[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 14th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 67 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
080/00:53:06
082 -3
6 4
2 4
2
N/A 1
1 -0
0 227
2
000/00:10:08
165 -1
8 -0
1 215
4
Coasting Arc #1 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2013/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3985969
76 A = 6792270
57 meter
Y = 5292097
40 meter E =
0009052
Z = -1519346
36 I = 51
41913
XDOT = -4700
923540 Wp = 52
43903
YDOT = 1899
365114 meter/sec RA = 222
47197 deg
ZDOT = -5735
165714 TA = 144
17571
MA = 144
11496
Ha = 226
474 n
mi
Hp = 214
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13077328
61 X = 3933876
70
Y = 17362524
28 feet Y = 5336379
53 meter
Z = -4984732
15 Z = -1500110
27
XDOT = -15422
977492 XDOT = -4693
953490
YDOT = 6231
512840 feet/sec YDOT = 1846
834551 meter/sec
ZDOT = -18816
160480 ZDOT = -5757
985630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10052747
85 X = 3064077
54
Y = 19292550
39 feet Y = 5880369
36 meter
Z = -4905210
25 Z = -1495108
08
XDOT = -14720
006266 XDOT = -4486
657910
YDOT = 2877
245643 feet/sec YDOT = 876
984472 meter/sec
ZDOT = -18911
334731 ZDOT = -5764
174826
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 13072
52930522
00016717 00000-0 10270-3 0 9008
2 25544 51
6443 223
3266 0012306 9
8066 350
3324 15
52789035 19858
Satellite: ISS
Catalog Number: 25544
Epoch time: 13072
52930522 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 223
3266 deg
Eccentricity:
0012306
Arg of perigee: 9
8066 deg
Mean anomaly: 350
3324 deg
Mean motion: 15
52789035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 290
Coasting Arc #2 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2013/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3353864
11 A = 6790218
40 meter
Y = -5250265
64 meter E =
0021751
Z = 2665027
83 I = 51
43678
XDOT = 5584
247496 Wp = 47
82744
YDOT = -927
968863 meter/sec RA = 217
48971 deg
ZDOT = 5186
633647 TA = 342
37036
MA = 342
44574
Ha = 226
490 n
mi
Hp = 214
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11003491
17 X = -3307851
22
Y = -17225280
96 feet Y = -5287513
02 meter
Z = 8743529
64 Z = 2648847
57
XDOT = 18321
021968 XDOT = 5569
013971
YDOT = -3044
517266 feet/sec YDOT = -865
606758 meter/sec
ZDOT = 17016
514591 ZDOT = 5213
724507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8375678
40 X = -2552906
78
Y = -18676162
51 feet Y = -5692494
33 meter
Z = 8676715
83 Z = 2644662
99
XDOT = 17103
843190 XDOT = 5213
251404
YDOT = 307
265593 feet/sec YDOT = 93
654553 meter/sec
ZDOT = 17129
372061 ZDOT = 5221
032604
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 13073
55903820
00016717 00000-0 10270-3 0 9014
2 25544 51
6455 218
2040 0012105 13
5310 346
6165 15
52804729 20014
Satellite: ISS
Catalog Number: 25544
Epoch time: 13073
55903820 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 218
2040 deg
Eccentricity:
0012105
Arg of perigee: 13
5310 deg
Mean anomaly: 346
6165 deg
Mean motion: 15
52804729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 262
Coasting Arc #3 (Orbit 2015)
---------------------------------------
Vector Time (GMT): 2013/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2539081
70 A = 6787466
49 meter
Y = 5109498
61 meter E =
0015615
Z = -3695718
43 I = 51
45274
XDOT = -6328
090384 Wp = 35
93918
YDOT = 31
437818 meter/sec RA = 212
