Date:
January 25th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10494 81 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 1828)
---------------------------------------
Vector Time (GMT): 2011/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5262783
07 A = 6732550
96 meter
Y = 2408901
69 meter E =
0003773
Z = -3437683
92 I = 51
66219
XDOT = -4782
766571 Wp = 147
38852
YDOT = 3916
617204 meter/sec RA = 176
57952 deg
ZDOT = -4582
919723 TA = 73
23228
MA = 73
19088
Ha = 192
614 n
mi
Hp = 187
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17266348
65 X = 5252154
49
Y = 7903220
77 feet Y = 2467693
89 meter
Z = -11278490
54 Z = -3412143
58
XDOT = -15691
491376 XDOT = -4803
944855
YDOT = 12849
793978 feet/sec YDOT = 3863
015019 meter/sec
ZDOT = -15035
825864 ZDOT = -4606
205422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2707055
61 X = 825110
55
Y = 18856584
24 feet Y = 5747486
88 meter
Z = -11175559
21 Z = -3406310
45
XDOT = -17863
977910 XDOT = -5444
940467
YDOT = -6391
558326 feet/sec YDOT = -1948
146978 meter/sec
ZDOT = -15129
726739 ZDOT = -4611
540710
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
52471349
00016717 00000-0 10270-3 0 9000
2 25544 51
6415 177
4800 0004328 221
5344 138
5490 15
72100803 18296
Satellite: ISS
Catalog Number: 25544
Epoch time: 11024
52471349 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 177
4800 deg
Eccentricity:
0004328
Arg of perigee: 221
5344 deg
Mean anomaly: 138
5490 deg
Mean motion: 15
72100803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1829
Checksum: 280
Coasting Arc #2 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2011/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3198856
08 A = 6729218
88 meter
Y = -3981304
37 meter E =
0005699
Z = 4376828
16 I = 51
68122
XDOT = 6714
258824 Wp = 89
00153
YDOT = 1682
027838 meter/sec RA = 171
41133 deg
ZDOT = -3373
305431 TA = 34
96126
MA = 34
92385
Ha = 192
422 n
mi
Hp = 187
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10494934
64 X = 3221876
49
Y = -13062022
20 feet Y = -3945404
19 meter
Z = 14359672
45 Z = 4392423
83
XDOT = 22028
408215 XDOT = 6711
337725
YDOT = 5518
464034 feet/sec YDOT = 1757
094458 meter/sec
ZDOT = -11067
275037 ZDOT = -3340
695099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16641046
26 X = 5072190
90
Y = 1423009
02 feet Y = 433733
15 meter
Z = 14422582
80 Z = 4396003
24
XDOT = 7758
616689 XDOT = 2364
826367
YDOT = 20234
120608 feet/sec YDOT = 6167
359961 meter/sec
ZDOT = -10935
827331 ZDOT = -3333
240170
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
54177165
00016717 00000-0 10270-3 0 9013
2 25544 51
6412 172
2715 0004370 224
3979 135
6833 15
72091577 18457
Satellite: ISS
Catalog Number: 25544
Epoch time: 11025
54177165 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 172
2715 deg
Eccentricity:
0004370
Arg of perigee: 224
3979 deg
Mean anomaly: 135
6833 deg
Mean motion: 15
72091577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 304
Coasting Arc #3 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2011/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6261759
32 A = 6734886
26 meter
Y = -449706
15 meter E =
0010091
Z = 2428568
59 I = 51
73201
XDOT = 2443
293950 Wp = 85
11995
YDOT = -4949
210596 meter/sec RA = 166
33996 deg
ZDOT = 5365
065472 TA = 302
23703
MA = 302
33480
Ha = 192
236 n
mi
Hp = 187
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20543829
80 X = -6268062
63
Y = -1475413
89 feet Y = -519764
26 meter
Z = 7967744
72 Z = 2398134
04
XDOT = 8016
056266 XDOT = 2472
393189
YDOT = -16237
567571 feet/sec YDOT = -4921
725704 meter/sec
