Date:
November 11th 2009
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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2900)
---------------------------------------
Vector Time (GMT): 2009/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4087882
33 A = 6714285
75 meter
Y = 1167084
40 meter E =
0006223
Z = 5199123
45 I = 51
28902
XDOT = -1199
957123 Wp = 343
96002
YDOT = 7571
903307 meter/sec RA = 274
50478 deg
ZDOT = -750
545234 TA = 113
24581
MA = 113
18028
Ha = 186
424 n
mi
Hp = 182
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13411687
45 X = 4049271
19
Y = 3829017
05 feet Y = 1212581
59 meter
Z = 17057491
64 Z = 5218888
90
XDOT = -3936
867201 XDOT = -1280
892214
YDOT = 24842
202452 feet/sec YDOT = 7558
032152 meter/sec
ZDOT = -2462
418746 ZDOT = -756
571261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11622091
62 X = -3542413
53
Y = 7536216
30 feet Y = 2297038
73 meter
Z = 17135494
83 Z = 5222898
83
XDOT = -15629
009071 XDOT = -4763
721965
YDOT = -18407
945105 feet/sec YDOT = -5610
741668 meter/sec
ZDOT = -2485
893914 ZDOT = -757
700465
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 09314
54630023
00016717 00000-0 10270-3 0 9007
2 25544 51
6426 275
0177 0006320 315
2108 44
8545 15
76107526 29018
Satellite: ISS
Catalog Number: 25544
Epoch time: 09314
54630023 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 275
0177 deg
Eccentricity:
0006320
Arg of perigee: 315
2108 deg
Mean anomaly: 44
8545 deg
Mean motion: 15
76107526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 279
Coasting Arc #2 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2009/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1016274
21 A = 6725217
85 meter
Y = -6497746
26 meter E =
0014117
Z = 1361849
80 I = 51
32528
XDOT = 4673
891074 Wp = 34
43973
YDOT = 1952
690689 meter/sec RA = 269
34877 deg
ZDOT = 5811
143256 TA = 340
61403
MA = 340
66767
Ha = 186
486 n
mi
Hp = 181
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3334232
98 X = 1082241
87
Y = -21318065
17 feet Y = -6486012
83 meter
Z = 4468011
15 Z = 1366947
23
XDOT = 15334
288299 XDOT = 4623
478357
YDOT = 6406
465515 feet/sec YDOT = 2004
675064 meter/sec
ZDOT = 19065
430630 ZDOT = 5833
726974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14202820
70 X = 4329019
75
Y = 16238200
29 feet Y = 4949403
45 meter
Z = 4487858
20 Z = 1367899
18
XDOT = -13509
345902 XDOT = -4117
648631
YDOT = 6506
075604 feet/sec YDOT = 1983
051844 meter/sec
ZDOT = 19154
583763 ZDOT = 5838
317131
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 09315
56075638
00016717 00000-0 10270-3 0 9016
2 25544 51
6426 269
7916 0006265 318
4074 41
6613 15
76163431 29179
Satellite: ISS
Catalog Number: 25544
Epoch time: 09315
56075638 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 269
7916 deg
Eccentricity:
0006265
Arg of perigee: 318
4074 deg
Mean anomaly: 41
6613 deg
Mean motion: 15
76163431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 319
Coasting Arc #3 (Orbit 2931)
---------------------------------------
Vector Time (GMT): 2009/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4114512
04 A = 6715778
33 meter
Y = -2226058
49 meter E =
0007864
Z = -4824508
44 I = 51
29551
XDOT = 1156
492410 Wp = 78
99625
YDOT = -7237
334275 meter/sec RA = 264
14100 deg
ZDOT = 2357
782747 TA = 214
08407
MA = 214
13460
Ha = 186
641 n
mi
Hp = 181
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13499055
26 X = -4065876
92
Y = -7303341
51 feet Y = -2271797
49 meter
Z = -15828439
76 Z = -4844379
06
XDOT = 3794
266437 XDOT = 1225
881637
YDOT = -23744
535023 feet/sec YDOT = -7224