50437 deg
ZDOT = -4301
044253 TA = 188
09777
MA = 188
12300
Ha = 226
636 n
mi
Hp = 214
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8330320
54 X = 2499710
29
Y = 16763446
90 feet Y = 5137671
64 meter
Z = -12125060
46 Z = -3683480
04
XDOT = -20761
451391 XDOT = -6307
078291
YDOT = 103
142449 feet/sec YDOT = -39
209905 meter/sec
ZDOT = -14111
037575 ZDOT = -4331
734516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6127239
75 X = 1867582
68
Y = 17722432
27 feet Y = 5401797
35 meter
Z = -12074635
02 Z = -3680348
76
XDOT = -19215
546059 XDOT = -5856
898439
YDOT = -3064
666076 feet/sec YDOT = -934
110220 meter/sec
ZDOT = -14238
795298 ZDOT = -4339
984807
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 13074
52440086
00016717 00000-0 10270-3 0 9023
2 25544 51
6457 213
4018 0012261 17
0450 343
1112 15
52804184 20160
Satellite: ISS
Catalog Number: 25544
Epoch time: 13074
52440086 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 213
4018 deg
Eccentricity:
0012261
Arg of perigee: 17
0450 deg
Mean anomaly: 343
1112 deg
Mean motion: 15
52804184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 257
Coasting Arc #4 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2013/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1539221
02 A = 6784504
97 meter
Y = -4833216
57 meter E =
0015020
Z = 4490229
33 I = 51
47037
XDOT = 6941
869083 Wp = 57
55044
YDOT = 752
292072 meter/sec RA = 207
51432 deg
ZDOT = 3189
494856 TA =
36883
MA =
36773
Ha = 226
640 n
mi
Hp = 213
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5049937
73 X = -1506872
89
Y = -15857009
73 feet Y = -4850247
77 meter
Z = 14731723
54 Z = 4482831
01
XDOT = 22775
161033 XDOT = 6917
447146
YDOT = 2468
149841 feet/sec YDOT = 829
784201 meter/sec
ZDOT = 10464
221967 ZDOT = 3223
158439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3292152
70 X = -1003448
14
Y = -16340148
44 feet Y = -4980477
25 meter
Z = 14701414
44 Z = 4480991
12
XDOT = 21086
855963 XDOT = 6427
273698
YDOT = 5291
965496 feet/sec YDOT = 1612
991083 meter/sec
ZDOT = 10604
289557 ZDOT = 3232
187457
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 13075
55410523
00016717 00000-0 10270-3 0 9031
2 25544 51
6463 208
2787 0012224 20
4856 339
6784 15
52853550 20323
Satellite: ISS
Catalog Number: 25544
Epoch time: 13075
55410523 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 208
2787 deg
Eccentricity:
0012224
Arg of perigee: 20
4856 deg
Mean anomaly: 339
6784 deg
Mean motion: 15
52853550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 298
Coasting Arc #5 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2013/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 426631
70 A = 6782324
01 meter
Y = 4527822
76 meter E =
0022779
Z = -5051003
35 I = 51
49074
XDOT = -7282
766522 Wp = 50
83561
YDOT = -1409
140922 meter/sec RA = 202
52197 deg
ZDOT = -1869
931021 TA = 200
91507
MA = 201
00841
Ha = 226
787 n
mi
Hp = 213
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1399710
29 X = 400505
30
Y = 14855061
55 feet Y = 4532447
08 meter
Z = -16571533
30 Z = -5048994
68
XDOT = -23893
590951 XDOT = -7257
384321
YDOT = -4623
165753 feet/sec YDOT = -1490
439650 meter/sec
ZDOT = -6134
944293 ZDOT = -1905
248234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 48760
20 X = 14862
11
Y = 14929553
29 feet Y = 4550527
84 meter
Z = -16563629
41 Z = -5048594
24
XDOT = -22203
