Date:
January 25th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 1786)
---------------------------------------
Vector Time (GMT): 2011/021/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3503833
70 A = 6727950
13 meter
Y = 3217159
26 meter E =
0011300
Z = -4768365
56 I = 51
56648
XDOT = -6481
338295 Wp = 130
12649
YDOT = -3236
121351 meter/sec RA = 190
14261 deg
ZDOT = 2576
031774 TA = 165
21262
MA = 165
17954
Ha = 192
921 n
mi
Hp = 187
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11495517
37 X = -3516384
98
Y = 10554984
46 feet Y = 3177907
22 meter
Z = -15644243
95 Z = -4785417
10
XDOT = -21264
233251 XDOT = -6457
183204
YDOT = -10617
196033 feet/sec YDOT = -3308
464591 meter/sec
ZDOT = 8451
547815 ZDOT = 2544
604942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4399539
37 X = 1340979
60
Y = 14901099
40 feet Y = 4541855
10 meter
Z = -15712997
02 Z = -4789321
49
XDOT = -17885
075352 XDOT = -5451
370967
YDOT = 14069
873890 feet/sec YDOT = 4288
497562 meter/sec
ZDOT = 8324
926695 ZDOT = 2537
437657
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 11021
85484354
00016717 00000-0 10270-3 0 9003
2 25544 51
6429 191
1521 0004322 213
6913 146
3975 15
71997732 17874
Satellite: ISS
Catalog Number: 25544
Epoch time: 11021
85484354 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 191
1521 deg
Eccentricity:
0004322
Arg of perigee: 213
6913 deg
Mean anomaly: 146
3975 deg
Mean motion: 15
71997732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1787
Checksum: 311
Coasting Arc #2 (Orbit 1802)
---------------------------------------
Vector Time (GMT): 2011/022/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6241932
21 A = 6736601
31 meter
Y = 1882257
48 meter E =
0009935
Z = -1673349
58 I = 51
62687
XDOT = -2827
484432 Wp = 167
24651
YDOT = 4300
939137 meter/sec RA = 185
05450 deg
ZDOT = -5725
145193 TA = 31
24162
MA = 31
18261
Ha = 192
823 n
mi
Hp = 187
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20478780
23 X = 6228549
17
Y = 6175385
43 feet Y = 1951983
71 meter
Z = -5489992
07 Z = -1643059
54
XDOT = -9276
523728 XDOT = -2847
557182
YDOT = 14110
692707 feet/sec YDOT = 4269
208295 meter/sec
ZDOT = -18783
284755 ZDOT = -5738
929499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14363579
78 X = 4378019
12
Y = -15891154
22 feet Y = -4843623
81 meter
Z = -5367926
18 Z = -1636143
90
XDOT = 7667
719326 XDOT = 2337
120850
YDOT = 13276
220660 feet/sec YDOT = 4046
592057 meter/sec
ZDOT = -18838
882700 ZDOT = -5742
091447
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 11022
87195576
00016717 00000-0 10270-3 0 9012
2 25544 51
6437 185
9443 0004249 216
9505 143
1365 15
72038742 18033
Satellite: ISS
Catalog Number: 25544
Epoch time: 11022
87195576 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 185
9443 deg
Eccentricity:
0004249
Arg of perigee: 216
9505 deg
Mean anomaly: 143
1365 deg
Mean motion: 15
72038742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1803
Checksum: 309
Coasting Arc #3 (Orbit 1818)
---------------------------------------
Vector Time (GMT): 2011/023/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1342452
60 A = 6726053
04 meter
Y = -4092911
20 meter E =
0001064
Z = 5165212
08 I = 51
62145
XDOT = 7543
673589 Wp = 150
90614
YDOT = 946
993568 meter/sec RA = 179
90793 deg
ZDOT = -1211
032857 TA = 310
66483
MA = 310
67407
Ha = 192
584 n
mi
Hp = 187
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4404372
05 X = 1363029
38
Y = -13428186
35 feet Y = -4077784
03 meter
Z = 16946233
87 Z = 5171783
57
XDOT = 24749
585267 XDOT = 7538
406325
YDOT = 3106
934277 feet/sec YDOT = 1031
322029 meter/sec
ZDOT = -3973
204910 ZDOT = -1174