013702 meter/sec
ZDOT = 7735
507700 ZDOT = 2363
569720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14114822
61 X = 4302197
93
Y = -5817639
57 feet Y = -1773216
54 meter
Z = -15906905
67 Z = -4848424
85
XDOT = 15663
370597 XDOT = 4774
195358
YDOT = 16832
406015 feet/sec YDOT = 5130
517353 meter/sec
ZDOT = 7758
039834 ZDOT = 2364
650541
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 09316
51179401
00016717 00000-0 10270-3 0 9026
2 25544 51
6430 264
8920 0006407 322
5484 37
5234 15
76164544 29320
Satellite: ISS
Catalog Number: 25544
Epoch time: 09316
51179401 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 264
8920 deg
Eccentricity:
0006407
Arg of perigee: 322
5484 deg
Mean anomaly: 37
5234 deg
Mean motion: 15
76164544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2932
Checksum: 300
Coasting Arc #4 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2009/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1047945
98 A = 6722636
29 meter
Y = 6056288
73 meter E =
0002877
Z = -2727880
28 I = 51
32413
XDOT = -4797
405864 Wp = 10
51857
YDOT = -3143
660047 meter/sec RA = 259
00726 deg
ZDOT = -5134
463982 TA = 200
78839
MA = 200
80009
Ha = 186
822 n
mi
Hp = 181
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3438142
99 X = -1102338
65
Y = 19869713
69 feet Y = 6044265
87 meter
Z = -8949738
46 Z = -2733103
44
XDOT = -15739
520550 XDOT = -4736
953349
YDOT = -10313
845297 feet/sec YDOT = -3196
969437 meter/sec
ZDOT = -16845
354273 ZDOT = -5157
623608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13564216
78 X = -4134373
27
Y = -14908843
80 feet Y = -4544215
59 meter
Z = -8970092
96 Z = -2734084
33
XDOT = 16673
452008 XDOT = 5082
068172
YDOT = -4975
599321 feet/sec YDOT = -1516
562673 meter/sec
ZDOT = -16936
833235 ZDOT = -5162
346770
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 09317
52621560
00016717 00000-0 10270-3 0 9037
2 25544 51
6437 259
6657 0006446 326
7785 33
2974 15
76209778 29489
Satellite: ISS
Catalog Number: 25544
Epoch time: 09317
52621560 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 259
6657 deg
Eccentricity:
0006446
Arg of perigee: 326
7785 deg
Mean anomaly: 33
2974 deg
Mean motion: 15
76209778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 350
Coasting Arc #5 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2009/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4301512
04 A = 6718634
12 meter
Y = 3213803
21 meter E =
0010771
Z = 4037895
80 I = 51
31828
XDOT = -1288
344284 Wp = 41
89298
YDOT = 6556
497262 meter/sec RA = 253
78339 deg
ZDOT = -3832
137203 TA = 87
75997
MA = 87
63665
Ha = 186
866 n
mi
Hp = 181
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14112572
30 X = 4245639
04
Y = 10543973
80 feet Y = 3261592
76 meter
Z = 13247689
64 Z = 4058657
56
XDOT = -4226
851326 XDOT = -1342
948013
YDOT = 21510
817789 feet/sec YDOT = 6541
785025 meter/sec
ZDOT = -12572
628620 ZDOT = -3838
528652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16871486
73 X = -5142429
16
Y = 4849016
01 feet Y = 1477980
08 meter
Z = 13329716
43 Z = 4062897
57
XDOT = -14312
405941 XDOT = -4362
421331
YDOT = -15044
297039 feet/sec YDOT = -4585
501738 meter/sec
ZDOT = -12597
571612 ZDOT = -3839
739827
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 09318
54061903
00016717 00000-0 10270-3 0 9040
2 25544 51
6442 254
4398 0006437 330
3008 29
7790 15
76232979 29642
Satellite: ISS
Catalog Number: 25544
Epoch time: 09318
54061903 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 254
4398 deg
Eccentricity:
0006437
Arg of perigee: 330
3008 deg
Mean anomaly: 29
7790 deg
Mean motion: 15
