Date:
November 9th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 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
There are no maneuvers
Coasting Arc #1 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2010/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5090918
15 A = 6728289
28 meter
Y = 937271
34 meter E =
0013861
Z = -4312190
15 I = 51
46057
XDOT = -3962
078953 Wp = 140
53734
YDOT = -5608
520333 meter/sec RA = 211
14046 deg
ZDOT = 3454
106535 TA = 164
54873
MA = 164
50637
Ha = 194
000 n
mi
Hp = 185
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16702487
38 X = -5080072
17
Y = 3075037
22 feet Y = 880402
57 meter
Z = -14147605
49 Z = -4336896
04
XDOT = -12998
946695 XDOT = -3915
848798
YDOT = -18400
657260 feet/sec YDOT = -5652
568424 meter/sec
ZDOT = 11332
370521 ZDOT = 3434
970205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9137880
90 X = 2785226
10
Y = -14216667
80 feet Y = -4333240
34 meter
Z = -14246724
86 Z = -4342401
74
XDOT = 21320
142706 XDOT = 6498
379497
YDOT = 2409
803238 feet/sec YDOT = 734
508027 meter/sec
ZDOT = 11255
599065 ZDOT = 3430
706595
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 10312
50978463
00016717 00000-0 10270-3 0 9006
2 25544 51
6463 212
1246 0007514 175
9528 184
1696 15
72499019 6175
Satellite: ISS
Catalog Number: 25544
Epoch time: 10312
50978463 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 212
1246 deg
Eccentricity:
0007514
Arg of perigee: 175
9528 deg
Mean anomaly: 184
1696 deg
Mean motion: 15
72499019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 315
Coasting Arc #2 (Orbit 632)
---------------------------------------
Vector Time (GMT): 2010/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4307308
47 A = 6733392
17 meter
Y = 4443550
80 meter E =
0011303
Z = -2640923
69 I = 51
50442
XDOT = -5285
782471 Wp = 160
18415
YDOT = 2033
668838 meter/sec RA = 206
05202 deg
ZDOT = -5216
187917 TA = 49
91487
MA = 49
81583
Ha = 193
882 n
mi
Hp = 185
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14131589
48 X = 4270129
11
Y = 14578578
75 feet Y = 4491510
02 meter
Z = -8664447
82 Z = -2620088
37
XDOT = -17341
806007 XDOT = -5282
790682
YDOT = 6672
141857 feet/sec YDOT = 1974
577138 meter/sec
ZDOT = -17113
477417 ZDOT = -5241
859345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20326883
47 X = -6195634
08
Y = 704481
84 feet Y = 214726
06 meter
Z = -8580847
82 Z = -2615442
42
XDOT = 6697
651641 XDOT = 2041
444220
YDOT = -15767
274486 feet/sec YDOT = -4805
865263 meter/sec
ZDOT = -17216
484906 ZDOT = -5247
584599
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 10313
52657110
00016717 00000-0 10270-3 0 9013
2 25544 51
6462 206
9149 0007599 181
0731 179
0416 15
72528894 6339
Satellite: ISS
Catalog Number: 25544
Epoch time: 10313
52657110 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 206
9149 deg
Eccentricity:
0007599
Arg of perigee: 181
0731 deg
Mean anomaly: 179
0416 deg
Mean motion: 15
72528894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 633
Checksum: 306
Coasting Arc #3 (Orbit 648)
---------------------------------------
Vector Time (GMT): 2010/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4010105
92 A = 6726057
71 meter
Y = -2526739
93 meter E =
0006744
Z = 4765950
94 I = 51
50845
XDOT = 5796
334933 Wp = 124
36082
YDOT = 4384
184219 meter/sec RA = 200
87607 deg
ZDOT = -2553
922021 TA = 350
69369
MA = 350
70619
Ha = 193
401 n
mi
Hp = 185
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13156515
48 X = 4014909
86
Y = -8289829
16 feet Y = -2481869
96 meter
Z = 15636321
