Date:
February 23rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
056/10:34:37
211 -1
4 1
5 1
5
N/A -0
0 -0
1 193
5
000/00:03:14
421 0
5 0
1 185
7
Coasting Arc #1 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2011/047/20:06:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4434898
56 A = 6725677
38 meter
Y = -405376
85 meter E =
0009717
Z = -5048153
00 I = 51
91792
XDOT = 2727
818127 Wp = 86
10022
YDOT = 6951
618083 meter/sec RA = 57
43114 deg
ZDOT = 1841
882125 TA = 201
59136
MA = 201
63236
Ha = 192
178 n
mi
Hp = 187
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14550192
12 X = 4463624
13
Y = -1329976
53 feet Y = -355622
65 meter
Z = -16562181
75 Z = -5026539
21
XDOT = 8949
534537 XDOT = 2640
933855
YDOT = 22807
145943 feet/sec YDOT = 6981
636448 meter/sec
ZDOT = 6042
920358 ZDOT = 1854
922196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -617792
74 X = -188303
23
Y = -14696220
41 feet Y = -4479407
98 meter
Z = -16474896
97 Z = -5021548
60
XDOT = 22141
599920 XDOT = 6748
759656
YDOT = -7750
307762 feet/sec YDOT = -2362
293806 meter/sec
ZDOT = 6095
381281 ZDOT = 1857
872215
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 11047
85032831
00016717 00000-0 10270-3 0 9000
2 25544 51
6449 58
0203 0004943 320
3289 39
7511 15
72443627 21961
Satellite: ISS
Catalog Number: 25544
Epoch time: 11047
85032831 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 58
0203 deg
Eccentricity:
0004943
Arg of perigee: 320
3289 deg
Mean anomaly: 39
7511 deg
Mean motion: 15
72443627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 295
Coasting Arc #2 (Orbit 2211)
---------------------------------------
Vector Time (GMT): 2011/048/20:06:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3311869
79 A = 6736061
42 meter
Y = -5752001
66 meter E =
0004529
Z = -1137722
11 I = 51
93544
XDOT = 4676
083102 Wp = 141
80972
YDOT = -1525
078670 meter/sec RA = 52
35334 deg
ZDOT = -5917
481173 TA = 50
58164
MA = 50
54155
Ha = 192
199 n
mi
Hp = 187
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10865714
53 X = -3241777
01
Y = -18871396
54 feet Y = -5788645
15 meter
Z = -3732684
10 Z = -1153640
06
XDOT = 15341
479992 XDOT = 4721
534377
YDOT = -5003
538942 feet/sec YDOT = -1472
534087 meter/sec
ZDOT = -19414
308312 ZDOT = -5894
655041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19202370
25 X = -5852882
45
Y = 10245954
51 feet Y = 3122966
94 meter
Z = -3796799
00 Z = -1157264
33
XDOT = -3769
857717 XDOT = -1149
052632
YDOT = -14206
310968 feet/sec YDOT = -4330
083583 meter/sec
ZDOT = -19322
096758 ZDOT = -5889
375092
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 11048
86716552
00016717 00000-0 10270-3 0 9012
2 25544 51
6449 52
8105 0004848 322
6087 37
4737 15
72430625 22127
Satellite: ISS
Catalog Number: 25544
Epoch time: 11048
86716552 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 52
8105 deg
Eccentricity:
0004848
Arg of perigee: 322
6087 deg
Mean anomaly: 37
4737 deg
Mean motion: 15
72430625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2212
Checksum: 303
Coasting Arc #3 (Orbit 2227)
---------------------------------------
Vector Time (GMT): 2011/049/20:10:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4583199
90 A = 6726125
42 meter
Y = 680593
08 meter E =
0008435
Z = 4875831
52 I = 51
88336
XDOT = -3467
940616 Wp = 21
39928
YDOT = -6458
567596 meter/sec RA = 47
20382 deg