ZDOT = 17601
920840 ZDOT = 5377
005336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10493918
21 X = -3198546
27
Y = -17777617
97 feet Y = -5418617
96 meter
Z = 7845044
61 Z = 2391169
60
XDOT = 16558
518115 XDOT = 5047
036321
YDOT = -1958
759100 feet/sec YDOT = -597
029774 meter/sec
ZDOT = 17650
111566 ZDOT = 5379
754005
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
55880759
00016717 00000-0 10270-3 0 9026
2 25544 51
6423 167
0633 0004423 229
0399 131
0381 15
72179276 18616
Satellite: ISS
Catalog Number: 25544
Epoch time: 11026
55880759 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 167
0633 deg
Eccentricity:
0004423
Arg of perigee: 229
0399 deg
Mean anomaly: 131
0381 deg
Mean motion: 15
72179276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 306
Coasting Arc #4 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2011/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1033774
82 A = 6726768
19 meter
Y = 4463895
72 meter E =
0010591
Z = -4934327
90 I = 51
73439
XDOT = -7345
339453 Wp = 124
56640
YDOT = 696
800951 meter/sec RA = 161
18808 deg
ZDOT = 2166
665254 TA = 166
47783
MA = 166
44943
Ha = 192
046 n
mi
Hp = 187
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3391649
66 X = -1059644
37
Y = 14645327
16 feet Y = 4452191
06 meter
Z = -16188739
83 Z = -4939412
49
XDOT = -24098
882720 XDOT = -7363
110408
YDOT = 2286
092359 feet/sec YDOT = 614
561446 meter/sec
ZDOT = 7108
481805 ZDOT = 2130
938977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13821984
21 X = -4212940
79
Y = 5854549
83 feet Y = 1784466
79 meter
Z = -16209293
35 Z = -4940592
61
XDOT = -15496
593046 XDOT = -4723
361561
YDOT = -17280
099852 feet/sec YDOT = -5266
974435 meter/sec
ZDOT = 6964
417325 ZDOT = 2122
754401
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
51226412
00016717 00000-0 10270-3 0 9034
2 25544 51
6423 162
1814 0004270 233
7910 126
2857 15
72186825 18762
Satellite: ISS
Catalog Number: 25544
Epoch time: 11027
51226412 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 162
1814 deg
Eccentricity:
0004270
Arg of perigee: 233
7910 deg
Mean anomaly: 126
2857 deg
Mean motion: 15
72186825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 290
Coasting Arc #5 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2011/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6380388
63 A = 6736504
58 meter
Y = -1664854
86 meter E =
0009434
Z = -1349845
18 I = 51
79589
XDOT = 71
410893 Wp = 169
36162
YDOT = 5004
259552 meter/sec RA = 156
10423 deg
ZDOT = -5850
082609 TA = 25
42451
MA = 25
37813
Ha = 191
924 n
mi
Hp = 187
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20933033
55 X = 6405088
33
Y = -5462122
23 feet Y = -1593367
30 meter
Z = -4428625
92 Z = -1318789
91
XDOT = 234
287707 XDOT = 43
865160
YDOT = 16418
174382 feet/sec YDOT = 5004
904509 meter/sec
ZDOT = -19193
184414 ZDOT = -5849
802254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16886682
45 X = 5147060
81
Y = 13563199
71 feet Y = 4134063
27 meter
Z = -4303367
29 Z = -1311666
35
XDOT = -11979
327017 XDOT = -3651
298875
YDOT = 8842
019711 feet/sec YDOT = 2695
047608 meter/sec
ZDOT = -19192
115765 ZDOT = -5849
756885
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
52926411
00016717 00000-0 10270-3 0 9043
2 25544 51
6423 156
9719 0004206 239
0228 121
0521 15
72218357 18922
Satellite: ISS
Catalog Number: 25544
Epoch time: 11028
52926411 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 156
9719 deg
Eccentricity:
0004206
Arg of perigee: 239
0228 deg
Mean anomaly: 121
0521 deg
Mean motion: 15
72218357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 289