399241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10455703
22 X = -3186898
34
Y = -9460086
12 feet Y = -2883434
25 meter
Z = 16972759
50 Z = 5173297
09
XDOT = 12361
650035 XDOT = 3767
830931
YDOT = -20521
475247 feet/sec YDOT = -6254
945655 meter/sec
ZDOT = -3825
550545 ZDOT = -1166
027806
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 11023
88905266
00016717 00000-0 10270-3 0 9020
2 25544 51
6429 180
7367 0004172 221
1265 138
9583 15
72068749 18199
Satellite: ISS
Catalog Number: 25544
Epoch time: 11023
88905266 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 180
7367 deg
Eccentricity:
0004172
Arg of perigee: 221
1265 deg
Mean anomaly: 138
9583 deg
Mean motion: 15
72068749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1819
Checksum: 323
Coasting Arc #4 (Orbit 1834)
---------------------------------------
Vector Time (GMT): 2011/024/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6713978
18 A = 6737608
81 meter
Y = 262244
06 meter E =
0008923
Z = 439272
51 I = 51
69135
XDOT = 211
485858 Wp = 50
92712
YDOT = -4793
037133 meter/sec RA = 174
80270 deg
ZDOT = 6017
960271 TA = 313
84188
MA = 313
91560
Ha = 192
446 n
mi
Hp = 187
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22027487
47 X = -6718545
52
Y = 860380
78 feet Y = 187138
76 meter
Z = 1441182
78 Z = 406645
45
XDOT = 693
851241 XDOT = 235
833099
YDOT = -15725
187443 feet/sec YDOT = -4790
536077 meter/sec
ZDOT = 19743
964145 ZDOT = 6019
046759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7955736
09 X = -2424908
36
Y = 20567414
28 feet Y = 6268947
87 meter
Z = 1309656
49 Z = 399183
30
XDOT = -12704
558902 XDOT = -3872
349553
YDOT = -6189
232572 feet/sec YDOT = -1886
478088 meter/sec
ZDOT = 19748
388462 ZDOT = 6019
308803
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 11024
90613564
00016717 00000-0 10270-3 0 9032
2 25544 51
6434 175
5288 0004039 226
6096 133
4730 15
72069374 18350
Satellite: ISS
Catalog Number: 25544
Epoch time: 11024
90613564 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 175
5288 deg
Eccentricity:
0004039
Arg of perigee: 226
6096 deg
Mean anomaly: 133
4730 deg
Mean motion: 15
72069374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 306
Coasting Arc #5 (Orbit 1849)
---------------------------------------
Vector Time (GMT): 2011/025/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 954903
60 A = 6725576
29 meter
Y = 4067661
92 meter E =
0012008
Z = -5280321
58 I = 51
68151
XDOT = -7534
370526 Wp = 100
65390
YDOT = 1524
636546 meter/sec RA = 169
68288 deg
ZDOT = -190
577456 TA = 167
55071
MA = 167
52102
Ha = 192
295 n
mi
Hp = 187
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3132885
83 X = 934997
76
Y = 13345347
52 feet Y = 4078229
06 meter
Z = -17323889
70 Z = -5275730
98
XDOT = -24719
063405 XDOT = -7549
933549
YDOT = 5002
088407 feet/sec YDOT = 1440
295653 meter/sec
ZDOT = -625
254120 ZDOT = -227
216691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13571057
99 X = 4136458
47
Y = 2092639
50 feet Y = 637836
52 meter
Z = -17305423
24 Z = -5274693
00
XDOT = -4639
844533 XDOT = -1414
224614
YDOT = 23766
774450 feet/sec YDOT = 7244
112852 meter/sec
ZDOT = -772
980013 ZDOT = -235
604308
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 11025
85963544
00016717 00000-0 10270-3 0 9044
2 25544 51
6436 170
6463 0004121 230
7560 129
3237 15
72087164 18507
Satellite: ISS
Catalog Number: 25544
Epoch time: 11025
85963544 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 170
6463 deg
Eccentricity:
0004121
Arg of perigee: 230
7560 deg
Mean anomaly: 129
3237 deg
Mean motion: 15
72087164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1850