ZDOT = -2349
331714 TA = 91
47333
MA = 91
37670
Ha = 192
311 n
mi
Hp = 186
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15036745
08 X = -4614154
99
Y = 2232916
94 feet Y = 629168
29 meter
Z = 15996822
58 Z = 4853491
77
XDOT = -11377
757928 XDOT = -3384
049660
YDOT = -21189
526233 feet/sec YDOT = -6496
879341 meter/sec
ZDOT = -7707
781213 ZDOT = -2365
974161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2283946
98 X = 696147
04
Y = 15124536
43 feet Y = 4609958
70 meter
Z = 15906600
43 Z = 4848331
81
XDOT = -20049
058097 XDOT = -6110
952908
YDOT = 11235
491559 feet/sec YDOT = 3424
577827 meter/sec
ZDOT = -7774
799607 ZDOT = -2369
758920
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 11049
88397870
00016717 00000-0 10270-3 0 9024
2 25544 51
6450 47
5999 0005075 327
4586 32
6263 15
72540463 22281
Satellite: ISS
Catalog Number: 25544
Epoch time: 11049
88397870 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 47
5999 deg
Eccentricity:
0005075
Arg of perigee: 327
4586 deg
Mean anomaly: 32
6263 deg
Mean motion: 15
72540463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2228
Checksum: 329
Coasting Arc #4 (Orbit 2243)
---------------------------------------
Vector Time (GMT): 2011/050/20:10:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3915072
41 A = 6735191
65 meter
Y = 5230852
83 meter E =
0014756
Z = 1597628
04 I = 51
89207
XDOT = -4767
655861 Wp = 43
08326
YDOT = 1797
556491 meter/sec RA = 42
12985 deg
ZDOT = 5777
362356 TA = 334
48640
MA = 334
55916
Ha = 192
316 n
mi
Hp = 186
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12844725
76 X = 3848528
25
Y = 17161590
64 feet Y = 5274261
62 meter
Z = 5241561
81 Z = 1616484
86
XDOT = -15641
915554 XDOT = -4815
466832
YDOT = 5897
495050 feet/sec YDOT = 1743
974902 meter/sec
ZDOT = 18954
600906 ZDOT = 5754
085355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16895090
84 X = 5149623
69
Y = -13162853
36 feet Y = -4012037
70 meter
Z = 5317550
22 Z = 1620789
31
XDOT = 5260
628292 XDOT = 1603
439503
YDOT = 14398
459292 feet/sec YDOT = 4388
650392 meter/sec
ZDOT = 18860
566167 ZDOT = 5748
700568
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 11050
90077292
00016717 00000-0 10270-3 0 9033
2 25544 51
6447 42
3892 0005042 331
1396 28
9486 15
72543100 22441
Satellite: ISS
Catalog Number: 25544
Epoch time: 11050
90077292 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 42
3892 deg
Eccentricity:
0005042
Arg of perigee: 331
1396 deg
Mean anomaly: 28
9486 deg
Mean motion: 15
72543100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2244
Checksum: 288
Coasting Arc #5 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2011/051/20:10:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3609886
68 A = 6724749
35 meter
Y = -2364987
63 meter E =
0011897
Z = -5166921
04 I = 51
83331
XDOT = 5374
034426 Wp = 79
77898
YDOT = 5341
975992 meter/sec RA = 36
99441 deg
ZDOT = 1314
088365 TA = 202
74713
MA = 202
79989
Ha = 192
409 n
mi
Hp = 186
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11843460
25 X = 3661163
62
Y = -7759145
76 feet Y = -2324333
46 meter
Z = -16951840
69 Z = -5149259
78
XDOT = 17631
346542 XDOT = 5307
516546
YDOT = 17526
167952 feet/sec YDOT = 5401
699896 meter/sec
ZDOT = 4311
313535 ZDOT = 1340
032868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8204916
86 X = -2500858
66
Y = -11643282
01 feet Y = -3548872
36 meter