Coasting Arc #6 (Orbit 1907)
---------------------------------------
Vector Time (GMT): 2011/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1124966
55 A = 6725350
04 meter
Y = -4081406
25 meter E =
0000876
Z = 5226334
15 I = 51
78718
XDOT = 6999
148690 Wp = 263
69121
YDOT = -3076
798112 meter/sec RA = 150
97354 deg
ZDOT = -896
424914 TA = 194
83061
MA = 194
83318
Ha = 191
745 n
mi
Hp = 187
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3690835
14 X = -1104631
92
Y = -13390440
44 feet Y = -4093873
00 meter
Z = 17146765
59 Z = 5220918
27
XDOT = 22963
086253 XDOT = 7037
388409
YDOT = -10094
481995 feet/sec YDOT = -2998
315529 meter/sec
ZDOT = -2941
026620 ZDOT = -862
331142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8292779
61 X = 2527639
22
Y = -11175990
24 feet Y = -3406441
82 meter
Z = 17124975
28 Z = 5219692
46
XDOT = 21205
677962 XDOT = 6463
490643
YDOT = 11440
333605 feet/sec YDOT = 3487
013683 meter/sec
ZDOT = -2803
475977 ZDOT = -854
499478
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
54624493
00016717 00000-0 10270-3 0 9052
2 25544 51
6434 151
7636 0004129 244
5723 115
5012 15
72242440 19081
Satellite: ISS
Catalog Number: 25544
Epoch time: 11029
54624493 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 151
7636 deg
Eccentricity:
0004129
Arg of perigee: 244
5723 deg
Mean anomaly: 115
5012 deg
Mean motion: 15
72242440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1908
Checksum: 287
Coasting Arc #7 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2011/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5665070
91 A = 6737110
40 meter
Y = 3630543
75 meter E =
0008958
Z = 220054
14 I = 51
85378
XDOT = -2396
873361 Wp = 37
69249
YDOT = -4114
041742 meter/sec RA = 145
87376 deg
ZDOT = 6048
237472 TA = 324
68959
MA = 324
74889
Ha = 191
555 n
mi
Hp = 187
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18586190
65 X = -5706316
25
Y = 11911232
78 feet Y = 3566962
88 meter
Z = 721962
41 Z = 192434
03
XDOT = -7863
757747 XDOT = -2380
071694
YDOT = -13497
512278 feet/sec YDOT = -4140
751518 meter/sec
ZDOT = 19843
298792 ZDOT = 6036
634284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20906032
88 X = -6372158
82
Y = -7100018
37 feet Y = -2164085
60 meter
Z = 610497
74 Z = 186079
71
XDOT = 5052
176575 XDOT = 1539
903420
YDOT = -13133
293743 feet/sec YDOT = -4003
027933 meter/sec
ZDOT = 19796
549205 ZDOT = 6033
988198
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
56320591
00016717 00000-0 10270-3 0 9069
2 25544 51
6441 146
5550 0004065 249
2688 110
8038 15
72263380 19247
Satellite: ISS
Catalog Number: 25544
Epoch time: 11030
56320591 = yrday
fracday
Element set: 906
Inclination: 51
6441 deg
RA of node: 146
5550 deg
Eccentricity:
0004065
Arg of perigee: 249
2688 deg
Mean anomaly: 110
8038 deg
Mean motion: 15
72263380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 290
Coasting Arc #8 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2011/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2947276
51 A = 6724992
86 meter
Y = 2953622
65 meter E =
0010994
Z = -5283394
28 I = 51
83841
XDOT = -5760
042789 Wp = 91
86377
YDOT = 5081
781977 meter/sec RA = 140
76825 deg
ZDOT = -373
269885 TA = 174
60299
MA = 174
59113
Ha = 191
385 n
mi
Hp = 187
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9669542
37 X = 2939694
49
Y = 9690363
02 feet Y = 2986538
79 meter
Z = -17333970
75 Z = -5269095
09
XDOT = -18897
778180 XDOT = -5814
626913
YDOT = 16672
513047 feet/sec YDOT = 5017
064527 meter/sec
ZDOT = -1224
638730 ZDOT = -401
383601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1241704