Checksum: 295
Coasting Arc #6 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2011/026/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6256758
12 A = 6737242
61 meter
Y = -2356074
45 meter E =
0012868
Z = 767482
53 I = 51
74962
XDOT = 2338
178462 Wp = 143
84497
YDOT = 4247
200625 meter/sec RA = 164
55768 deg
ZDOT = -5982
712486 TA = 27
80478
MA = 27
73606
Ha = 192
155 n
mi
Hp = 187
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20527421
66 X = 6278910
93
Y = -7729903
05 feet Y = -2285983
77 meter
Z = 2517987
29 Z = 797931
16
XDOT = 7671
189179 XDOT = 2319
574235
YDOT = 13934
385253 feet/sec YDOT = 4273
243791 meter/sec
ZDOT = -19628
321804 ZDOT = -5971
398767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 292075
58 X = 89024
64
Y = -21918204
27 feet Y = -6680668
66 meter
Z = 2640779
13 Z = 804909
48
XDOT = 14216
837387 XDOT = 4333
292036
YDOT = -2185
204313 feet/sec YDOT = -666
050275 meter/sec
ZDOT = -19582
751893 ZDOT = -5968
822777
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 11026
87668765
00016717 00000-0 10270-3 0 9055
2 25544 51
6422 165
4379 0003940 234
3077 125
7719 15
72124133 18661
Satellite: ISS
Catalog Number: 25544
Epoch time: 11026
87668765 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 165
4379 deg
Eccentricity:
0003940
Arg of perigee: 234
3077 deg
Mean anomaly: 125
7719 deg
Mean motion: 15
72124133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 320
Coasting Arc #7 (Orbit 1881)
---------------------------------------
Vector Time (GMT): 2011/027/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3037442
82 A = 6726243
09 meter
Y = -3159414
56 meter E =
0004871
Z = 5102982
63 I = 51
74108
XDOT = 6534
323617 Wp = 172
95341
YDOT = -3759
041579 meter/sec RA = 159
46423 deg
ZDOT = 1557
183602 TA = 262
08953
MA = 262
14482
Ha = 192
076 n
mi
Hp = 187
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9965363
59 X = -3026676
89
Y = -10365533
33 feet Y = -3193321
20 meter
Z = 16742069
00 Z = 5088252
91
XDOT = 21438
069611 XDOT = 6568
307881
YDOT = -12332
813578 feet/sec YDOT = -3685
780909 meter/sec
ZDOT = 5108
870086 ZDOT = 1589
009180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13225886
54 X = -4031250
22
Y = 5814871
63 feet Y = 1772372
87 meter
Z = 16682710
22 Z = 5084890
07
XDOT = -3661
933341 XDOT = -1116
157282
YDOT = -23400
811878 feet/sec YDOT = -7132
567460 meter/sec
ZDOT = 5237
247925 ZDOT = 1596
313167
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 11027
89372390
00016717 00000-0 10270-3 0 9065
2 25544 51
6415 160
2291 0003911 240
1507 119
9267 15
72142246 18826
Satellite: ISS
Catalog Number: 25544
Epoch time: 11027
89372390 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 160
2291 deg
Eccentricity:
0003911
Arg of perigee: 240
1507 deg
Mean anomaly: 119
9267 deg
Mean motion: 15
72142246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1882
Checksum: 295
Coasting Arc #8 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2011/028/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4993812
38 A = 6735634
86 meter
Y = 4084663
30 meter E =
0003718
Z = -1928449
53 I = 51
80203
XDOT = -4446
141617 Wp = 14
82392
YDOT = -2779
559722 meter/sec RA = 154
32234 deg
ZDOT = 5631
987631 TA = 323
80407
MA = 323
82922
Ha = 191
814 n
mi
Hp = 187
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16383898
89 X = -5029748
82
Y = 13401126
31 feet Y = 4028618
68 meter
Z = -6326934
14 Z = -1952796
00
XDOT = -14587
078795 XDOT = -4442
088270
YDOT = -9119
290426 feet/sec YDOT = -2829
256912 meter/sec
ZDOT = 18477
649707 ZDOT = 5610
398321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7196409
31 X = 2193465
56
Y = 19874135
