[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 3rd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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
There are no maneuvers
Coasting Arc #1 (Orbit 1363)
---------------------------------------
Vector Time (GMT): 2013/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -605099
43 A = 6788183
89 meter
Y = 5463359
31 meter E =
0011309
Z = 3990071
74 I = 51
95615
XDOT = -5474
749607 Wp = 170
56943
YDOT = -3546
051253 meter/sec RA = 61
70740 deg
ZDOT = 4012
671665 TA = 237
66881
MA = 237
77836
Ha = 225
266 n
mi
Hp = 218
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1985234
36 X = -685529
38
Y = 17924407
18 feet Y = 5456143
17 meter
Z = 13090786
54 Z = 3986936
66
XDOT = -17961
776925 XDOT = -5454
182279
YDOT = -11634
026422 feet/sec YDOT = -3607
158171 meter/sec
ZDOT = 13164
933285 ZDOT = 3986
126219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14875402
21 X = -4534022
59
Y = 10213110
50 feet Y = 3112956
08 meter
Z = 13077041
08 Z = 3985882
12
XDOT = -2329
882822 XDOT = -710
148284
YDOT = -20161
620860 feet/sec YDOT = -6145
262038 meter/sec
ZDOT = 13054
907306 ZDOT = 3979
135747
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 13032
55570380
00016717 00000-0 10270-3 0 9009
2 25544 51
6460 62
0843 0012778 224
5786 135
4339 15
52217282 13643
Satellite: ISS
Catalog Number: 25544
Epoch time: 13032
55570380 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 62
0843 deg
Eccentricity:
0012778
Arg of perigee: 224
5786 deg
Mean anomaly: 135
4339 deg
Mean motion: 15
52217282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1364
Checksum: 296
Coasting Arc #2 (Orbit 1378)
---------------------------------------
Vector Time (GMT): 2013/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1178742
61 A = 6785770
86 meter
Y = -4816129
76 meter E =
0005034
Z = -4630307
62 I = 51
93424
XDOT = 5614
473309 Wp = 178
97097
YDOT = 4264
025901 meter/sec RA = 56
75438 deg
ZDOT = -3010
815877 TA = 61
13056
MA = 61
08006
Ha = 225
071 n
mi
Hp = 218
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3867265
78 X = 1255002
58
Y = -15800950
64 feet Y = -4802522
05 meter
Z = -15191297
95 Z = -4624396
07
XDOT = 18420
188021 XDOT = 5581
000392
YDOT = 13989
586288 feet/sec YDOT = 4326
623221 meter/sec
ZDOT = -9878
004847 ZDOT = -2983
622930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14389148
18 X = 4385812
37
Y = -7638323
27 feet Y = -2328160
93 meter
Z = -15166072
38 Z = -4622618
86
XDOT = 1426
215192 XDOT = 434
710391
YDOT = 22043
820557 feet/sec YDOT = 6718
956506 meter/sec
ZDOT = -9765
384031 ZDOT = -2976
489053
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 13033
52141191
00016717 00000-0 10270-3 0 9012
2 25544 51
6473 57
2843 0012854 228
4755 131
5295 15
52241106 13793
Satellite: ISS
Catalog Number: 25544
Epoch time: 13033
52141191 = yrday
fracday
Element set: 901
Inclination: 51
6473 deg
RA of node: 57
2843 deg
Eccentricity:
0012854
Arg of perigee: 228
4755 deg
Mean anomaly: 131
5295 deg
Mean motion: 15
52241106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1379
Checksum: 289
Coasting Arc #3 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2013/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1805755
43 A = 6783994
39 meter
Y = 4135476
01 meter E =
0012235
Z = 5073323
04 I = 51
90958
XDOT = -5661
346239 Wp = 206
22038
YDOT = -4799
797651 meter/sec RA = 51
79608 deg
ZDOT = 1888
514546 TA = 225
47093
MA = 225
57095
Ha = 224
767 n
mi
Hp = 219
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5924394
46 X = -1876509
62
Y = 13567834
69 feet Y = 4114887
36 meter
Z = 16644760
62 Z = 5064379