231298 XDOT = -6767
544900
YDOT = -6927
440460 feet/sec YDOT = -2111
483852 meter/sec
ZDOT = -6281
844372 ZDOT = -1914
706165
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 13076
51944182
00016717 00000-0 10270-3 0 9042
2 25544 51
6465 203
4770 0012376 23
9700 336
2025 15
52845121 20470
Satellite: ISS
Catalog Number: 25544
Epoch time: 13076
51944182 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 203
4770 deg
Eccentricity:
0012376
Arg of perigee: 23
9700 deg
Mean anomaly: 336
2025 deg
Mean motion: 15
52845121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 286
Coasting Arc #6 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2013/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 809778
51 A = 6780995
91 meter
Y = -4154432
10 meter E =
0013032
Z = 5289999
93 I = 51
51602
XDOT = 7401
839720 Wp = 39
58983
YDOT = 1978
795769 meter/sec RA = 197
52588 deg
ZDOT = 430
228300 TA = 46
35701
MA = 46
24902
Ha = 226
752 n
mi
Hp = 213
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2656753
64 X = 830476
74
Y = -13630026
57 feet Y = -4145260
47 meter
Z = 17355642
81 Z = 5293984
37
XDOT = 24284
251050 XDOT = 7377
072353
YDOT = 6492
112103 feet/sec YDOT = 2061
429353 meter/sec
ZDOT = 1411
510171 ZDOT = 466
125352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3634662
74 X = 1107845
20
Y = -13380373
82 feet Y = -4078337
94 meter
Z = 17372654
50 Z = 5295185
09
XDOT = 22700
393328 XDOT = 6919
079886
YDOT = 8153
430445 feet/sec YDOT = 2485
165600 meter/sec
ZDOT = 1560
783452 ZDOT = 475
726796
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 13077
54911814
00016717 00000-0 10270-3 0 9053
2 25544 51
6468 198
3533 0012422 27
4089 332
7716 15
52897948 20633
Satellite: ISS
Catalog Number: 25544
Epoch time: 13077
54911814 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 198
3533 deg
Eccentricity:
0012422
Arg of perigee: 27
4089 deg
Mean anomaly: 332
7716 deg
Mean motion: 15
52897948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 330
Coasting Arc #7 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2013/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2028957
44 A = 6781221
40 meter
Y = 3814473
94 meter E =
0022569
Z = -5243418
03 I = 51
54644
XDOT = -7183
558132 Wp = 67
40075
YDOT = -2429
917841 meter/sec RA = 192
53304 deg
ZDOT = 1023
991191 TA = 212
36872
MA = 212
50737
Ha = 226
892 n
mi
Hp = 213
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6656684
51 X = -2045989
91
Y = 12514678
29 feet Y = 3791689
20 meter
Z = -17202815
07 Z = -5253316
16
XDOT = -23568
104107 XDOT = -7160
826623
YDOT = -7972
171394 feet/sec YDOT = -2510
121726 meter/sec
ZDOT = 3359
551151 ZDOT = 989
149690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7326468
12 X = -2233107
48
Y = 12075524
57 feet Y = 3680619
89 meter
Z = -17244420
51 Z = -5256099
37
XDOT = -22158
202789 XDOT = -6753
820210
YDOT = -8909
192056 feet/sec YDOT = -2715
521739 meter/sec
ZDOT = 3214
701395 ZDOT = 979
840985
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 13078
51442813
00016717 00000-0 10270-3 0 9060
2 25544 51
6468 193
5518 0012539 31
3667 328
8231 15
52909983 20785
Satellite: ISS
Catalog Number: 25544
Epoch time: 13078
51442813 = yrday
fracday
Element set: 906
Inclination: 51
6468 deg
RA of node: 193
5518 deg
Eccentricity:
0012539
Arg of perigee: 31
3667 deg
Mean anomaly: 328
8231 deg
Mean motion: 15