51 feet Y = 6057636
50 meter
Z = -6425173
57 Z = -1958392
91
XDOT = -12041
082059 XDOT = -3670
121812
YDOT = 10299
469234 feet/sec YDOT = 3139
278223 meter/sec
ZDOT = 18390
616616 ZDOT = 5605
459945
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 11028
84718067
00016717 00000-0 10270-3 0 9077
2 25544 51
6419 155
3470 0003850 243
4642 116
6126 15
72200247 18972
Satellite: ISS
Catalog Number: 25544
Epoch time: 11028
84718067 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 155
3470 deg
Eccentricity:
0003850
Arg of perigee: 243
4642 deg
Mean anomaly: 116
6126 deg
Mean motion: 15
72200247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 303
Coasting Arc #9 (Orbit 1912)
---------------------------------------
Vector Time (GMT): 2011/029/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4569730
74 A = 6727923
63 meter
Y = 1572978
80 meter E =
0006976
Z = -4687292
49 I = 51
80193
XDOT = -4727
552920 Wp = 71
03849
YDOT = 5380
397294 meter/sec RA = 149
25037 deg
ZDOT = -2804
571372 TA = 171
32447
MA = 171
31241
Ha = 191
725 n
mi
Hp = 188
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14992554
94 X = 4574571
25
Y = 5160691
60 feet Y = 1624107
71 meter
Z = -15378256
21 Z = -4665081
38
XDOT = -15510
344225 XDOT = -4773
742395
YDOT = 17652
222093 feet/sec YDOT = 5327
272896 meter/sec
ZDOT = -9201
349646 ZDOT = -2827
649071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9669746
07 X = 2947338
60
Y = -12674865
13 feet Y = -3863298
89 meter
Z = -15288688
96 Z = -4659992
40
XDOT = 10927
260740 XDOT = 3330
629073
YDOT = 19543
082208 feet/sec YDOT = 5956
731457 meter/sec
ZDOT = -9294
504823 ZDOT = -2832
965070
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 11029
86418660
00016717 00000-0 10270-3 0 9087
2 25544 51
6410 150
1375 0003873 250
3697 109
7048 15
72188551 19130
Satellite: ISS
Catalog Number: 25544
Epoch time: 11029
86418660 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 150
1375 deg
Eccentricity:
0003873
Arg of perigee: 250
3697 deg
Mean anomaly: 109
7048 deg
Mean motion: 15
72188551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1913
Checksum: 311
Coasting Arc #10 (Orbit 1928)
---------------------------------------
Vector Time (GMT): 2011/030/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3166879
88 A = 6733363
20 meter
Y = -5152510
62 meter E =
0009682
Z = 2948611
49 I = 51
84670
XDOT = 5794
047484 Wp = 105
23515
YDOT = 679
070147 meter/sec RA = 144
09654 deg
ZDOT = -5025
185807 TA = 40
89621
MA = 40
82361
Ha = 191
447 n
mi
Hp = 187
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10390025
86 X = 3209937
44
Y = -16904562
41 feet Y = -5116856
11 meter
Z = 9673922
20 Z = 2964099
99
XDOT = 19009
342140 XDOT = 5810
434128
YDOT = 2227
920429 feet/sec YDOT = 743
954649 meter/sec
ZDOT = -16486
830076 ZDOT = -4996
999263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13022810
91 X = -3969352
77
Y = -14930140
95 feet Y = -4550706
96 meter
Z = 9736473
98 Z = 2967677
27
XDOT = 6771
825909 XDOT = 2064
052537
YDOT = -16607
882474 feet/sec YDOT = -5062
082578 meter/sec
ZDOT = -16373
133960 ZDOT = -4990
531231
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 11030
88117586
00016717 00000-0 10270-3 0 9095
2 25544 51
6411 144
9288 0003924 257
7631 102
3092 15
72241816 19290
Satellite: ISS
Catalog Number: 25544
Epoch time: 11030
88117586 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 144
9288 deg
Eccentricity:
0003924
Arg of perigee: 257
7631 deg
Mean anomaly: 102
3092 deg
Mean motion: 15
72241816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1929
Checksum: 309
Coasting Arc #11 (Orbit 1944)
---------------------------------------