01
XDOT = -18573
970602 XDOT = -5616
426938
YDOT = -15747
367622 feet/sec YDOT = -4862
855200 meter/sec
ZDOT = 6195
913864 ZDOT = 1861
121616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14032493
91 X = -4277104
14
Y = 4850717
02 feet Y = 1478498
55 meter
Z = 16606995
61 Z = 5061812
26
XDOT = -830
497467 XDOT = -253
135628
YDOT = -23327
538778 feet/sec YDOT = -7110
233819 meter/sec
ZDOT = 6082
538478 ZDOT = 1853
957728
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 13034
55149477
00016717 00000-0 10270-3 0 9022
2 25544 51
6462 52
1636 0012730 232
3136 127
6862 15
52243167 13958
Satellite: ISS
Catalog Number: 25544
Epoch time: 13034
55149477 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 52
1636 deg
Eccentricity:
0012730
Arg of perigee: 232
3136 deg
Mean anomaly: 127
6862 deg
Mean motion: 15
52243167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 294
Coasting Arc #4 (Orbit 1409)
---------------------------------------
Vector Time (GMT): 2013/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2521586
16 A = 6782963
29 meter
Y = -3395591
65 meter E =
0007075
Z = -5305713
01 I = 51
88705
XDOT = 5594
201446 Wp = 145
73355
YDOT = 5194
215938 meter/sec RA = 46
83454 deg
ZDOT = -671
671528 TA = 117
90635
MA = 117
83468
Ha = 224
576 n
mi
Hp = 219
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8272920
47 X = 2585142
43
Y = -11140392
56 feet Y = -3367038
29 meter
Z = -17407194
91 Z = -5293309
15
XDOT = 18353
679285 XDOT = 5538
965615
YDOT = 17041
390873 feet/sec YDOT = 5256
464973 meter/sec
ZDOT = -2203
646746 ZDOT = -644
629799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13835726
59 X = 4217129
47
Y = -1712427
98 feet Y = -521948
05 meter
Z = -17355121
84 Z = -5289841
14
XDOT = 376
931667 XDOT = 114
888772
YDOT = 24040
937269 feet/sec YDOT = 7327
677680 meter/sec
ZDOT = -2091
791902 ZDOT = -637
578172
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 13035
51719043
00016717 00000-0 10270-3 0 9032
2 25544 51
6468 47
3637 0012816 236
2931 123
7000 15
52246950 14104
Satellite: ISS
Catalog Number: 25544
Epoch time: 13035
51719043 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 47
3637 deg
Eccentricity:
0012816
Arg of perigee: 236
2931 deg
Mean anomaly: 123
7000 deg
Mean motion: 15
52246950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 280
Coasting Arc #5 (Orbit 1425)
---------------------------------------
Vector Time (GMT): 2013/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3254177
78 A = 6782890
59 meter
Y = 2688324
53 meter E =
0009864
Z = 5316304
37 I = 51
86429
XDOT = -5384
746004 Wp = 238
07513
YDOT = -5418
699440 meter/sec RA = 41
87002 deg
ZDOT = -561
811385 TA = 217
24118
MA = 217
30962
Ha = 224
237 n
mi
Hp = 219
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10676436
30 X = -3309822
15
Y = 8819962
38 feet Y = 2651623
04 meter
Z = 17441943
46 Z = 5300360
98
XDOT = -17666
489514 XDOT = -5321
023663
YDOT = -17777
885301 feet/sec YDOT = -5478
558745 meter/sec
ZDOT = -1843
213207 ZDOT = -587
814962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13862464
45 X = -4225279
16
Y = -1390300
06 feet Y = -423763
46 meter
Z = 17375228
49 Z = 5295969
64
XDOT = -9
484642 XDOT = -2
890919
YDOT = -24043
908472 feet/sec YDOT = -7328
583302 meter/sec
ZDOT = -1950
712646 ZDOT = -594
577215
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 13036
54725932
00016717 00000-0 10270-3 0 9041
2 25544 51
6457 42
2429 0012732 240
3043 119
6841 15
52267687 14266
Satellite: ISS
Catalog Number: 25544
Epoch time: 13036
54725932 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 42
2429 deg
Eccentricity:
0012732
Arg of perigee: 240