08 X = -378471
40
Y = 13706076
90 feet Y = 4177612
24 meter
Z = -17276323
51 Z = -5265823
41
XDOT = -23886
430203 XDOT = -7280
583926
YDOT = -3846
480670 feet/sec YDOT = -1172
407308 meter/sec
ZDOT = -1338
130255 ZDOT = -407
862102
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
51658850
00016717 00000-0 10270-3 0 9078
2 25544 51
6445 141
6726 0004101 254
2286 105
8424 15
72303994 19398
Satellite: ISS
Catalog Number: 25544
Epoch time: 11031
51658850 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 141
6726 deg
Eccentricity:
0004101
Arg of perigee: 254
2286 deg
Mean anomaly: 105
8424 deg
Mean motion: 15
72303994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 300
Coasting Arc #9 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2011/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4275358
06 A = 6736630
07 meter
Y = -5125366
56 meter E =
0011335
Z = 862780
21 I = 51
90078
XDOT = 4176
383282 Wp = 141
35449
YDOT = 2471
888063 meter/sec RA = 135
65060 deg
ZDOT = -5977
783467 TA = 29
26976
MA = 29
20630
Ha = 191
339 n
mi
Hp = 187
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14026765
29 X = 4328162
03
Y = -16815507
10 feet Y = -5077261
72 meter
Z = 2830643
72 Z = 883677
25
XDOT = 13702
044887 XDOT = 4177
469797
YDOT = 8109
868972 feet/sec YDOT = 2518
597225 meter/sec
ZDOT = -19612
150481 ZDOT = -5957
492526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21884724
77 X = 6670464
11
Y = -292199
99 feet Y = -89062
56 meter
Z = 2915031
45 Z = 888501
58
XDOT = 2804
802365 XDOT = 854
903761
YDOT = 14175
392387 feet/sec YDOT = 4320
659599 meter/sec
ZDOT = -19530
314317 ZDOT = -5952
839804
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
53351195
00016717 00000-0 10270-3 0 9084
2 25544 51
6446 136
4641 0004045 257
1150 102
9561 15
72317027 19556
Satellite: ISS
Catalog Number: 25544
Epoch time: 11032
53351195 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 136
4641 deg
Eccentricity:
0004045
Arg of perigee: 257
1150 deg
Mean anomaly: 102
9561 deg
Mean motion: 15
72317027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 284
Coasting Arc #10 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2011/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4192295
31 A = 6725552
21 meter
Y = -1262473
01 meter E =
0003397
Z = 5106059
28 I = 51
88593
XDOT = 3883
448794 Wp = 179
80974
YDOT = -6453
561124 meter/sec RA = 130
56718 deg
ZDOT = 1589
509724 TA = 254
95617
MA = 254
99377
Ha = 191
271 n
mi
Hp = 187
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13754249
69 X = -4202669
98
Y = -4141971
82 feet Y = -1309411
90 meter
Z = 16752162
98 Z = 5085668
58
XDOT = 12740
973735 XDOT = 3947
603820
YDOT = -21173
100800 feet/sec YDOT = -6409
775376 meter/sec
ZDOT = 5214
926917 ZDOT = 1608
530570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6089688
81 X = -1856137
15
Y = -13114893
14 feet Y = -3997419
43 meter
Z = 16669899
46 Z = 5080985
35
XDOT = 23318
921249 XDOT = 7107
607197
YDOT = -4087
631035 feet/sec YDOT = -1245
909939 meter/sec
ZDOT = 5291
770842 ZDOT = 1612
931753
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
55041376
00016717 00000-0 10270-3 0 9095
2 25544 51
6454 131
2549 0004050 263
0592 97
0110 15
72389504 19718
Satellite: ISS
Catalog Number: 25544
Epoch time: 11033
55041376 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 131
2549 deg
Eccentricity:
0004050
Arg of perigee: 263
0592 deg
Mean anomaly: 97
0110 deg
Mean motion: 15
72389504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 287
Coasting Arc #11 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2011/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2437973
