[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 3rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 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
348/14:46:55
238 -1
2 1
6 1
6
N/A -0
1 -0
1 230
2
000/00:07:50
475 -1
0 -0
0 213
7
Coasting Arc #1 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2012/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3380691
81 A = 6786844
27 meter
Y = 3657379
58 meter E =
0021079
Z = 4613969
68 I = 51
64022
XDOT = -6651
494388 Wp = 20
03322
YDOT = -2351
991280 meter/sec RA = 359
90411 deg
ZDOT = -2985
819464 TA = 99
89053
MA = 99
65251
Ha = 228
903 n
mi
Hp = 215
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11091508
57 X = -3443751
86
Y = 11999276
84 feet Y = 3619221
66 meter
Z = 15137695
79 Z = 4597393
44
XDOT = -21822
488151 XDOT = -6610
195071
YDOT = -7716
506825 feet/sec YDOT = -2426
141324 meter/sec
ZDOT = -9795
995618 ZDOT = -3018
032117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7934325
37 X = -2418382
37
Y = -14357640
03 feet Y = -4376208
68 meter
Z = 15068466
90 Z = 4592868
71
XDOT = 13046
112221 XDOT = 3976
455005
YDOT = -17711
367599 feet/sec YDOT = -5398
424844 meter/sec
ZDOT = -9929
233753 ZDOT = -3026
430448
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 12338
54292141
00016717 00000-0 10270-3 0 9002
2 25544 51
6473
2407 0016295 358
6771 1
4335 15
51921618 4325
Satellite: ISS
Catalog Number: 25544
Epoch time: 12338
54292141 = yrday
fracday
Element set: 900
Inclination: 51
6473 deg
RA of node:
2407 deg
Eccentricity:
0016295
Arg of perigee: 358
6771 deg
Mean anomaly: 1
4335 deg
Mean motion: 15
51921618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 281
Coasting Arc #2 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2012/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4066108
21 A = 6788868
08 meter
Y = -3598126
79 meter E =
0015955
Z = -4071389
75 I = 51
61752
XDOT = 6106
913215 Wp = 27
27832
YDOT = 2539
517703 meter/sec RA = 354
93264 deg
ZDOT = 3874
542471 TA = 282
78539
MA = 282
96363
Ha = 229
093 n
mi
Hp = 215
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13340250
02 X = 4125818
98
Y = -11804877
92 feet Y = -3552322
94 meter
Z = -13357577
92 Z = -4051491
86
XDOT = 20035
804511 XDOT = 6059
240187
YDOT = 8331
750993 feet/sec YDOT = 2607
542258 meter/sec
ZDOT = 12711
753515 ZDOT = 3904
094039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7336035
73 X = 2236023
69
Y = 16300619
56 feet Y = 4968428
84 meter
Z = -13274587
86 Z = -4046094
38
XDOT = -12645
213198 XDOT = -3854
260983
YDOT = 16088
957818 feet/sec YDOT = 4903
914343 meter/sec
ZDOT = 12833
930998 ZDOT = 3911
782168
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 12339
50883836
00016717 00000-0 10270-3 0 9017
2 25544 51
6485 355
4423 0016366 2
2765 357
8459 15
51904253 4472
Satellite: ISS
Catalog Number: 25544
Epoch time: 12339
50883836 = yrday
fracday
Element set: 901
Inclination: 51
6485 deg
RA of node: 355
4423 deg
Eccentricity:
0016366
Arg of perigee: 2
2765 deg
Mean anomaly: 357
8459 deg
Mean motion: 15
51904253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 323
Coasting Arc #3 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2012/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4744030
96 A = 6791026
88 meter
Y = 3531224
96 meter E =
0021444
Z = 3342939
34 I = 51
59354
XDOT = -5392
397060 Wp = 41
50063
YDOT = -2799
265207 meter/sec RA = 349
96108 deg
ZDOT = -4662
609059 TA = 99
59956
MA = 99
35721
Ha = 229
148 n
mi
Hp = 214
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15564406
03 X = -4799404
59
Y = 11585383
72 feet Y = 3477864
49 meter
Z = 10967648
74 Z = 3319758
58
XDOT = -17691
591403 XDOT = -5338
044299
YDOT = -9183
940967 feet/sec YDOT = -2859
262268 meter/sec
ZDOT = -15297
273815 ZDOT = -4688
673301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6790902
99 X = -2069867
23
Y = -18233618
30 feet Y = -5557606
86 meter
Z = 10871061
13 Z = 3313499
43
XDOT = 12379
897584 XDOT = 3773
392784
YDOT = -13860
298659 feet/sec YDOT = -4224
619031 meter/sec
ZDOT = -15404
954862 ZDOT = -4695
430242
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 12340
53913857
00016717 00000-0 10270-3 0 9020
2 25544 51
6472 350
3227 0016435 6
1662 353
9689 15
51954069 4630
Satellite: ISS
Catalog Number: 25544
Epoch time: 12340
53913857 = yrday
fracday
Element set: 902
Inclination: 51
6472 deg
RA of node: 350
3227 deg
Eccentricity:
0016435
Arg of perigee: 6
1662 deg