3043 deg
Mean anomaly: 119
6841 deg
Mean motion: 15
52267687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 301
Coasting Arc #6 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2013/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4020122
98 A = 6783901
28 meter
Y = -1986288
45 meter E =
0008736
Z = -5094114
97 I = 51
84403
XDOT = 5005
506008 Wp = 171
15756
YDOT = 5518
198534 meter/sec RA = 36
90486 deg
ZDOT = 1790
542599 TA = 116
17556
MA = 116
08569
Ha = 223
975 n
mi
Hp = 219
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13189379
84 X = 4066780
65
Y = -6516694
37 feet Y = -1941071
92 meter
Z = -16712975
62 Z = -5074472
66
XDOT = 16422
263805 XDOT = 4934
730517
YDOT = 18104
325898 feet/sec YDOT = 5573
777477 meter/sec
ZDOT = 5874
483594 ZDOT = 1814
686644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14087208
55 X = 4293781
17
Y = 4551092
83 feet Y = 1387173
09 meter
Z = -16630956
36 Z = -5069115
50
XDOT = -468
582142 XDOT = -142
823837
YDOT = 23378
374969 feet/sec YDOT = 7125
728691 meter/sec
ZDOT = 5974
227986 ZDOT = 1820
944690
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 13037
51294222
00016717 00000-0 10270-3 0 9053
2 25544 51
6457 37
4425 0012744 244
2673 115
7164 15
52259137 14416
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
51294222 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 37
4425 deg
Eccentricity:
0012744
Arg of perigee: 244
2673 deg
Mean anomaly: 115
7164 deg
Mean motion: 15
52259137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 293
Coasting Arc #7 (Orbit 1456)
---------------------------------------
Vector Time (GMT): 2013/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4741216
99 A = 6785588
94 meter
Y = 1363660
09 meter E =
0004463
Z = 4662020
89 I = 51
82419
XDOT = -4460
296588 Wp = 253
86212
YDOT = -5496
911583 meter/sec RA = 31
94013 deg
ZDOT = -2931
733254 TA = 225
24632
MA = 225
28264
Ha = 223
642 n
mi
Hp = 219
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15555173
86 X = -4778759
64
Y = 4473950
41 feet Y = 1310430
86 meter
Z = 15295344
13 Z = 4638897
87
XDOT = -14633
518991 XDOT = -4384
256236
YDOT = -18034
486821 feet/sec YDOT = -5546
364220 meter/sec
ZDOT = -9618
547422 ZDOT = -2953
215820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14491860
96 X = -4417119
22
Y = -7409860
17 feet Y = -2258525
38 meter
Z = 15198919
58 Z = 4632630
69
XDOT = 1116
898570 XDOT = 340
430684
YDOT = -22071
629731 feet/sec YDOT = -6727
432742 meter/sec
ZDOT = -9707
217087 ZDOT = -2958
759768
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 13038
54299680
00016717 00000-0 10270-3 0 9061
2 25544 51
6449 32
3215 0012751 248
4383 111
5411 15
52294539 14571
Satellite: ISS
Catalog Number: 25544
Epoch time: 13038
54299680 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 32
3215 deg
Eccentricity:
0012751
Arg of perigee: 248
4383 deg
Mean anomaly: 111
5411 deg
Mean motion: 15
52294539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1457
Checksum: 306
Coasting Arc #8 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2013/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5416329
46 A = 6788005
31 meter
Y = -787322
19 meter E =
0008082
Z = -4014768
30 I = 51
80550
XDOT = 3729
092170 Wp = 222
79415
YDOT = 5396
169237 meter/sec RA = 26
97712 deg
ZDOT = 3962
233100 TA = 88
39156
MA = 88
29899
Ha = 223
275 n
mi
Hp = 219
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17770109
77 X = 5444233
03
Y = -2583078
04 feet Y = -726597
41 meter
Z = -13171812
01 Z = -3988389
21
XDOT = 12234
554362 XDOT = 3649
226985
YDOT = 17703
967313 feet/sec YDOT = 5437
423766 meter/sec
ZDOT = 12999