52909983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 329
Coasting Arc #8 (Orbit 2093)
---------------------------------------
Vector Time (GMT): 2013/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3264721
51 A = 6782851
26 meter
Y = -3441434
91 meter E =
0019196
Z = 4842004
22 I = 51
58238
XDOT = 6682
788324 Wp = 44
08298
YDOT = 2852
211577 meter/sec RA = 187
54166 deg
ZDOT = -2459
293156 TA = 70
17426
MA = 69
96743
Ha = 226
944 n
mi
Hp = 213
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10711028
58 X = 3279440
74
Y = -11290796
95 feet Y = -3404844
03 meter
Z = 15885840
60 Z = 4857899
88
XDOT = 21925
158543 XDOT = 6662
344108
YDOT = 9357
649530 feet/sec YDOT = 2926
828202 meter/sec
ZDOT = -8068
547100 ZDOT = -2426
878892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11119630
18 X = 3389263
28
Y = -10790884
89 feet Y = -3289061
71 meter
Z = 15952391
32 Z = 4862288
87
XDOT = 20735
190868 XDOT = 6320
086177
YDOT = 9544
541358 feet/sec YDOT = 2909
176206 meter/sec
ZDOT = -7933
831288 ZDOT = -2418
231777
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 13079
54407764
00016717 00000-0 10270-3 0 9071
2 25544 51
6471 188
4278 0012644 35
1235 325
0748 15
52908481 20947
Satellite: ISS
Catalog Number: 25544
Epoch time: 13079
54407764 = yrday
fracday
Element set: 907
Inclination: 51
6471 deg
RA of node: 188
4278 deg
Eccentricity:
0012644
Arg of perigee: 35
1235 deg
Mean anomaly: 325
0748 deg
Mean motion: 15
52908481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2094
Checksum: 322
Coasting Arc #9 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2013/080/00:58:10
165
Vector Time (MET): N/A
Weight (LBS) : 921890
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1164845
54 A = 6783839
76 meter
Y = 4230464
59 meter E =
0021605
Z = -5191910
85 I = 51
59424
XDOT = -7520
044115 Wp = 58
95622
YDOT = 421
242868 meter/sec RA = 184
88486 deg
ZDOT = -1337
201673 TA = 198
11566
MA = 198
19276
Ha = 227
183 n
mi
Hp = 215
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3821671
73 X = 1142673
72
Y = 13879477
00 feet Y = 4243366
19 meter
Z = -17033828
24 Z = -5186306
41
XDOT = -24672
060745 XDOT = -7517
699920
YDOT = 1382
030406 feet/sec YDOT = 337
161989 meter/sec
ZDOT = -4387
144596 ZDOT = -1373
727433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6825283
35 X = -2080346
37
Y = -12705936
30 feet Y = -3872769
38 meter
Z = -17010909
77 Z = -5184925
30
XDOT = 22841
128770 XDOT = 6961
976049
YDOT = -6162
660004 feet/sec YDOT = -1878
378769 meter/sec
ZDOT = -4539
323366 ZDOT = -1383
585762
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 13080
05890256
00016717 00000-0 10270-3 0 9082
2 25544 51
6470 185
8697 0009975 28
8430 331
3271 15
52125024 21026
Satellite: ISS
Catalog Number: 25544
Epoch time: 13080
05890256 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 185
8697 deg
Eccentricity:
0009975
Arg of perigee: 28
8430 deg
Mean anomaly: 331
3271 deg
Mean motion: 15
52125024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 302
Coasting Arc #10 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2013/081/00:58:10
165
Vector Time (MET): N/A
Weight (LBS) : 921890
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -176806
83 A = 6783077
12 meter
Y = -4206258
36 meter E =
0011072
Z = 5311661
84 I = 51
62268
XDOT = 7669
037255 Wp = 43
91744
YDOT = -135
858552 meter/sec RA = 179
90386 deg
ZDOT = 155
301455 TA = 44