Z = -16880465
63 Z = -5145165
92
XDOT = 16000
620482 XDOT = 4876
989123
YDOT = -17655
647244 feet/sec YDOT = -5381
441280 meter/sec
ZDOT = 4415
906577 ZDOT = 1345
968325
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 11051
85399714
00016717 00000-0 10270-3 0 9045
2 25544 51
6443 37
5041 0005038 334
7154 25
3761 15
72579039 22598
Satellite: ISS
Catalog Number: 25544
Epoch time: 11051
85399714 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 37
5041 deg
Eccentricity:
0005038
Arg of perigee: 334
7154 deg
Mean anomaly: 25
3761 deg
Mean motion: 15
72579039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 307
Coasting Arc #6 (Orbit 2274)
---------------------------------------
Vector Time (GMT): 2011/052/20:10:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5368790
96 A = 6736008
10 meter
Y = -4001947
78 meter E =
0006018
Z = -712994
92 I = 51
84634
XDOT = 3365
593917 Wp = 126
06990
YDOT = -3453
671553 meter/sec RA = 31
90281 deg
ZDOT = -5996
114093 TA = 61
66816
MA = 61
60747
Ha = 192
449 n
mi
Hp = 186
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17614143
57 X = -5320177
85
Y = -13129749
93 feet Y = -4061713
09 meter
Z = -2339222
19 Z = -738957
73
XDOT = 11041
974792 XDOT = 3433
090993
YDOT = -11330
943414 feet/sec YDOT = -3415
658500 meter/sec
ZDOT = -19672
290330 ZDOT = -5979
600075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12143612
64 X = -3701373
13
Y = 18294269
02 feet Y = 5576093
20 meter
Z = -2443919
05 Z = -744906
53
XDOT = -10593
344339 XDOT = -3228
851354
YDOT = -9634
731917 feet/sec YDOT = -2936
666288 meter/sec
ZDOT = -19605
514133 ZDOT = -5975
760708
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 11052
87074885
00016717 00000-0 10270-3 0 9058
2 25544 51
6445 32
2946 0004908 337
6871 22
4077 15
72568557 22758
Satellite: ISS
Catalog Number: 25544
Epoch time: 11052
87074885 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 32
2946 deg
Eccentricity:
0004908
Arg of perigee: 337
6871 deg
Mean anomaly: 22
4077 deg
Mean motion: 15
72568557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2275
Checksum: 330
Coasting Arc #7 (Orbit 2290)
---------------------------------------
Vector Time (GMT): 2011/053/20:10:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2179831
78 A = 6724060
22 meter
Y = 3553309
91 meter E =
0005503
Z = 5275403
58 I = 51
77978
XDOT = -6756
119234 Wp = 9
16888
YDOT = -3680
677288 meter/sec RA = 26
77963 deg
ZDOT = -307
141264 TA = 83
77282
MA = 83
71013
Ha = 192
582 n
mi
Hp = 186
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7151679
07 X = -2245030
17
Y = 11657840
93 feet Y = 3528569
45 meter
Z = 17307754
51 Z = 5264655
54
XDOT = -22165
745520 XDOT = -6712
967057
YDOT = -12075
712887 feet/sec YDOT = -3755
987041 meter/sec
ZDOT = -1007
681311 ZDOT = -339
857038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12151121
79 X = 3703661
92
Y = 6395781
48 feet Y = 1949434
19 meter
Z = 17264250
73 Z = 5262143
62
XDOT = -9980
757546 XDOT = -3042
134900
YDOT = 22086
015968 feet/sec YDOT = 6731
817667 meter/sec
ZDOT = -1139
642499 ZDOT = -347
363034
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 11053
88747675
00016717 00000-0 10270-3 0 9065
2 25544 51
6443 27
0835 0004964 342
1005 17
9982 15
72623332 22912
Satellite: ISS
Catalog Number: 25544
Epoch time: 11053
88747675 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 27
0835 deg