Vector Time (GMT): 2011/031/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5357676
53 A = 6730119
63 meter
Y = 444613
74 meter E =
0007232
Z = 4045195
21 I = 51
86000
XDOT = 2438
896356 Wp = 114
07773
YDOT = -6172
756130 meter/sec RA = 139
03960 deg
ZDOT = 3900
329176 TA = 295
78090
MA = 295
85550
Ha = 191
462 n
mi
Hp = 187
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17577678
91 X = -5381900
30
Y = 1458706
51 feet Y = 384565
31 meter
Z = 13271637
82 Z = 4019109
62
XDOT = 8001
628463 XDOT = 2488
793519
YDOT = -20251
824573 feet/sec YDOT = -6145
204137 meter/sec
ZDOT = 12796
355564 ZDOT = 3912
297826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3610729
52 X = -1100550
36
Y = 17344965
81 feet Y = 5286745
58 meter
Z = 13166388
43 Z = 4013115
19
XDOT = -15905
433130 XDOT = -4847
976018
YDOT = -13082
288127 feet/sec YDOT = -3987
481421 meter/sec
ZDOT = 12844
729337 ZDOT = 3915
073502
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 11031
89814974
00016717 00000-0 10270-3 0 9104
2 25544 51
6412 139
7205 0004026 261
0626 99
0080 15
72268332 19457
Satellite: ISS
Catalog Number: 25544
Epoch time: 11031
89814974 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 139
7205 deg
Eccentricity:
0004026
Arg of perigee: 261
0626 deg
Mean anomaly: 99
0080 deg
Mean motion: 15
72268332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1945
Checksum: 295
Coasting Arc #12 (Orbit 1959)
---------------------------------------
Vector Time (GMT): 2011/032/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1068671
49 A = 6730810
22 meter
Y = 5438049
50 meter E =
0002939
Z = -3823076
75 I = 51
88485
XDOT = -6217
844187 Wp = 129
23247
YDOT = 1723
359536 meter/sec RA = 133
88262 deg
ZDOT = 4189
756552 TA = 184
57074
MA = 184
57342
Ha = 191
408 n
mi
Hp = 187
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3506140
07 X = -1110830
17
Y = 17841369
76 feet Y = 5425863
38 meter
Z = -12542902
73 Z = -3828370
40
XDOT = -20399
751269 XDOT = -6257
005392
YDOT = 5654
066720 feet/sec YDOT = 1653
608741 meter/sec
ZDOT = 13745
920446 ZDOT = 4159
456220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16275291
03 X = 4960708
71
Y = 8073673
34 feet Y = 2460855
64 meter
Z = -12564338
52 Z = -3829610
38
XDOT = 564
897489 XDOT = 172
180755
YDOT = 20060
884568 feet/sec YDOT = 6114
557616 meter/sec
ZDOT = 13623
635064 ZDOT = 4152
483967
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 11032
85154965
00016717 00000-0 10270-3 0 9119
2 25544 51
6414 134
8371 0003837 267
1465 92
9258 15
72246279 19608
Satellite: ISS
Catalog Number: 25544
Epoch time: 11032
85154965 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 134
8371 deg
Eccentricity:
0003837
Arg of perigee: 267
1465 deg
Mean anomaly: 92
9258 deg
Mean motion: 15
72246279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1960
Checksum: 321
Coasting Arc #13 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2011/033/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5318440
52 A = 6732525
60 meter
Y = -2542676
78 meter E =
0000881
Z = -3252134
66 I = 51
91189
XDOT = -41
046914 Wp = 124
31235
YDOT = 6028
166799 meter/sec RA = 128
82913 deg
ZDOT = -4781
641207 TA = 93
54748
MA = 93
53740
Ha = 191
359 n
mi
Hp = 187
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17448951
83 X = 5362275
67
Y = -8342115
42 feet Y = -2482957
63 meter
Z = -10669733
12 Z = -3226192
11
XDOT = -134
668352 XDOT = -85
224405
YDOT = 19777
450128 feet/sec YDOT = 6027
460840 meter/sec
ZDOT = -15687
799237 ZDOT = -4781
947832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3687847
81 X = -1124056
01
Y = -19044168
47 feet Y = -5804662
55 meter
Z = -10565010