99 Z = 4785443
85
XDOT = 19016
846894 XDOT = 5759
286054
YDOT = 14383
806492 feet/sec YDOT = 4448
795335 meter/sec
ZDOT = -8379
009256 ZDOT = -2525
852693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2378876
27 X = -725081
49
Y = 15287369
19 feet Y = 4659590
13 meter
Z = 15714548
14 Z = 4789794
27
XDOT = -22269
910143 XDOT = -6787
868612
YDOT = 5027
948388 feet/sec YDOT = 1532
518669 meter/sec
ZDOT = -8266
366143 ZDOT = -2519
588400
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 10314
54332133
00016717 00000-0 10270-3 0 9022
2 25544 51
6458 201
7050 0007415 185
2758 174
8328 15
72642911 6499
Satellite: ISS
Catalog Number: 25544
Epoch time: 10314
54332133 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 201
7050 deg
Eccentricity:
0007415
Arg of perigee: 185
2758 deg
Mean anomaly: 174
8328 deg
Mean motion: 15
72642911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 649
Checksum: 295
Coasting Arc #4 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2010/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5684177
33 A = 6734628
09 meter
Y = -3112309
35 meter E =
0011799
Z = 1826274
29 I = 51
56595
XDOT = 3792
107433 Wp = 97
58720
YDOT = -3589
695260 meter/sec RA = 195
77982 deg
ZDOT = 5652
569966 TA = 282
67258
MA = 282
80446
Ha = 193
372 n
mi
Hp = 185
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18648875
76 X = -5657824
27
Y = -10210988
69 feet Y = -3175725
99 meter
Z = 5991713
56 Z = 1798724
06
XDOT = 12441
297351 XDOT = 3804
506719
YDOT = -11777
215420 feet/sec YDOT = -3547
220602 meter/sec
ZDOT = 18545
177055 ZDOT = 5671
022190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19866297
18 X = 6055247
38
Y = -7660805
47 feet Y = -2335013
51 meter
Z = 5881138
03 Z = 1792570
87
XDOT = 460
513917 XDOT = 140
364642
YDOT = 15571
835341 feet/sec YDOT = 4746
295412 meter/sec
ZDOT = 18619
234613 ZDOT = 5675
142710
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 10315
56003911
00016717 00000-0 10270-3 0 9035
2 25544 51
6457 196
4942 0007391 189
1554 170
9475 15
72650517 6657
Satellite: ISS
Catalog Number: 25544
Epoch time: 10315
56003911 = yrday
fracday
Element set: 903
Inclination: 51
6457 deg
RA of node: 196
4942 deg
Eccentricity:
0007391
Arg of perigee: 189
1554 deg
Mean anomaly: 170
9475 deg
Mean motion: 15
72650517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 316
Coasting Arc #5 (Orbit 679)
---------------------------------------
Vector Time (GMT): 2010/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2557438
94 A = 6724603
56 meter
Y = 3616296
67 meter E =
0015397
Z = -5072272
24 I = 51
56259
XDOT = -7027
120026 Wp = 131
40449
YDOT = -2648
317113 meter/sec RA = 190
61857 deg
ZDOT = 1648
173895 TA = 154
51712
MA = 154
44114
Ha = 193
084 n
mi
Hp = 185
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8390547
69 X = -2573046
49
Y = 11864490
40 feet Y = 3587610
77 meter
Z = -16641313
11 Z = -5084734
20
XDOT = -23054
855728 XDOT = -7004
990399
YDOT = -8688
704440 feet/sec YDOT = -2726
774921 meter/sec
ZDOT = 5407
394668 ZDOT = 1614
089408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3936243
85 X = -1199767
13
Y = -13928608
34 feet Y = -4245439
82 meter
Z = -16691332
46 Z = -5087518
13
XDOT = 20324
071229 XDOT = 6194
776911
YDOT = -12086
140400 feet/sec YDOT = -3683
855594 meter/sec
ZDOT = 5270
576658 ZDOT = 1606
471765
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 10316
51317870
00016717 00000-0 10270-3 0 9044
2 25544 51
6456 191
6090 0007420 193
7422 166
3540 15
72723149 6806
Satellite: ISS
Catalog Number: 25544