Eccentricity:
0004964
Arg of perigee: 342
1005 deg
Mean anomaly: 17
9982 deg
Mean motion: 15
72623332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2291
Checksum: 311
Coasting Arc #8 (Orbit 2305)
---------------------------------------
Vector Time (GMT): 2011/054/20:10:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6298548
48 A = 6735994
04 meter
Y = 2356283
91 meter E =
0015181
Z = -172139
42 I = 51
79142
XDOT = -1530
198971 Wp = 27
35991
YDOT = 4516
019568 meter/sec RA = 21
66535 deg
ZDOT = 6049
451118 TA = 330
77388
MA = 330
85873
Ha = 192
576 n
mi
Hp = 186
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20664529
14 X = 6272568
16
Y = 7730590
26 feet Y = 2426572
82 meter
Z = -564761
87 Z = -141604
69
XDOT = -5020
337832 XDOT = -1609
970955
YDOT = 14816
337166 feet/sec YDOT = 4498
462125 meter/sec
ZDOT = 19847
280571 ZDOT = 6041
823607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5855698
40 X = 1784816
87
Y = -21274857
46 feet Y = -6484576
55 meter
Z = -441568
56 Z = -134590
10
XDOT = 13665
146493 XDOT = 4165
136651
YDOT = 3369
309393 feet/sec YDOT = 1026
965503 meter/sec
ZDOT = 19816
339039 ZDOT = 6040
020139
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 11054
84063838
00016717 00000-0 10270-3 0 9075
2 25544 51
6433 22
1979 0005001 345
2493 14
8523 15
72657324 23066
Satellite: ISS
Catalog Number: 25544
Epoch time: 11054
84063838 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 22
1979 deg
Eccentricity:
0005001
Arg of perigee: 345
2493 deg
Mean anomaly: 14
8523 deg
Mean motion: 15
72657324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2306
Checksum: 295
Coasting Arc #9 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2011/055/20:10:08
628
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 466249
29 A = 6723925
82 meter
Y = -4186416
64 meter E =
0015166
Z = -5253427
20 I = 51
72134
XDOT = 7474
325443 Wp = 66
04354
YDOT = 1673
611958 meter/sec RA = 16
55465 deg
ZDOT = -665
806889 TA = 197
59653
MA = 197
64912
Ha = 192
560 n
mi
Hp = 185
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1529689
27 X = 538547
71
Y = -13734962
73 feet Y = -4180798
61 meter
Z = -17235653
54 Z = -5250986
51
XDOT = 24522
065103 XDOT = 7458
289604
YDOT = 5490
852882 feet/sec YDOT = 1757
104714 meter/sec
ZDOT = -2184
405805 ZDOT = -629
536210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13831381
56 X = -4215805
10
Y = -162709
95 feet Y = -49593
99 meter
Z = -17225658
57 Z = -5250380
73
XDOT = 2838
664973 XDOT = 865
225084
YDOT = -23970
864528 feet/sec YDOT = -7306
319508 meter/sec
ZDOT = -2038
035404 ZDOT = -621
193191
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 11055
85732219
00016717 00000-0 10270-3 0 9084
2 25544 51
6422 16
9865 0004887 349
6344 10
4717 15
72705009 23222
Satellite: ISS
Catalog Number: 25544
Epoch time: 11055
85732219 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 16
9865 deg
Eccentricity:
0004887
Arg of perigee: 349
6344 deg
Mean anomaly: 10
4717 deg
Mean motion: 15
72705009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2322
Checksum: 310
Coasting Arc #10 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2011/056/10:36:14
421
Vector Time (MET): N/A
Weight (LBS) : 863338
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1176256
21 A = 6725722
00 meter
Y = 4339459
11 meter E =
0005577
Z = 4997050
50 I = 51
70704
XDOT = -7451
546432 Wp = 67
68193