76232979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 326
Coasting Arc #6 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2009/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1260877
54 A = 6719109
01 meter
Y = -5324998
94 meter E =
0009060
Z = 3888824
83 I = 51
32997
XDOT = 5088
988165 Wp = 65
27450
YDOT = 4153
762981 meter/sec RA = 248
66008 deg
ZDOT = 4034
175362 TA = 342
62208
MA = 342
65307
Ha = 186
908 n
mi
Hp = 180
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4136737
33 X = 1301437
07
Y = -17470468
97 feet Y = -5310672
47 meter
Z = 12758611
66 Z = 3895048
65
XDOT = 16696
155397 XDOT = 5022
563901
YDOT = 13627
831301 feet/sec YDOT = 4210
299458 meter/sec
ZDOT = 13235
483470 ZDOT = 4058
737319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11731325
26 X = 3575707
94
Y = 13567768
70 feet Y = 4135455
90 meter
Z = 12782946
20 Z = 3896242
00
XDOT = -19810
005558 XDOT = -6038
089694
YDOT = 4556
226996 feet/sec YDOT = 1388
737989 meter/sec
ZDOT = 13332
543294 ZDOT = 4063
759196
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 09319
55500385
00016717 00000-0 10270-3 0 9055
2 25544 51
6444 249
2135 0006396 334
0101 26
0741 15
76264966 29809
Satellite: ISS
Catalog Number: 25544
Epoch time: 09319
55500385 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 249
2135 deg
Eccentricity:
0006396
Arg of perigee: 334
0101 deg
Mean anomaly: 26
0741 deg
Mean motion: 15
76264966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 308
Coasting Arc #7 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2009/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4582541
63 A = 6721918
00 meter
Y = -3955569
13 meter E =
0007932
Z = -2913518
46 I = 51
35192
XDOT = 1669
162705 Wp = 12
75003
YDOT = -5613
704397 meter/sec RA = 243
43568 deg
ZDOT = 5006
367910 TA = 313
51990
MA = 313
58578
Ha = 187
003 n
mi
Hp = 180
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15034585
38 X = -4523815
38
Y = -12977589
02 feet Y = -4006485
26 meter
Z = -9558787
59 Z = -2935638
78
XDOT = 5476
255595 XDOT = 1707
491272
YDOT = -18417
665346 feet/sec YDOT = -5594
824879 meter/sec
ZDOT = 16425
091569 ZDOT = 5014
569670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19228514
46 X = 5860851
21
Y = -4800186
32 feet Y = -1463096
79 meter
Z = -9646213
63 Z = -2940165
92
XDOT = 11630
588776 XDOT = 3545
003459
YDOT = 13584
760476 feet/sec YDOT = 4140
634993 meter/sec
ZDOT = 16457
220565 ZDOT = 5016
160828
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 09320
50597361
00016717 00000-0 10270-3 0 9063
2 25544 51
6445 244
3139 0006497 337
5202 22
5677 15
76280507 29956
Satellite: ISS
Catalog Number: 25544
Epoch time: 09320
50597361 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 244
3139 deg
Eccentricity:
0006497
Arg of perigee: 337
5202 deg
Mean anomaly: 22
5677 deg
Mean motion: 15
76280507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 323
Coasting Arc #8 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2009/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1734898
41 A = 6715677
26 meter
Y = 4427471
89 meter E =
0013323
Z = -4753874
95 I = 51
34641
XDOT = -5395
669675 Wp = 42
76184
YDOT = -4857
460675 meter/sec RA = 238
30658 deg
ZDOT = -2549
364459 TA = 202
10582
MA = 202
16333
Ha = 187
165 n
mi
Hp = 180
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5691923
91 X = -1761184
10
Y = 14525826
40 feet Y = 4407924
68 meter
Z = -15596702
60 Z = -4762366
79
XDOT = -17702
328329 XDOT = -5328
566970
YDOT = -15936
550770 feet/sec YDOT = -4917
422817 meter/sec
ZDOT = -8364
056625 ZDOT = -2575