Epoch time: 10316
51317870 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 191
6090 deg
Eccentricity:
0007420
Arg of perigee: 193
7422 deg
Mean anomaly: 166
3540 deg
Mean motion: 15
72723149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 294
Coasting Arc #6 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2010/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6477348
46 A = 6735369
55 meter
Y = 1468989
31 meter E =
0015372
Z = -1060676
41 I = 51
62887
XDOT = -1987
611306 Wp = 166
45337
YDOT = 4514
819956 meter/sec RA = 185
51381 deg
ZDOT = -5917
008589 TA = 25
15049
MA = 25
07570
Ha = 193
061 n
mi
Hp = 186
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21251143
25 X = 6465593
17
Y = 4819518
72 feet Y = 1541357
21 meter
Z = -3479909
49 Z = -1029237
60
XDOT = -6521
034470 XDOT = -2009
205030
YDOT = 14812
401431 feet/sec YDOT = 4492
472670 meter/sec
ZDOT = -19412
757839 ZDOT = -5926
716886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16962138
98 X = -5170059
96
Y = 13710841
19 feet Y = 4179064
39 meter
Z = -3353698
79 Z = -1022207
39
XDOT = -6657
782568 XDOT = -2029
292127
YDOT = -12967
957931 feet/sec YDOT = -3952
633577 meter/sec
ZDOT = -19451
725184 ZDOT = -5928
885836
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 10317
52982928
00016717 00000-0 10270-3 0 9059
2 25544 51
6457 186
3987 0007602 197
9353 162
1543 15
72720502 6968
Satellite: ISS
Catalog Number: 25544
Epoch time: 10317
52982928 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 186
3987 deg
Eccentricity:
0007602
Arg of perigee: 197
9353 deg
Mean anomaly: 162
1543 deg
Mean motion: 15
72720502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 331
Coasting Arc #7 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2010/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 881430
82 A = 6723611
69 meter
Y = -4134745
61 meter E =
0005422
Z = 5227705
98 I = 51
62072
XDOT = 7632
912633 Wp = 181
47659
YDOT = 659
619594 meter/sec RA = 180
37002 deg
ZDOT = -770
595264 TA = 275
82705
MA = 275
88886
Ha = 192
658 n
mi
Hp = 186
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2891833
39 X = 902205
19
Y = -13565438
34 feet Y = -4124772
80 meter
Z = 17151266
33 Z = 5232038
46
XDOT = 25042
364282 XDOT = 7628
712809
YDOT = 2164
106281 feet/sec YDOT = 744
951938 meter/sec
ZDOT = -2528
199685 ZDOT = -733
524244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9099969
59 X = 2773670
73
Y = 10439234
72 feet Y = 3181878
74 meter
Z = 17168654
19 Z = 5233005
80
XDOT = -16144
173048 XDOT = -4920
743945
YDOT = 17957
395809 feet/sec YDOT = 5473
414242 meter/sec
ZDOT = -2379
366306 ZDOT = -725
230850
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 10318
54644337
00016717 00000-0 10270-3 0 9062
2 25544 51
6456 181
1874 0007413 202
4800 157
6039 15
72826249 7127
Satellite: ISS
Catalog Number: 25544
Epoch time: 10318
54644337 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 181
1874 deg
Eccentricity:
0007413
Arg of perigee: 202
4800 deg
Mean anomaly: 157
6039 deg
Mean motion: 15
72826249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 303
Coasting Arc #8 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2010/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6719443
75 A = 6735319
09 meter
Y = 314037
35 meter E =
0006410
Z = 307721
50 I = 51
69027
XDOT = 57
126040 Wp = 72
95515
YDOT = -4782
857671 meter/sec RA = 175
25305 deg
ZDOT = 6027
283403 TA = 290
38355
MA = 290
45239
Ha = 192
409 n
mi
Hp = 186
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22045419
11 X = -6723950
84
Y = 1030306