YDOT = -212
764560 meter/sec RA = 13
48758 deg
ZDOT = 1939
149607 TA = 3
61111
MA = 3
60709
Ha = 193
468 n
mi
Hp = 185
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3859108
31 X = 1103369
83
Y = 14237070
58 feet Y = 4352205
26 meter
Z = 16394522
65 Z = 5002587
55
XDOT = -24447
330814 XDOT = -7458
033302
YDOT = -698
046458 feet/sec YDOT = -296
128504 meter/sec
ZDOT = 6362
039392 ZDOT = 1902
934933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7799540
61 X = -2377299
98
Y = 12491016
47 feet Y = 3807261
82 meter
Z = 16416727
53 Z = 5003818
55
XDOT = -15348
428529 XDOT = -4678
201016
YDOT = -17751
554881 feet/sec YDOT = -5410
673928 meter/sec
ZDOT = 6215
845233 ZDOT = 1894
589627
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 11056
49275026
00016717 00000-0 10270-3 0 9094
2 25544 51
6421 13
7314 0005323 5
8808 354
2416 15
72441924 23326
Satellite: ISS
Catalog Number: 25544
Epoch time: 11056
49275026 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 13
7314 deg
Eccentricity:
0005323
Arg of perigee: 5
8808 deg
Mean anomaly: 354
2416 deg
Mean motion: 15
72441924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 284
Coasting Arc #11 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2011/057/10:36:14
421
Vector Time (MET): N/A
Weight (LBS) : 863338
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6321940
88 A = 6734576
07 meter
Y = -800653
96 meter E =
0011295
Z = -2163911
71 I = 51
70681
XDOT = 2483
560843 Wp = 27
17903
YDOT = 4764
075305 meter/sec RA = 8
33413 deg
ZDOT = 5514
193876 TA = 308
63597
MA = 308
73702
Ha = 193
624 n
mi
Hp = 185
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20741275
84 X = 6340935
73
Y = -2626817
46 feet Y = -729852
02 meter
Z = -7099447
87 Z = -2133154
29
XDOT = 8148
165496 XDOT = 2403
317131
YDOT = 15630
168324 feet/sec YDOT = 4791
399396 meter/sec
ZDOT = 18091
187257 ZDOT = 5526
063759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16374437
04 X = 4990928
41
Y = 13066237
49 feet Y = 3982589
19 meter
Z = -6975249
29 Z = -2126055
98
XDOT = -4645
939005 XDOT = -1416
082209
YDOT = 15467
849168 feet/sec YDOT = 4714
600426 meter/sec
ZDOT = 18138
942630 ZDOT = 5528
749713
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 11057
44602865
00016717 00000-0 10270-3 0 9107
2 25544 51
6420 8
8474 0005336 11
1142 349
0138 15
72466760 23476
Satellite: ISS
Catalog Number: 25544
Epoch time: 11057
44602865 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 8
8474 deg
Eccentricity:
0005336
Arg of perigee: 11
1142 deg
Mean anomaly: 349
0138 deg
Mean motion: 15
72466760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 287
Coasting Arc #12 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2011/058/10:36:14
421
Vector Time (MET): N/A
Weight (LBS) : 863338
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3083314
31 A = 6727168
95 meter
Y = -3826512
55 meter E =
0014284
Z = -4607985
45 I = 51
65273
XDOT = 6826
554890 Wp = 51
65556
YDOT = -1947
725010 meter/sec RA = 3
25370 deg
ZDOT = -2947
874041 TA = 189
05688
MA = 189
08268
Ha = 193
553 n
mi
Hp = 185
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10115860
60 X = -3017912
21
Y = -12554175
05 feet Y = -3860626
47 meter
Z = -15118062
51 Z = -4622804
84
XDOT = 22396
833629 XDOT = 6862
147209
YDOT = -6390
173918 feet/sec YDOT = -1871
187405 meter/sec
ZDOT = -9671
502760 ZDOT = -2914