452429 ZDOT = 3980
154166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14985385
87 X = 4567545
61
Y = 10038444
83 feet Y = 3059717
98 meter
Z = -13061912
60 Z = -3981270
96
XDOT = -2102
597369 XDOT = -640
871678
YDOT = 20194
662579 feet/sec YDOT = 6155
333154 meter/sec
ZDOT = 13073
313022 ZDOT = 3984
745809
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 13039
50866667
00016717 00000-0 10270-3 0 9074
2 25544 51
6448 27
5206 0012660 252
2315 107
7456 15
52279839 14722
Satellite: ISS
Catalog Number: 25544
Epoch time: 13039
50866667 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 27
5206 deg
Eccentricity:
0012660
Arg of perigee: 252
2315 deg
Mean anomaly: 107
7456 deg
Mean motion: 15
52279839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 320
Coasting Arc #9 (Orbit 1487)
---------------------------------------
Vector Time (GMT): 2013/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5975941
46 A = 6790334
63 meter
Y = 305392
89 meter E =
0003952
Z = 3204989
02 I = 51
78591
XDOT = -2847
879241 Wp = 173
09714
YDOT = -5239
878574 meter/sec RA = 22
01659 deg
ZDOT = -4814
002424 TA = 329
96625
MA = 329
98891
Ha = 222
953 n
mi
Hp = 219
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19606107
16 X = -5994480
80
Y = 1001945
18 feet Y = 238462
60 meter
Z = 10515055
85 Z = 3175914
25
XDOT = -9343
435829 XDOT = -2765
689707
YDOT = -17191
202672 feet/sec YDOT = -5271
265953 meter/sec
ZDOT = -15793
971206 ZDOT = -4827
636967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15488817
96 X = -4720991
71
Y = -12166796
71 feet Y = -3708439
64 meter
Z = 10394003
45 Z = 3168092
25
XDOT = 3436
693534 XDOT = 1047
504189
YDOT = -17906
494655 feet/sec YDOT = -5457
899571 meter/sec
ZDOT = -15850
012793 ZDOT = -4831
083899
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 13040
53870678
00016717 00000-0 10270-3 0 9087
2 25544 51
6447 22
3995 0012741 256
6044 103
3688 15
52323051 14888
Satellite: ISS
Catalog Number: 25544
Epoch time: 13040
53870678 = yrday
fracday
Element set: 908
Inclination: 51
6447 deg
RA of node: 22
3995 deg
Eccentricity:
0012741
Arg of perigee: 256
6044 deg
Mean anomaly: 103
3688 deg
Mean motion: 15
52323051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1488
Checksum: 309
Coasting Arc #10 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2013/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6408686
49 A = 6792555
14 meter
Y = 123274
31 meter E =
0008559
Z = -2236415
79 I = 51
76471
XDOT = 1814
627305 Wp = 285
20366
YDOT = 5059
852542 meter/sec RA = 17
05844 deg
ZDOT = 5463
667266 TA = 49
99979
MA = 49
92470
Ha = 222
568 n
mi
Hp = 219
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21025874
31 X = 6417695
30
Y = 404443
27 feet Y = 194990
51 meter
Z = -7337322
14 Z = -2205261
97
XDOT = 5953
501658 XDOT = 1731
371820
YDOT = 16600
566084 feet/sec YDOT = 5079
679640 meter/sec
ZDOT = 17925
417540 ZDOT = 5472
279815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15861385
83 X = 4834550
40
Y = 13876349
20 feet Y = 4229511
24 meter
Z = -7207678
78 Z = -2196900
49
XDOT = -5207
420500 XDOT = -1587
221768
YDOT = 15307
918032 feet/sec YDOT = 4665
853416 meter/sec
ZDOT = 17960
582410 ZDOT = 5474
385519
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 13041
50436323
00016717 00000-0 10270-3 0 9091
2 25544 51
6449 17
5986 0012603 259
9091 100
0639 15
52318034 15034
Satellite: ISS
Catalog Number: 25544
Epoch time: 13041
50436323 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 17
5986 deg
Eccentricity:
0012603
Arg of perigee: 259
9091 deg
Mean anomaly: 100
0639 deg
Mean motion: 15
52318034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 289