25 feet Y = 238871
28 meter
Z = 1009584
97 Z = 275066
93
XDOT = 187
421390 XDOT = 81
324637
YDOT = -15691
790260 feet/sec YDOT = -4782
083553 meter/sec
ZDOT = 19774
551847 ZDOT = 6027
619704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12228513
46 X = 3727250
90
Y = -18378602
77 feet Y = -5601798
12 meter
Z = 878473
43 Z = 267758
70
XDOT = 11262
088293 XDOT = 3432
684512
YDOT = 8456
912717 feet/sec YDOT = 2577
666996 meter/sec
ZDOT = 19775
895337 ZDOT = 6027
692899
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 10319
56302382
00016717 00000-0 10270-3 0 9077
2 25544 51
6448 175
9754 0007417 207
0108 153
0669 15
72884886 7289
Satellite: ISS
Catalog Number: 25544
Epoch time: 10319
56302382 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 175
9754 deg
Eccentricity:
0007417
Arg of perigee: 207
0108 deg
Mean anomaly: 153
0669 deg
Mean motion: 15
72884886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 330
Coasting Arc #9 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2010/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 750630
04 A = 6723145
84 meter
Y = 4105513
95 meter E =
0012819
Z = -5280440
67 I = 51
67876
XDOT = -7572
375766 Wp = 119
02573
YDOT = 1346
605770 meter/sec RA = 170
12614 deg
ZDOT = -35
619067 TA = 150
67207
MA = 150
60006
Ha = 192
153 n
mi
Hp = 186
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2462696
97 X = 730317
59
Y = 13469533
96 feet Y = 4113794
37 meter
Z = -17324280
43 Z = -5276843
38
XDOT = -24843
752514 XDOT = -7586
697926
YDOT = 4417
997934 feet/sec YDOT = 1261
846829 meter/sec
ZDOT = -116
860455 ZDOT = -72
441227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12472258
69 X = -3801544
45
Y = -5695296
33 feet Y = -1735926
32 meter
Z = -17309831
79 Z = -5276036
73
XDOT = 10345
688060 XDOT = 3153
365721
YDOT = -21913
201185 feet/sec YDOT = -6679
143721 meter/sec
ZDOT = -264
715788 ZDOT = -80
685372
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 10320
51603779
00016717 00000-0 10270-3 0 9089
2 25544 51
6436 171
0888 0007350 211
1091 148
9637 15
72932517 7434
Satellite: ISS
Catalog Number: 25544
Epoch time: 10320
51603779 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 171
0888 deg
Eccentricity:
0007350
Arg of perigee: 211
1091 deg
Mean anomaly: 148
9637 deg
Mean motion: 15
72932517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 743
Checksum: 307
Coasting Arc #10 (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 = 6406951
58 A = 6735058
90 meter
Y = -2011604
95 meter E =
0015526
Z = 361416
52 I = 51
74920
XDOT = 1744
132731 Wp = 159
35330
YDOT = 4459
095924 meter/sec RA = 165
00090 deg
ZDOT = -6036
033285 TA = 16
72264
MA = 16
67151
Ha = 191
952 n
mi
Hp = 186
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21020182
36 X = 6427213
80
Y = -6599753
78 feet Y = -1939845
27 meter
Z = 1185749
75 Z = 392591
47
XDOT = 5722
220247 XDOT = 1723
463340
YDOT = 14629
579803 feet/sec YDOT = 4478
484327 meter/sec
ZDOT = -19803
258808 ZDOT = -6027
610265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6404853
29 X = -1952199
28
Y = 21072971
10 feet Y = 6423041
59 meter
Z = 1310939
53 Z = 399574
37
XDOT = -13836
568149 XDOT = -4217
385972
YDOT = -2963
790805 feet/sec YDOT = -903
363437 meter/sec
ZDOT = -19769
433434 ZDOT = -6025
723311
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
53255272
00016717 00000-0 10270-3 0 9094
2 25544 51
6437 165
8779 0007355 215
2378 144
8299 15
72965445 7595
Satellite: ISS
Catalog Number: 25544
Epoch time: 10321
53255272 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 165