625040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1734877
09 X = 528790
54
Y = -15972464
03 feet Y = -4868407
04 meter
Z = -15177758
57 Z = -4626180
81
XDOT = 19269
715594 XDOT = 5873
409313
YDOT = 11163
555809 feet/sec YDOT = 3402
651811 meter/sec
ZDOT = -9537
205586 ZDOT = -2906
940263
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 11058
46283610
00016717 00000-0 10270-3 0 9114
2 25544 51
6427 3
6369 0005338 13
9170 346
2138 15
72505934 23636
Satellite: ISS
Catalog Number: 25544
Epoch time: 11058
46283610 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 3
6369 deg
Eccentricity:
0005338
Arg of perigee: 13
9170 deg
Mean anomaly: 346
2138 deg
Mean motion: 15
72505934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 294
Coasting Arc #13 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2011/059/10:36:14
421
Vector Time (MET): N/A
Weight (LBS) : 863338
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5482558
56 A = 6732569
42 meter
Y = 2532989
67 meter E =
0015154
Z = 2967146
38 I = 51
64066
XDOT = -4467
806298 Wp = 76
62401
YDOT = -3799
665516 meter/sec RA = 358
08438 deg
ZDOT = -4987
002865 TA = 69
15786
MA = 68
99563
Ha = 193
604 n
mi
Hp = 185
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17987396
84 X = -5524888
89
Y = 8310333
56 feet Y = 2471443
82 meter
Z = 9734732
22 Z = 2940409
99
XDOT = -14658
157145 XDOT = -4400
760422
YDOT = -12466
094212 feet/sec YDOT = -3849
252554 meter/sec
ZDOT = -16361
557957 ZDOT = -5008
543821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18774105
81 X = -5722347
45
Y = -6498655
59 feet Y = -1980790
22 meter
Z = 9626709
03 Z = 2934220
91
XDOT = -2346
808082 XDOT = -715
307104
YDOT = -17707
349349 feet/sec YDOT = -5397
200082 meter/sec
ZDOT = -16448
392130 ZDOT = -5013
469921
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 11059
47961951
00016717 00000-0 10270-3 0 9128
2 25544 51
6429 358
4270 0005396 16
7431 343
3908 15
72551150 23796
Satellite: ISS
Catalog Number: 25544
Epoch time: 11059
47961951 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 358
4270 deg
Eccentricity:
0005396
Arg of perigee: 16
7431 deg
Mean anomaly: 343
3908 deg
Mean motion: 15
72551150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 318
Coasting Arc #14 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2011/060/10:36:14
421
Vector Time (MET): N/A
Weight (LBS) : 863338
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622821
76 A = 6728801
01 meter
Y = 2686037
94 meter E =
0012182
Z = 4073570
11 I = 51
59925
XDOT = -5547
798488 Wp = 78
50803
YDOT = 3735
285071 meter/sec RA = 353
00858 deg
ZDOT = 3825
617417 TA = 332
14570
MA = 332
21087
Ha = 193
365 n
mi
Hp = 185
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15166738
07 X = 4572654
34
Y = 8812460
43 feet Y = 2737452
87 meter
Z = 13364731
34 Z = 4095905
08
XDOT = -18201
438610 XDOT = -5607
738420
YDOT = 12254
872280 feet/sec YDOT = 3672
911316 meter/sec
ZDOT = 12551
238246 ZDOT = 3798
521230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5071048
31 X = 1545655
52
Y = 16719988
68 feet Y = 5096252
55 meter
Z = 13454809
32 Z = 4101025
88
XDOT = -20515
151632 XDOT = -6253
018217
YDOT = -3808
895048 feet/sec YDOT = -1160
951211 meter/sec
ZDOT = 12441
726635 ZDOT = 3792
238278
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 11060
49637783
00016717 00000-0 10270-3 0 9136
2 25544 51
6438 353
2175 0005193 19
9513 340