64744
MA = 44
55833
Ha = 227
140 n
mi
Hp = 215
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -580074
90 X = -155560
80
Y = -13800060
25 feet Y = -4208116
21 meter
Z = 17426712
06 Z = 5310854
96
XDOT = 25160
883384 XDOT = 7669
232069
YDOT = -445
730157 feet/sec YDOT = -50
097444 meter/sec
ZDOT = 509
519209 ZDOT = 192
557098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3873860
35 X = 1180752
63
Y = 13261742
99 feet Y = 4042179
26 meter
Z = 17423771
75 Z = 5310765
63
XDOT = -23398
635835 XDOT = -7131
904203
YDOT = 5994
397141 feet/sec YDOT = 1827
092249 meter/sec
ZDOT = 664
726562 ZDOT = 202
608656
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 13081
08906784
00016717 00000-0 10270-3 0 9091
2 25544 51
6469 180
7497 0009904 31
7637 328
4110 15
52164241 21180
Satellite: ISS
Catalog Number: 25544
Epoch time: 13081
08906784 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 180
7497 deg
Eccentricity:
0009904
Arg of perigee: 31
7637 deg
Mean anomaly: 328
4110 deg
Mean motion: 15
52164241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 315
Coasting Arc #11 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2013/082/00:58:10
165
Vector Time (MET): N/A
Weight (LBS) : 921890
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -780366
98 A = 6783408
88 meter
Y = 4240860
37 meter E =
0021021
Z = -5252954
79 I = 51
65522
XDOT = -7581
212213 Wp = 72
97372
YDOT = -139
286725 meter/sec RA = 174
92503 deg
ZDOT = 1023
193583 TA = 206
78937
MA = 206
89809
Ha = 227
271 n
mi
Hp = 215
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2560259
13 X = -802213
99
Y = 13913583
91 feet Y = 4232011
07 meter
Z = -17234103
64 Z = -5256799
26
XDOT = -24872
743481 XDOT = -7584
061579
YDOT = -456
977444 feet/sec YDOT = -224
080429 meter/sec
ZDOT = 3356
934327 ZDOT = 986
358176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1087136
93 X = -331359
34
Y = -14085240
01 feet Y = -4293181
15 meter
Z = -17250542
58 Z = -5257965
38
XDOT = 23195
725765 XDOT = 7070
057213
YDOT = -5675
982779 feet/sec YDOT = -1730
039551 meter/sec
ZDOT = 3203
489335 ZDOT = 976
423549
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 13082
05483745
00016717 00000-0 10270-3 0 9108
2 25544 51
6478 175
9499 0010035 35
3737 324
8079 15
52159570 21336
Satellite: ISS
Catalog Number: 25544
Epoch time: 13082
05483745 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 175
9499 deg
Eccentricity:
0010035
Arg of perigee: 35
3737 deg
Mean anomaly: 324
8079 deg
Mean motion: 15
52159570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 318
Coasting Arc #12 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2013/083/00:58:10
165
Vector Time (MET): N/A
Weight (LBS) : 921890
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1764734
66 A = 6784477
75 meter
Y = -4284172
88 meter E =
0016129
Z = 4949658
68 I = 51
68984
XDOT = 7333
781022 Wp = 45
93605
YDOT = 463
688041 meter/sec RA = 169
94892 deg
ZDOT = -2197
998482 TA = 65
56845
MA = 65
40026
Ha = 227
205 n
mi
Hp = 214
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5789811
86 X = 1788466
12
Y = -14055685
30 feet Y = -4264305
17 meter
Z = 16239037
65 Z = 4958289
73
XDOT = 24060
961359 XDOT = 7338
728097
YDOT = 1521
286225 feet/sec YDOT = 545
726372 meter/sec
ZDOT = -7211
281110 ZDOT = -2162
359974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1752398
42 X = -534131
04
Y = 15060883
