73
8595 15
73076780 9755
Satellite: ISS
Catalog Number: 25544
Epoch time: 10335
25551157 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 95
5230 deg
Eccentricity:
0008162
Arg of perigee: 286
1669 deg
Mean anomaly: 73
8595 deg
Mean motion: 15
73076780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 324
Coasting Arc #16 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2010/336/05:07:35
497
Vector Time (MET): N/A
Weight (LBS) : 829753
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2015044
75 A = 6731893
29 meter
Y = 5868113
89 meter E =
0008227
Z = 2598291
32 I = 51
99483
XDOT = -4142
265999 Wp = 44
04105
YDOT = -3765
785845 meter/sec RA = 89
85015 deg
ZDOT = 5288
249894 TA = 345
31428
MA = 345
33817
Ha = 190
460 n
mi
Hp = 188
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6611039
20 X = -2093135
64
Y = 19252342
15 feet Y = 5845143
64 meter
Z = 8524577
84 Z = 2588312
73
XDOT = -13590
111546 XDOT = -4125
538359
YDOT = -12354
940435 feet/sec YDOT = -3812
013986 meter/sec
ZDOT = 17349
901228 ZDOT = 5268
166683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16060140
85 X = 4895130
93
Y = -12534543
47 feet Y = -3820528
85 meter
Z = 8484340
91 Z = 2586027
11
XDOT = 3859
181551 XDOT = 1176
278537
YDOT = 16643
060162 feet/sec YDOT = 5072
804737 meter/sec
ZDOT = 17269
221786 ZDOT = 5263
658800
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 10336
27195641
00016717 00000-0 10270-3 0 9151
2 25544 51
6435 90
3097 0008176 290
1966 69
8317 15
73079718 9910
Satellite: ISS
Catalog Number: 25544
Epoch time: 10336
27195641 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 90
3097 deg
Eccentricity:
0008176
Arg of perigee: 290
1966 deg
Mean anomaly: 69
8317 deg
Mean motion: 15
73079718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 335
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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