414817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8890043
22 X = -2709685
17
Y = -12779832
70 feet Y = -3895293
01 meter
Z = -15630027
84 Z = -4764032
49
XDOT = 22160
799765 XDOT = 6754
611768
YDOT = -5038
481390 feet/sec YDOT = -1535
729128 meter/sec
ZDOT = -8467
032785 ZDOT = -2580
751593
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 09321
52032354
00016717 00000-0 10270-3 0 9073
2 25544 51
6452 239
0875 0006485 342
2606 17
8338 15
76330564 30110
Satellite: ISS
Catalog Number: 25544
Epoch time: 09321
52032354 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 239
0875 deg
Eccentricity:
0006485
Arg of perigee: 342
2606 deg
Mean anomaly: 17
8338 deg
Mean motion: 15
76330564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 297
Coasting Arc #9 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2009/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4816756
11 A = 6724557
99 meter
Y = 4450115
13 meter E =
0010803
Z = 1477711
19 I = 51
39314
XDOT = -2381
342836 Wp = 92
34483
YDOT = 4506
666184 meter/sec RA = 233
09986 deg
ZDOT = -5773
707266 TA = 71
31705
MA = 71
19982
Ha = 187
253 n
mi
Hp = 180
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15803005
61 X = 4759457
52
Y = 14600115
26 feet Y = 4503658
42 meter
Z = 4848133
82 Z = 1500972
85
XDOT = -7812
804581 XDOT = -2403
511847
YDOT = 14785
650210 feet/sec YDOT = 4479
913238 meter/sec
ZDOT = -18942
609142 ZDOT = -5785
329514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20845798
92 X = -6353799
51
Y = 5239352
73 feet Y = 1596954
71 meter
Z = 4940101
60 Z = 1505742
97
XDOT = -7796
402074 XDOT = -2376
343352
YDOT = -13006
962792 feet/sec YDOT = -3964
522259 meter/sec
ZDOT = -18988
286632 ZDOT = -5787
629766
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 09322
53465555
00016717 00000-0 10270-3 0 9089
2 25544 51
6449 233
8611 0006450 345
5414 14
5565 15
76332776 30271
Satellite: ISS
Catalog Number: 25544
Epoch time: 09322
53465555 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 233
8611 deg
Eccentricity:
0006450
Arg of perigee: 345
5414 deg
Mean anomaly: 14
5565 deg
Mean motion: 15
76332776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 314
Coasting Arc #10 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2009/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2485918
03 A = 6713489
72 meter
Y = -3443910
45 meter E =
0004925
Z = 5197260
96 I = 51
37517
XDOT = 5592
381659 Wp = 17
83992
YDOT = 5242
005195 meter/sec RA = 227
94969 deg
ZDOT = 803
074945 TA = 64
52080
MA = 64
46986
Ha = 187
154 n
mi
Hp = 180
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8155899
05 X = 2498995
80
Y = -11298918
79 feet Y = -3416038
88 meter
Z = 17051381
09 Z = 5209369
20
XDOT = 18347
708856 XDOT = 5529
447726
YDOT = 17198
179773 feet/sec YDOT = 5304
190535 meter/sec
ZDOT = 2634
760319 ZDOT = 830
090997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5285831
05 X = 1611121
30
Y = 12830324
43 feet Y = 3910682
89 meter
Z = 17099023
87 Z = 5211782
48
XDOT = -23377
198620 XDOT = -7125
370139
YDOT = 5996
493088 feet/sec YDOT = 1827
731093 meter/sec
ZDOT = 2741
589105 ZDOT = 835
636359
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 09323
54896797
00016717 00000-0 10270-3 0 9098
2 25544 51
6447 228
6345 0006486 348
2987 11
8025 15
76398908 30437
Satellite: ISS
Catalog Number: 25544
Epoch time: 09323
54896797 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 228
6345 deg
Eccentricity:
0006486
Arg of perigee: 348
2987 deg
Mean anomaly: 11
8025 deg
Mean motion: 15
76398908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 359