54 A = 6735277
89 meter
Y = 5982679
52 meter E =
0005524
Z = -1892732
82 I = 51
93740
XDOT = -5204
253487 Wp = 4
22802
YDOT = -331
859233 meter/sec RA = 125
43375 deg
ZDOT = 5660
906372 TA = 334
84976
MA = 334
87666
Ha = 191
154 n
mi
Hp = 187
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7998600
86 X = -2495497
55
Y = 19628213
66 feet Y = 5955094
99 meter
Z = -6209753
33 Z = -1904715
82
XDOT = -17074
322464 XDOT = -5227
654520
YDOT = -1088
777010 feet/sec YDOT = -390
187177 meter/sec
ZDOT = 18572
527467 ZDOT = 5635
568121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19845322
89 X = -6048854
42
Y = 7402943
20 feet Y = 2256417
09 meter
Z = -6258195
80 Z = -1907498
08
XDOT = -10276
208757 XDOT = -3132
188429
YDOT = -11951
318927 feet/sec YDOT = -3642
762009 meter/sec
ZDOT = 18470
278207 ZDOT = 5629
740797
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
50374369
00016717 00000-0 10270-3 0 9104
2 25544 51
6453 126
3723 0004048 270
4530 89
6169 15
72355434 19869
Satellite: ISS
Catalog Number: 25544
Epoch time: 11034
50374369 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 126
3723 deg
Eccentricity:
0004048
Arg of perigee: 270
4530 deg
Mean anomaly: 89
6169 deg
Mean motion: 15
72355434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 307
Coasting Arc #12 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2011/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4722588
52 A = 6727080
22 meter
Y = -706154
63 meter E =
0007624
Z = -4745631
57 I = 51
92614
XDOT = -1660
659215 Wp = 60
13087
YDOT = 7010
072447 meter/sec RA = 120
36948 deg
ZDOT = -2695
202347 TA = 183
43583
MA = 183
44107
Ha = 191
112 n
mi
Hp = 187
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15494056
84 X = 4753186
58
Y = -2316780
27 feet Y = -653172
80 meter
Z = -15569657
40 Z = -4722615
63
XDOT = -5448
357005 XDOT = -1725
831353
YDOT = 22998
925352 feet/sec YDOT = 6991
137502 meter/sec
ZDOT = -8842
527384 ZDOT = -2703
428009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12413741
52 X = 3783708
42
Y = 9706515
15 feet Y = 2958545
82 meter
Z = -15476759
50 Z = -4717316
30
XDOT = -19684
399076 XDOT = -5999
804838
YDOT = 11019
664623 feet/sec YDOT = 3358
793777 meter/sec
ZDOT = -8875
825249 ZDOT = -2705
351536
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
52060911
00016717 00000-0 10270-3 0 9113
2 25544 51
6445 121
1635 0004019 272
7285 87
3418 15
72402366 20024
Satellite: ISS
Catalog Number: 25544
Epoch time: 11035
52060911 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 121
1635 deg
Eccentricity:
0004019
Arg of perigee: 272
7285 deg
Mean anomaly: 87
3418 deg
Mean motion: 15
72402366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 271
Coasting Arc #13 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2011/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 456824
35 A = 6733168
93 meter
Y = -6103235
72 meter E =
0009637
Z = 2796225
17 I = 51
96158
XDOT = 5377
268913 Wp = 100
16917
YDOT = -1962
508910 meter/sec RA = 115
22393 deg
ZDOT = -5148
745482 TA = 47
98543
MA = 47
90342
Ha = 191
120 n
mi
Hp = 187
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1498767
56 X = 511454
77
Y = -20023739
25 feet Y = -6097821
69 meter
Z = 9173967
11 Z = 2798577
26
XDOT = 17641
958375 XDOT = 5423
825368
YDOT = -6438
677525 feet/sec YDOT = -1902
116901 meter/sec
ZDOT = -16892
209585 ZDOT = -5122
510311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15292281
82 X = 4661087
50
Y = -13006406
84 feet Y = -3964352
81 meter
Z = 9183550
94 Z = 2799146
33
XDOT = 16081
248796 XDOT = 4901