1851 15
72616433 23950
Satellite: ISS
Catalog Number: 25544
Epoch time: 11060
49637783 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 353
2175 deg
Eccentricity:
0005193
Arg of perigee: 19
9513 deg
Mean anomaly: 340
1851 deg
Mean motion: 15
72616433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 310
Coasting Arc #15 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2011/061/10:36:14
421
Vector Time (MET): N/A
Weight (LBS) : 863338
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4100155
94 A = 6730358
49 meter
Y = -3869875
87 meter E =
0008591
Z = -3678691
21 I = 51
57373
XDOT = 5964
563868 Wp = 62
43722
YDOT = 2221
583813 meter/sec RA = 347
82883 deg
ZDOT = 4322
467914 TA = 253
33396
MA = 253
42829
Ha = 193
628 n
mi
Hp = 185
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13451955
18 X = 4160994
78
Y = -12696443
13 feet Y = -3823685
56 meter
Z = -12069196
87 Z = -3658625
17
XDOT = 19568
779096 XDOT = 5918
281258
YDOT = 7288
660805 feet/sec YDOT = 2288
024743 meter/sec
ZDOT = 14181
325178 ZDOT = 4351
330300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18545010
90 X = 5652519
32
Y = -434830
83 feet Y = -132536
44 meter
Z = -11988067
92 Z = -3653963
10
XDOT = 9618
172669 XDOT = 2931
619030
YDOT = 17076
601903 feet/sec YDOT = 5204
948260 meter/sec
ZDOT = 14297
768293 ZDOT = 4357
959776
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 11061
44956938
00016717 00000-0 10270-3 0 9149
2 25544 51
6436 348
3328 0005366 22
9201 337
2200 15
72602516 24103
Satellite: ISS
Catalog Number: 25544
Epoch time: 11061
44956938 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 348
3328 deg
Eccentricity:
0005366
Arg of perigee: 22
9201 deg
Mean anomaly: 337
2200 deg
Mean motion: 15
72602516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 286
Coasting Arc #16 (Orbit 2425)
---------------------------------------
Vector Time (GMT): 2011/062/10:36:14
421
Vector Time (MET): N/A
Weight (LBS) : 863338
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5655584
12 A = 6730622
86 meter
Y = -1136846
79 meter E =
0009255
Z = -3479194
11 I = 51
54672
XDOT = 3775
242960 Wp = 54
78963
YDOT = -4936
509533 meter/sec RA = 342
74978 deg
ZDOT = -4527
017759 TA = 166
47122
MA = 166
44639
Ha = 193
563 n
mi
Hp = 184
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18555066
00 X = -5625550
52
Y = -3729812
31 feet Y = -1199923
37 meter
Z = -11414678
85 Z = -3506595
12
XDOT = 12385
967715 XDOT = 3852
154188
YDOT = -16195
897418 feet/sec YDOT = -4893
862885 meter/sec
ZDOT = -14852
420470 ZDOT = -4508
490850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11539892
56 X = -3517359
25
Y = -14916308
96 feet Y = -4546490
97 meter
Z = -11525253
75 Z = -3512897
34
XDOT = 18943
192545 XDOT = 5773
885088
YDOT = -3245
376294 feet/sec YDOT = -989
190694 meter/sec
ZDOT = -14777
478571 ZDOT = -4504
175468
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 11062
46628239
00016717 00000-0 10270-3 0 9153
2 25544 51
6445 343
1223 0005379 27
0228 333
1213 15
72667146 24265
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
46628239 = yrday
fracday
Element set: 915
Inclination: 51
6445 deg
RA of node: 343
1223 deg
Eccentricity:
0005379
Arg of perigee: 27
0228 deg
Mean anomaly: 333
1213 deg
Mean motion: 15
72667146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 292
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list