Coasting Arc #11 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2009/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4875988
57 A = 6725397
76 meter
Y = -4616068
76 meter E =
0017191
Z = 96758
49 I = 51
43638
XDOT = 3372
223884 Wp = 28
26583
YDOT = -3426
953303 meter/sec RA = 222
77319 deg
ZDOT = 6027
739469 TA = 332
79007
MA = 332
88004
Ha = 187
387 n
mi
Hp = 180
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15997337
82 X = -4824478
53
Y = -15144582
53 feet Y = -4670306
94 meter
Z = 317449
11 Z = 73195
17
XDOT = 11063
726655 XDOT = 3381
011878
YDOT = -11243
285114 feet/sec YDOT = -3389
194603 meter/sec
ZDOT = 19776
048128 ZDOT = 6044
143000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21235273
85 X = 6472511
47
Y = -5864028
01 feet Y = -1787355
74 meter
Z = 224257
53 Z = 68353
69
XDOT = 3535
255995 XDOT = 1077
546027
YDOT = 13635
502489 feet/sec YDOT = 4156
101159 meter/sec
ZDOT = 19840
648089 ZDOT = 6047
429538
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 09324
56326551
00016717 00000-0 10270-3 0 9109
2 25544 51
6448 223
4075 0006605 352
7351 7
3717 15
76387616 30598
Satellite: ISS
Catalog Number: 25544
Epoch time: 09324
56326551 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 223
4075 deg
Eccentricity:
0006605
Arg of perigee: 352
7351 deg
Mean anomaly: 7
3717 deg
Mean motion: 15
76387616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 311
Coasting Arc #12 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2009/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3443215
94 A = 6713505
09 meter
Y = 2559198
32 meter E =
0014682
Z = -5175220
69 I = 51
41991
XDOT = -5493
906282 Wp = 72
08868
YDOT = -5285
552408 meter/sec RA = 217
59474 deg
ZDOT = 1048
365826 TA = 207
90803
MA = 207
98686
Ha = 187
412 n
mi
Hp = 179
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11296640
21 X = -3446436
79
Y = 8396319
93 feet Y = 2520676
73 meter
Z = -16979070
50 Z = -5191955
65
XDOT = -18024
626909 XDOT = -5439
486832
YDOT = -17341
051208 feet/sec YDOT = -5346
684333 meter/sec
ZDOT = 3439
520426 ZDOT = 1021
807732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1636488
15 X = -498801
59
Y = -13899291
00 feet Y = -4236503
90 meter
Z = -17045020
38 Z = -5195322
21
XDOT = 23044
337114 XDOT = 7023
913952
YDOT = -6774
781303 feet/sec YDOT = -2064
953341 meter/sec
ZDOT = 3334
464819 ZDOT = 1016
344877
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 09325
51415137
00016717 00000-0 10270-3 0 9115
2 25544 51
6450 218
5073 0006589 356
0012 4
1098 15
76435064 30741
Satellite: ISS
Catalog Number: 25544
Epoch time: 09325
51415137 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 218
5073 deg
Eccentricity:
0006589
Arg of perigee: 356
0012 deg
Mean anomaly: 4
1098 deg
Mean motion: 15
76435064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 290
Coasting Arc #13 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622012
86 A = 6724029
05 meter
Y = 4569381
66 meter E =
0004576
Z = -1728218
88 I = 51
47974
XDOT = -4561
160491 Wp = 85
76599
YDOT = 2466
595281 meter/sec RA = 212
45208 deg
ZDOT = -5689
483440 TA = 113
40868
MA = 113
36055
Ha = 187
513 n
mi
Hp = 179
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15164084
20 X = 4578969
20
Y = 14991409
66 feet Y = 4620827
21 meter
Z = -5670009
45 Z = -1705869
04
XDOT = -14964
437306 XDOT = -4560
764567
YDOT = 8092
504203 feet/sec YDOT = 2415
592377 meter/sec
ZDOT = -18666
284251 ZDOT = -5711
640670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20496356
05 X = -6247289
32
Y = 5965413
28 feet Y = 1818257
97 meter
Z = -5581581
61 Z = -1701266
07
XDOT = 607
463680 XDOT = 185
154930
YDOT = -15420