8779 deg
Eccentricity:
0007355
Arg of perigee: 215
2378 deg
Mean anomaly: 144
8299 deg
Mean motion: 15
72965445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 343
Coasting Arc #11 (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 = -2238964
99 A = 6723207
99 meter
Y = -3577732
10 meter E =
0007530
Z = 5235778
89 I = 51
73742
XDOT = 6956
520899 Wp = 194
11719
YDOT = -3202
059907 meter/sec RA = 159
89015 deg
ZDOT = 779
833017 TA = 248
42947
MA = 248
50973
Ha = 191
819 n
mi
Hp = 186
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7345685
66 X = -2224226
89
Y = -11737966
21 feet Y = -3602687
24 meter
Z = 17177752
26 Z = 5224937
43
XDOT = 22823
231297 XDOT = 6988
021505
YDOT = -10505
445888 feet/sec YDOT = -3124
091789 meter/sec
ZDOT = 2558
507272 ZDOT = 813
705188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13898865
47 X = 4236374
20
Y = 233024
88 feet Y = 71025
98 meter
Z = 17134216
04 Z = 5222509
05
XDOT = -3749
101364 XDOT = -1142
726096
YDOT = 23813
202566 feet/sec YDOT = 7258
264142 meter/sec
ZDOT = 2694
542711 ZDOT = 821
296618
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
54903343
00016717 00000-0 10270-3 0 9107
2 25544 51
6426 160
6649 0007318 219
2009 140
8625 15
72988095 7759
Satellite: ISS
Catalog Number: 25544
Epoch time: 10322
54903343 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 160
6649 deg
Eccentricity:
0007318
Arg of perigee: 219
2009 deg
Mean anomaly: 140
8625 deg
Mean motion: 15
72988095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 310
Coasting Arc #12 (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 = -5657960
54 A = 6734386
67 meter
Y = 3516829
91 meter E =
0002547
Z = -975718
78 I = 51
80284
XDOT = -3277
225796 Wp = 22
59272
YDOT = -3625
440611 meter/sec RA = 154
75373 deg
ZDOT = 5943
909333 TA = 326
78118
MA = 326
79717
Ha = 191
464 n
mi
Hp = 186
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18562862
67 X = -5692125
86
Y = 11538155
88 feet Y = 3453368
20 meter
Z = -3201177
11 Z = -1003288
82
XDOT = -10752
053136 XDOT = -3265
317160
YDOT = -11894
490195 feet/sec YDOT = -3662
022164 meter/sec
ZDOT = 19501
014873 ZDOT = 5928
016888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 183261
20 X = 55858
01
Y = -21839277
92 feet Y = -6656611
91 meter
Z = -3311918
10 Z = -1009472
64
XDOT = 14271
538317 XDOT = 4349
964879
YDOT = -2824
322981 feet/sec YDOT = -860
853645 meter/sec
ZDOT = 19437
193300 ZDOT = 5924
456518
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
50195053
00016717 00000-0 10270-3 0 9116
2 25544 51
6413 155
7771 0007395 223
7063 136
3514 15
73066108 7908
Satellite: ISS
Catalog Number: 25544
Epoch time: 10323
50195053 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 155
7771 deg
Eccentricity:
0007395
Arg of perigee: 223
7063 deg
Mean anomaly: 136
3514 deg
Mean motion: 15
73066108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 288
Coasting Arc #13 (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 = 3406553
26 A = 6723279
20 meter
Y = 2693396
13 meter E =
0008669
Z = -5139232
60 I = 51
79201
XDOT = -5888
605454 Wp = 105
92972
YDOT = 4743
488525 meter/sec RA = 149
65754 deg
ZDOT = -1421
588321 TA = 150
49487
MA = 150
44591
Ha = 191
266 n
mi
Hp = 186
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11176355
83 X = 3401148
22
Y = 8836601
48 feet Y = 2731460
36 meter
Z = -16860999
35 Z = -5122696
03
XDOT = -19319
571699 XDOT = -5934
304340
YDOT = 15562
626393 feet/sec YDOT = 4677
383170 meter/sec
ZDOT = -4664
003677 ZDOT = -1450
306729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13415800