82 feet Y = 4590557
39 meter
Z = 16275424
20 Z = 4960749
30
XDOT = -22544
909173 XDOT = -6871
688316
YDOT = 5063
748454 feet/sec YDOT = 1543
430529 meter/sec
ZDOT = -7062
841210 ZDOT = -2152
754001
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 13083
08497613
00016717 00000-0 10270-3 0 9112
2 25544 51
6478 170
8299 0010059 38
2547 321
9316 15
52211088 21497
Satellite: ISS
Catalog Number: 25544
Epoch time: 13083
08497613 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 170
8299 deg
Eccentricity:
0010059
Arg of perigee: 38
2547 deg
Mean anomaly: 321
9316 deg
Mean motion: 15
52211088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 313
Coasting Arc #13 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2013/084/00:58:10
165
Vector Time (MET): N/A
Weight (LBS) : 921890
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2631008
40 A = 6786397
50 meter
Y = 4371079
67 meter E =
0016198
Z = -4486400
15 I = 51
72651
XDOT = -6880
541011 Wp = 75
45395
YDOT = -813
573588 meter/sec RA = 164
97805 deg
ZDOT = 3256
181059 TA = 227
28339
MA = 227
41988
Ha = 227
324 n
mi
Hp = 214
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8631917
33 X = -2657897
60
Y = 14340812
58 feet Y = 4341507
08 meter
Z = -14719160
60 Z = -4499247
23
XDOT = -22573
953447 XDOT = -6886
749642
YDOT = -2669
204685 feet/sec YDOT = -890
550372 meter/sec
ZDOT = 10683
008725 ZDOT = 3222
741237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4148179
18 X = 1264365
01
Y = -16166940
40 feet Y = -4927683
43 meter
Z = -14773125
56 Z = -4502848
67
XDOT = 21293
629244 XDOT = 6490
298194
YDOT = -4129
873372 feet/sec YDOT = -1258
785404 meter/sec
ZDOT = 10543
753313 ZDOT = 3213
736010
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 13084
05072070
00016717 00000-0 10270-3 0 9127
2 25544 51
6482 166
0301 0010078 41
7518 318
4401 15
52193774 21645
Satellite: ISS
Catalog Number: 25544
Epoch time: 13084
05072070 = yrday
fracday
Element set: 912
Inclination: 51
6482 deg
RA of node: 166
0301 deg
Eccentricity:
0010078
Arg of perigee: 41
7518 deg
Mean anomaly: 318
4401 deg
Mean motion: 15
52193774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 276
Coasting Arc #14 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2013/085/00:58:10
165
Vector Time (MET): N/A
Weight (LBS) : 921890
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3464082
29 A = 6788697
76 meter
Y = -4435577
38 meter E =
0020486
Z = 3787474
60 I = 51
76384
XDOT = 6270
835062 Wp = 65
45880
YDOT = 1264
391741 meter/sec RA = 160
01234 deg
ZDOT = -4228
360551 TA = 69
24045
MA = 69
02107
Ha = 227
328 n
mi
Hp = 214
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11365099
37 X = 3495025
90
Y = -14552419
23 feet Y = -4396666
23 meter
Z = 12426097
77 Z = 3804378
62
XDOT = 20573
605847 XDOT = 6276
770505
YDOT = 4148
266868 feet/sec YDOT = 1334
548708 meter/sec
ZDOT = -13872
573986 ZDOT = -4197
883225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6428178
97 X = -1959308
95
Y = 17258340
41 feet Y = 5260342
16 meter
Z = 12496979
50 Z = 3809079
35
XDOT = -19696
185092 XDOT = -6003
397216
YDOT = 2679
337157 feet/sec YDOT = 816
661965 meter/sec
ZDOT = -13745
699113 ZDOT = -4189
689090
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 13085
08083383
00016717 00000-0 10270-3 0 9131
2 25544 51
6481 160
9100 0010191 45
2522 314
9458 15
52236152 21803
Satellite: ISS
Catalog Number: 25544