585067 feet/sec YDOT = -4700
194328 meter/sec
ZDOT = -18753
648791 ZDOT = -5716
112151
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 09326
52841398
00016717 00000-0 10270-3 0 9120
2 25544 51
6449 213
2801 0006475 358
7969 1
3179 15
76420739 30904
Satellite: ISS
Catalog Number: 25544
Epoch time: 09326
52841398 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 213
2801 deg
Eccentricity:
0006475
Arg of perigee: 358
7969 deg
Mean anomaly: 1
3179 deg
Mean motion: 15
76420739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 328
Coasting Arc #14 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2009/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4520345
27 A = 6715581
25 meter
Y = -1811272
50 meter E =
0012743
Z = 4622691
48 I = 51
47836
XDOT = 4991
070901 Wp = 36
05128
YDOT = 5128
552087 meter/sec RA = 207
24832 deg
ZDOT = -2856
956997 TA = 82
30890
MA = 82
16421
Ha = 187
438 n
mi
Hp = 179
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14830529
10 X = 4517806
79
Y = -5942495
08 feet Y = -1760737
84 meter
Z = 15166310
65 Z = 4644645
31
XDOT = 16374
904530 XDOT = 4947
230337
YDOT = 16825
958291 feet/sec YDOT = 5184
120253 meter/sec
ZDOT = -9373
218495 ZDOT = -2832
816218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1723043
19 X = -525183
57
Y = 15800466
76 feet Y = 4815982
27 meter
Z = 15252907
66 Z = 4649086
26
XDOT = -21437
554429 XDOT = -6534
166590
YDOT = 6662
903337 feet/sec YDOT = 2030
852937 meter/sec
ZDOT = -9277
682508 ZDOT = -2827
837628
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 09327
54265739
00016717 00000-0 10270-3 0 9133
2 25544 51
6449 208
0525 0006731 2
2262 357
8931 15
76519810 31063
Satellite: ISS
Catalog Number: 25544
Epoch time: 09327
54265739 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 208
0525 deg
Eccentricity:
0006731
Arg of perigee: 2
2262 deg
Mean anomaly: 357
8931 deg
Mean motion: 15
76519810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3106
Checksum: 310
Coasting Arc #15 (Orbit 3121)
---------------------------------------
Vector Time (GMT): 2009/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 716700
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3983553
98 A = 6720738
07 meter
Y = -4357718
62 meter E =
0015670
Z = 3190737
21 I = 51
52231
XDOT = 5777
836622 Wp = 61
55604
YDOT = -1763
778873 meter/sec RA = 202
13055 deg
ZDOT = 4794
228813 TA = 335
83985
MA = 335
91326
Ha = 187
752 n
mi
Hp = 179
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13069402
83 X = -3950029
38
Y = -14296977
09 feet Y = -4402077
79 meter
Z = 10468297
92 Z = 3171466
03
XDOT = 18956
156897 XDOT = 5773
840267
YDOT = -5786
676094 feet/sec YDOT = -1699
190297 meter/sec
ZDOT = 15729
097156 ZDOT = 4822
288126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18716886
69 X = 5704907
06
Y = -5146100
63 feet Y = -1568531
47 meter
Z = 10392011
67 Z = 3167485
16
XDOT = -3848
612204 XDOT = -1173
057000
YDOT = 18058
382635 feet/sec YDOT = 5504
195027 meter/sec
ZDOT = 15839
810234 ZDOT = 4827
974159
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 09328
55688730
00016717 00000-0 10270-3 0 9146
2 25544 51
6447 202
8246 0006778 6
7262 353
3992 15
76483464 31224
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328
55688730 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 202
8246 deg
Eccentricity:
0006778
Arg of perigee: 6
7262 deg
Mean anomaly: 353
3992 deg
Mean motion: 15
76483464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3122
Checksum: 334
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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