82 X = -4089136
09
Y = 5024730
00 feet Y = 1531537
70 meter
Z = -16794586
37 Z = -5118989
92
XDOT = -2872
035233 XDOT = -875
396339
YDOT = -23595
351459 feet/sec YDOT = -7191
863125 meter/sec
ZDOT = -4779
379414 ZDOT = -1456
754845
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
51836330
00016717 00000-0 10270-3 0 9129
2 25544 51
6403 150
5641 0007312 226
8903 133
1649 15
73129735 8060
Satellite: ISS
Catalog Number: 25544
Epoch time: 10324
51836330 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 150
5641 deg
Eccentricity:
0007312
Arg of perigee: 226
8903 deg
Mean anomaly: 133
1649 deg
Mean motion: 15
73129735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 283
Coasting Arc #14 (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 = 4568833
94 A = 6733368
20 meter
Y = -4701926
78 meter E =
0012763
Z = 1497911
14 I = 51
85325
XDOT = 4427
264416 Wp = 149
38735
YDOT = 2447
690536 meter/sec RA = 144
51520 deg
ZDOT = -5809
703557 TA = 14
15990
MA = 14
12416
Ha = 190
768 n
mi
Hp = 186
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14989612
68 X = 4613795
41
Y = -15426268
96 feet Y = -4650584
07 meter
Z = 4914406
61 Z = 1520215
96
XDOT = 14525
145721 XDOT = 4427
788118
YDOT = 8030
480761 feet/sec YDOT = 2497
202301 meter/sec
ZDOT = -19060
707209 ZDOT = -5788
193815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5734867
83 X = 1747987
72
Y = 20709431
30 feet Y = 6312234
66 meter
Z = 5004038
46 Z = 1525230
92
XDOT = -12823
055023 XDOT = -3908
467171
YDOT = 8144
144266 feet/sec YDOT = 2482
335172 meter/sec
ZDOT = -18974
311329 ZDOT = -5783
370093
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
53473886
00016717 00000-0 10270-3 0 9136
2 25544 51
6408 145
3509 0007312 233
4267 126
6224 15
73227564 8220
Satellite: ISS
Catalog Number: 25544
Epoch time: 10325
53473886 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 145
3509 deg
Eccentricity:
0007312
Arg of perigee: 233
4267 deg
Mean anomaly: 126
6224 deg
Mean motion: 15
73227564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 822
Checksum: 300
Coasting Arc #15 (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 = -4231884
95 A = 6723706
68 meter
Y = -1543070
73 meter E =
0007499
Z = 4994925
97 I = 51
84371
XDOT = 4508
318700 Wp = 188
02196
YDOT = -5913
899681 meter/sec RA = 139
43001 deg
ZDOT = 1985
732055 TA = 242
78658
MA = 242
86301
Ha = 190
763 n
mi
Hp = 187
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13884136
97 X = -4238580
56
Y = -5062568
01 feet Y = -1590432
18 meter
Z = 16387552
40 Z = 4974350
54
XDOT = 14791
071851 XDOT = 4564
467389
YDOT = -19402
558009 feet/sec YDOT = -5863
171216 meter/sec
ZDOT = 6514
868948 ZDOT = 2007
769776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11275960
24 X = 3436912
68
Y = -9692976
19 feet Y = -2954419
14 meter
Z = 16304896
84 Z = 4969732
56
XDOT = 8949
259692 XDOT = 2727
734354
YDOT = 21557
042913 feet/sec YDOT = 6570
586680 meter/sec
ZDOT = 6603
455797 ZDOT = 2012
733327
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
55108356
00016717 00000-0 10270-3 0 9147
2 25544 51
6400 140
1367 0007221 235
6276 124
4204 15
73207074 8385
Satellite: ISS
Catalog Number: 25544
Epoch time: 10326
55108356 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 140
1367 deg
Eccentricity:
0007221
Arg of perigee: 235
6276 deg
Mean anomaly: 124
4204 deg
Mean motion: 15
73207074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 838
Checksum: 276
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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