Epoch time: 13085
08083383 = yrday
fracday
Element set: 913
Inclination: 51
6481 deg
RA of node: 160
9100 deg
Eccentricity:
0010191
Arg of perigee: 45
2522 deg
Mean anomaly: 314
9458 deg
Mean motion: 15
52236152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 278
Coasting Arc #15 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2013/086/00:58:10
165
Vector Time (MET): N/A
Weight (LBS) : 921890
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4113724
97 A = 6791026
83 meter
Y = 4503991
85 meter E =
0014415
Z = -2984532
85 I = 51
79961
XDOT = -5534
878877 Wp = 55
24522
YDOT = -1761
352365 meter/sec RA = 155
05252 deg
ZDOT = 4996
039301 TA = 270
75058
MA = 270
91574
Ha = 227
367 n
mi
Hp = 214
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13496473
01 X = -4149285
73
Y = 14776876
16 feet Y = 4457790
31 meter
Z = -9791774
44 Z = -3004604
07
XDOT = -18159
051433 XDOT = -5539
041182
YDOT = -5778
715109 feet/sec YDOT = -1823
269385 meter/sec
ZDOT = 16391
205057 ZDOT = 4969
141432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8097879
14 X = 2468233
56
Y = -18255992
39 feet Y = -5564426
48 meter
Z = -9875869
32 Z = -3010164
97
XDOT = 17818
929637 XDOT = 5431
209753
YDOT = -858
315828 feet/sec YDOT = -261
614664 meter/sec
ZDOT = 16279
289780 ZDOT = 4961
927525
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 13086
04655284
00016717 00000-0 10270-3 0 9144
2 25544 51
6477 156
1097 0010111 48
1723 312
0290 15
52225905 21950
Satellite: ISS
Catalog Number: 25544
Epoch time: 13086
04655284 = yrday
fracday
Element set: 914
Inclination: 51
6477 deg
RA of node: 156
1097 deg
Eccentricity:
0010111
Arg of perigee: 48
1723 deg
Mean anomaly: 312
0290 deg
Mean motion: 15
52225905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2195
Checksum: 288
Coasting Arc #16 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2013/087/00:58:10
165
Vector Time (MET): N/A
Weight (LBS) : 921890
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4682834
00 A = 6793094
26 meter
Y = -4494784
34 meter E =
0021078
Z = 1987375
92 I = 51
83359
XDOT = 4676
466099 Wp = 87
37844
YDOT = 2377
974813 meter/sec RA = 150
09860 deg
ZDOT = -5588
851768 TA = 70
75984
MA = 70
53192
Ha = 227
449 n
mi
Hp = 214
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15363628
62 X = 4723093
39
Y = -14746667
78 feet Y = -4442192
56 meter
Z = 6520262
22 Z = 2010223
30
XDOT = 15342
736545 XDOT = 4676
676851
YDOT = 7801
754636 feet/sec YDOT = 2430
270402 meter/sec
ZDOT = -18336
127847 ZDOT = -5566
133566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9573332
62 X = -2917951
78
Y = 18989465
54 feet Y = 5787989
10 meter
Z = 6615936
45 Z = 2016537
43
XDOT = -15782
146571 XDOT = -4810
398275
YDOT = -1542
329912 feet/sec YDOT = -470
102157 meter/sec
ZDOT = -18241
689267 ZDOT = -5560
066888
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 13087
07664064
00016717 00000-0 10270-3 0 9155
2 25544 51
6473 150
9893 0010198 52
6314 307
5765 15
52245145 22116
Satellite: ISS
Catalog Number: 25544
Epoch time: 13087
07664064 = yrday
fracday
Element set: 915
Inclination: 51
6473 deg
RA of node: 150
9893 deg
Eccentricity:
0010198
Arg of perigee: 52
6314 deg
Mean anomaly: 307
5765 deg
Mean motion: 15
52245145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 305
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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