564633
YDOT = 7024
397298 feet/sec YDOT = 2141
036296 meter/sec
ZDOT = -16786
295494 ZDOT = -5116
462867
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 11036
53745470
00016717 00000-0 10270-3 0 9126
2 25544 51
6444 115
9543 0003887 279
5562 80
5161 15
72457972 20187
Satellite: ISS
Catalog Number: 25544
Epoch time: 11036
53745470 = yrday
fracday
Element set: 912
Inclination: 51
6444 deg
RA of node: 115
9543 deg
Eccentricity:
0003887
Arg of perigee: 279
5562 deg
Mean anomaly: 80
5161 deg
Mean motion: 15
72457972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2018
Checksum: 317
Coasting Arc #14 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2011/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4500573
55 A = 6728848
63 meter
Y = 2688743
91 meter E =
0006255
Z = 4214322
04 I = 51
95899
XDOT = -583
887290 Wp = 107
84845
YDOT = -6742
229233 meter/sec RA = 110
17033 deg
ZDOT = 3671
700767 TA = 304
85631
MA = 304
91511
Ha = 191
205 n
mi
Hp = 187
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14765661
25 X = -4550777
00
Y = 8821338
30 feet Y = 2638135
25 meter
Z = 13826515
89 Z = 4192336
75
XDOT = -1915
640716 XDOT = -526
287028
YDOT = -22120
174648 feet/sec YDOT = -6748
436400 meter/sec
ZDOT = 12046
262358 ZDOT = 3669
004502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16773096
11 X = -5112439
70
Y = -4117171
01 feet Y = -1254913
72 meter
Z = 13737738
27 Z = 4187262
62
XDOT = 13788
410806 XDOT = 4202
707614
YDOT = -15944
925498 feet/sec YDOT = -4860
013292 meter/sec
ZDOT = 12035
485565 ZDOT = 3668
416000
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 11037
55427972
00016717 00000-0 10270-3 0 9134
2 25544 51
6441 110
7442 0003961 283
1130 76
9590 15
72494992 20346
Satellite: ISS
Catalog Number: 25544
Epoch time: 11037
55427972 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 110
7442 deg
Eccentricity:
0003961
Arg of perigee: 283
1130 deg
Mean anomaly: 76
9590 deg
Mean motion: 15
72494992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 304
Coasting Arc #15 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2011/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 814270
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1422975
84 A = 6730810
38 meter
Y = 5516359
10 meter E =
0001779
Z = -3585530
47 I = 51
97450
XDOT = -4721
506328 Wp = 74
38362
YDOT = 4119
477107 meter/sec RA = 105
01925 deg
ZDOT = 4466
324184 TA = 243
06959
MA = 243
08777
Ha = 191
183 n
mi
Hp = 187
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4668555
92 X = 1378602
61
Y = 18098291
00 feet Y = 5532023
42 meter
Z = -11763551
42 Z = -3578725
82
XDOT = -15490
506324 XDOT = -4788
916321
YDOT = 13515
344838 feet/sec YDOT = 4066
301649 meter/sec
ZDOT = 14653
294567 ZDOT = 4443
223685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9026736
65 X = -2751349
33
Y = 16386116
91 feet Y = 4994488
43 meter
Z = -11736178
76 Z = -3577187
29
XDOT = -19408
188228 XDOT = -5915
615772
YDOT = -268
668868 feet/sec YDOT = -81
890271 meter/sec
ZDOT = 14559
986106 ZDOT = 4437
883765
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 11038
50753706
00016717 00000-0 10270-3 0 9148
2 25544 51
6431 105
8605 0003829 288
6136 71
4610 15
72529031 20492
Satellite: ISS
Catalog Number: 25544
Epoch time: 11038
50753706 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 105
8605 deg
Eccentricity:
0003829
Arg of perigee: 288
6136 deg
Mean anomaly: 71
4610 deg
Mean motion: 15
72529031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 294
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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