19 Z = -3220215
11
XDOT = 17746
787762 XDOT = 5409
220910
YDOT = 5264
563494 feet/sec YDOT = 1604
638953 meter/sec
ZDOT = -15689
121097 ZDOT = -4782
044110
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 11033
86849326
00016717 00000-0 10270-3 0 9124
2 25544 51
6420 129
6280 0003836 272
4446 87
6277 15
72297650 19761
Satellite: ISS
Catalog Number: 25544
Epoch time: 11033
86849326 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 129
6280 deg
Eccentricity:
0003836
Arg of perigee: 272
4446 deg
Mean anomaly: 87
6277 deg
Mean motion: 15
72297650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 329
Coasting Arc #14 (Orbit 1991)
---------------------------------------
Vector Time (GMT): 2011/034/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -955195
88 A = 6728216
26 meter
Y = -4915248
79 meter E =
0005826
Z = 4492483
05 I = 51
91592
XDOT = 5712
730373 Wp = 47
79129
YDOT = -4044
706449 meter/sec RA = 123
67850 deg
ZDOT = -3204
227677 TA = 74
16608
MA = 74
10186
Ha = 191
307 n
mi
Hp = 187
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3133844
76 X = -921984
60
Y = -16126144
31 feet Y = -4925744
64 meter
Z = 14739117
63 Z = 4487923
57
XDOT = 18742
553716 XDOT = 5773
099506
YDOT = -13270
034283 feet/sec YDOT = -3980
485729 meter/sec
ZDOT = -10512
557996 ZDOT = -3176
329491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16431819
23 X = -5008418
50
Y = -639415
89 feet Y = -194893
96 meter
Z = 14720786
87 Z = 4486895
84
XDOT = -8550
365528 XDOT = -2606
151413
YDOT = -20189
134430 feet/sec YDOT = -6153
648174 meter/sec
ZDOT = -10399
913403 ZDOT = -3169
893605
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 11034
88542074
00016717 00000-0 10270-3 0 9138
2 25544 51
6420 124
4195 0003968 277
4092 82
6619 15
72321572 19921
Satellite: ISS
Catalog Number: 25544
Epoch time: 11034
88542074 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 124
4195 deg
Eccentricity:
0003968
Arg of perigee: 277
4092 deg
Mean anomaly: 82
6619 deg
Mean motion: 15
72321572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1992
Checksum: 313
Coasting Arc #15 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2011/035/20:14:23
815
Vector Time (MET): N/A
Weight (LBS) : 829370
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4493652
27 A = 6734537
80 meter
Y = 4435839
12 meter E =
0010628
Z = 2325399
45 I = 51
95381
XDOT = -2121
244314 Wp = 63
08923
YDOT = -5011
845053 meter/sec RA = 118
62017 deg
ZDOT = 5446
998351 TA = 322
94027
MA = 323
01362
Ha = 191
304 n
mi
Hp = 187
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14742953
66 X = -4554216
71
Y = 14553277
97 feet Y = 4385249
81 meter
Z = 7629263
29 Z = 2303422
74
XDOT = -6959
462971 XDOT = -2091
502982
YDOT = -16443
061197 feet/sec YDOT = -5035
399659 meter/sec
ZDOT = 17870
729498 ZDOT = 5436
766029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10995103
77 X = 3351307
63
Y = 17595645
40 feet Y = 5363152
72 meter
Z = 7540503
74 Z = 2298345
54
XDOT = -16301
294104 XDOT = -4968
634443
YDOT = 2525
287590 feet/sec YDOT = 769
707657 meter/sec
ZDOT = 17829
505857 ZDOT = 5434
433385
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 11035
90233162
00016717 00000-0 10270-3 0 9148
2 25544 51
6423 119
2105 0003936 280
0193 80
0525 15
72367346 20080
Satellite: ISS
Catalog Number: 25544
Epoch time: 11035
90233162 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 119
2105 deg
Eccentricity:
0003936
Arg of perigee: 280
0193 deg
Mean anomaly: 80
0525 deg
Mean motion: 15
72367346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 272
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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