Coasting Arc #11 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2013/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6667655
66 A = 6793977
40 meter
Y = -475729
99 meter E =
0008681
Z = 1182734
79 I = 51
74101
XDOT = -690
557729 Wp = 187
11343
YDOT = -4882
091569 meter/sec RA = 12
10165 deg
ZDOT = -5869
741414 TA = 340
06684
MA = 340
10073
Ha = 222
336 n
mi
Hp = 219
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21875510
70 X = -6667585
66
Y = -1560793
93 feet Y = -550291
42 meter
Z = 3880363
47 Z = 1150344
93
XDOT = -2265
609346 XDOT = -607
400916
YDOT = -16017
360791 feet/sec YDOT = -4889
349309 meter/sec
ZDOT = -19257
681805 ZDOT = -5872
893648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16011180
10 X = -4880207
70
Y = -15021439
16 feet Y = -4578534
66 meter
Z = 3745630
01 Z = 1141668
03
XDOT = 7340
456779 XDOT = 2237
371226
YDOT = -12618
136476 feet/sec YDOT = -3846
007998 meter/sec
ZDOT = -19270
146201 ZDOT = -5873
540562
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 13042
53438904
00016717 00000-0 10270-3 0 9104
2 25544 51
6457 12
4776 0012713 264
4262 95
5440 15
52341269 15198
Satellite: ISS
Catalog Number: 25544
Epoch time: 13042
53438904 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 12
4776 deg
Eccentricity:
0012713
Arg of perigee: 264
4262 deg
Mean anomaly: 95
5440 deg
Mean motion: 15
52341269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 296
Coasting Arc #12 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2013/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6741527
56 A = 6794467
87 meter
Y = 800322
26 meter E =
0008875
Z = -56272
51 I = 51
71285
XDOT = -507
327328 Wp = 332
27519
YDOT = 4722
787200 meter/sec RA = 7
14510 deg
ZDOT = 6016
322858 TA = 27
11975
MA = 27
07342
Ha = 222
109 n
mi
Hp = 219
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22117872
56 X = 6732350
49
Y = 2625729
19 feet Y = 875658
94 meter
Z = -184621
11 Z = -23545
83
XDOT = -1664
459737 XDOT = -589
325889
YDOT = 15494
708660 feet/sec YDOT = 4716
656003 meter/sec
ZDOT = 19738
592055 ZDOT = 6013
658772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15782540
69 X = 4810518
40
Y = 15717438
69 feet Y = 4790675
31 meter
Z = -48537
73 Z = -14794
30
XDOT = -9823
254310 XDOT = -2994
127914
YDOT = 9939
268822 feet/sec YDOT = 3029
489137 meter/sec
ZDOT = 19726
873577 ZDOT = 6012
751066
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 13043
50003138
00016717 00000-0 10270-3 0 9110
2 25544 51
6458 7
6770 0012678 267
3948 92
5752 15
52361785 15347
Satellite: ISS
Catalog Number: 25544
Epoch time: 13043
50003138 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 7
6770 deg
Eccentricity:
0012678
Arg of perigee: 267
3948 deg
Mean anomaly: 92
5752 deg
Mean motion: 15
52361785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 311
Coasting Arc #13 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2013/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6616140
73 A = 6793966
66 meter
Y = -1089814
86 meter E =
0009821
Z = -1058617
60 I = 51
68185
XDOT = 1704
296432 Wp = 224
15179
YDOT = -4596
087801 meter/sec RA = 2
18658 deg
ZDOT = -5893
916014 TA = 327
31290
MA = 327
37364
Ha = 222
137 n
mi
Hp = 219
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21706498
44 X = -6598320
07
Y = -3575508
07 feet Y = -1163701
16 meter
Z = -3473154
86 Z = -1090714
28
XDOT = 5591
523728 XDOT = 1784
194761
YDOT = -15079
028220 feet/sec YDOT = -4576
583099 meter/sec
ZDOT = -19336
994797 ZDOT = -5885
442344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15131199
49 X = -4611989
60
Y = -15939215
77 feet Y = -4858272
97 meter
Z = -3606569
02 Z = -1099282
24
XDOT = 12492
839739 XDOT = 3807
817552
YDOT = -7473
642143 feet/sec YDOT = -2277
966125 meter/sec
ZDOT = -19301
119328 ZDOT = -5882
981171
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 13044
53004245
00016717 00000-0 10270-3 0 9125
2 25544 51
6469 2
5565 0012759 272
0447 87
9243 15
52359187 15506
Satellite: ISS
Catalog Number: 25544
Epoch time: 13044
53004245 = yrday
fracday
Element set: 912
Inclination: 51
6469 deg
RA of node: 2
5565 deg
Eccentricity:
0012759
Arg of perigee: 272
0447 deg
Mean anomaly: 87
9243 deg
Mean motion: 15
52359187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 305
Coasting Arc #14 (Orbit 1565)
---------------------------------------
Vector Time (GMT): 2013/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6287760
89 A = 6792390
49 meter
Y = 1395088
50 meter E =
0005751
Z = 2145844
85 I = 51
64634
XDOT = -2873
586116 Wp = 3
29899
YDOT = 4497
370004 meter/sec RA = 357
22423 deg
ZDOT = 5501
168569 TA = 20
47154
MA = 20
44849
Ha = 222
158 n
mi
Hp = 219
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20629136
77 X = 6261269
60
Y = 4577062
02 feet Y = 1465254
26 meter
Z = 7040173
38 Z = 2176325
33
XDOT = -9427
775971 XDOT = -2950
385913
YDOT = 14755
150933 feet/sec YDOT = 4464
806827 meter/sec
ZDOT = 18048
453312 ZDOT = 5487
022208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13924525
68 X = 4244195
43
Y = 15837272
25 feet Y = 4827200
58 meter
Z = 7166813
40 Z = 2184444
73
XDOT = -15251
241506 XDOT = -4648
578411
YDOT = 5275
856639 feet/sec YDOT = 1608
081104 meter/sec
ZDOT = 17988
989025 ZDOT = 5483
043855
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 13045
56004512
00016717 00000-0 10270-3 0 9137
2 25544 51
6470 357
4358 0012780 275
5230 84
4464 15
52382274 15669
Satellite: ISS
Catalog Number: 25544
Epoch time: 13045
56004512 = yrday
fracday
Element set: 913
Inclination: 51
6470 deg
RA of node: 357
4358 deg
Eccentricity:
0012780
Arg of perigee: 275
5230 deg
Mean anomaly: 84
4464 deg
Mean motion: 15
52382274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1566
Checksum: 300
Coasting Arc #15 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2013/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5779409
10 A = 6790173
10 meter
Y = -1710172
80 meter E =
0008275
Z = -3121545
64 I = 51
60903
XDOT = 3941
741623 Wp = 277
69033
YDOT = -4423
898216 meter/sec RA = 352
25631 deg
ZDOT = -4862
141088 TA = 298
23692
MA = 298
32044
Ha = 222
436 n
mi
Hp = 219
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18961315
94 X = -5744692
60
Y = -5610803
14 feet Y = -1774607
90 meter
Z = -10241291
46 Z = -3149536
70
XDOT = 12932
223174 XDOT = 4014
536321
YDOT = -14514
101758 feet/sec YDOT = -4379
412530 meter/sec
ZDOT = -15951
906456 ZDOT = -4842
815547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12219833
60 X = -3724605
28
Y = -15469131
14 feet Y = -4714991
17 meter
Z = -10357524
49 Z = -3156973
47
XDOT = 17883
184710 XDOT = 5450
794700
YDOT = -3473
897258 feet/sec YDOT = -1058
843884 meter/sec
ZDOT = -15870
905335 ZDOT = -4837
451946
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 13046
52566642
00016717 00000-0 10270-3 0 9142
2 25544 51
6475 352
6354 0012800 279
7963 80
1743 15
52389565 15819
Satellite: ISS
Catalog Number: 25544
Epoch time: 13046
52566642 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node: 352
6354 deg
Eccentricity:
0012800
Arg of perigee: 279
7963 deg
Mean anomaly: 80
1743 deg
Mean motion: 15
52389565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 325
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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