Mean anomaly: 353
9689 deg
Mean motion: 15
51954069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 314
Coasting Arc #4 (Orbit 477)
---------------------------------------
Vector Time (GMT): 2012/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5227146
81 A = 6792963
03 meter
Y = -3493571
92 meter E =
0020720
Z = -2546995
85 I = 51
57085
XDOT = 4625
788689 Wp = 18
96655
YDOT = 3095
723090 meter/sec RA = 344
99219 deg
ZDOT = 5278
398543 TA = 312
39385
MA = 312
56902
Ha = 229
271 n
mi
Hp = 214
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17149431
78 X = 5278196
98
Y = -11461850
13 feet Y = -3434833
18 meter
Z = -8356285
60 Z = -2521478
54
XDOT = 15176
472076 XDOT = 4565
186410
YDOT = 10156
571819 feet/sec YDOT = 3147
112539 meter/sec
ZDOT = 17317
580523 ZDOT = 5300
723473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6574510
44 X = 2003910
78
Y = 19596364
19 feet Y = 5972971
80 meter
Z = -8250021
27 Z = -2514606
48
XDOT = -12310
764991 XDOT = -3752
321169
YDOT = 11415
989985 feet/sec YDOT = 3479
593747 meter/sec
ZDOT = 17409
715669 ZDOT = 5306
481336
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 12341
50503672
00016717 00000-0 10270-3 0 9039
2 25544 51
6478 345
5247 0016386 10
0094 350
1381 15
51958338 4789
Satellite: ISS
Catalog Number: 25544
Epoch time: 12341
50503672 = yrday
fracday
Element set: 903
Inclination: 51
6478 deg
RA of node: 345
5247 deg
Eccentricity:
0016386
Arg of perigee: 10
0094 deg
Mean anomaly: 350
1381 deg
Mean motion: 15
51958338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 478
Checksum: 302
Coasting Arc #5 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2012/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5657509
02 A = 6794554
48 meter
Y = 3410619
89 meter E =
0018861
Z = 1602407
64 I = 51
54594
XDOT = -3728
729805 Wp = 58
60129
YDOT = -3472
653019 meter/sec RA = 340
02266 deg
ZDOT = -5713
957133 TA = 103
87981
MA = 103
66991
Ha = 229
366 n
mi
Hp = 214
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18561381
29 X = -5703011
02
Y = 11189697
80 feet Y = 3347099
62 meter
Z = 5257242
92 Z = 1574813
01
XDOT = -12233
365501 XDOT = -3661
863339
YDOT = -11393
218567 feet/sec YDOT = -3513
975973 meter/sec
ZDOT = -18746
578521 ZDOT = -5731
909003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6306056
87 X = -1922086
13
Y = -20764449
29 feet Y = -6329004
14 meter
Z = 5142383
46 Z = 1567398
48
XDOT = 12496
683614 XDOT = 3808
989166
YDOT = -8505
564011 feet/sec YDOT = -2592
495911 meter/sec
ZDOT = -18820
530258 ZDOT = -5736
497623
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 12342
53531732
00016717 00000-0 10270-3 0 9042
2 25544 51
6465 340
4047 0016543 13
5336 346
6256 15
51975443 4944
Satellite: ISS
Catalog Number: 25544
Epoch time: 12342
53531732 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 340
4047 deg
Eccentricity:
0016543
Arg of perigee: 13
5336 deg
Mean anomaly: 346
6256 deg
Mean motion: 15
51975443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 300
Coasting Arc #6 (Orbit 508)
---------------------------------------
Vector Time (GMT): 2012/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5880722
80 A = 6795336
50 meter
Y = -3310386
19 meter E =
0026546
Z = -655858
44 I = 51
52046
XDOT = 2849
270910 Wp = 26
19508
YDOT = 3902
851031 meter/sec RA = 335
05435 deg
ZDOT = 5963
934890 TA = 326
70700
MA = 326
87370
Ha = 229
349 n
mi
Hp = 214
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19293709
99 X = 5920489
22
Y = -10860847
09 feet Y = -3244401
90 meter
Z = -2151766
53 Z = -627193
28
XDOT = 9348
001673 XDOT = 2776
444799
YDOT = 12804
629367 feet/sec YDOT = 3934
305959 meter/sec
ZDOT = 19566
715518 ZDOT = 5977
599950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6179463
37 X = 1883500
44
Y = 21272483
87 feet Y = 6483853
08 meter
Z = -2032487
64 Z = -619502
23
XDOT = -13019
590079 XDOT = -3968
371056
YDOT = 5618
655492 feet/sec YDOT = 1712
566194 meter/sec
ZDOT = 19622
835307 ZDOT = 5981
040202
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 12343
50119624
00016717 00000-0 10270-3 0 9053
2 25544 51
6464 335
6064 0016351 17
3723 342
7985 15
52011143 5099
Satellite: ISS
Catalog Number: 25544
Epoch time: 12343
50119624 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 335
6064 deg
Eccentricity:
0016351
Arg of perigee: 17
3723 deg
Mean anomaly: 342
7985 deg
Mean motion: 15
52011143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 509
Checksum: 286
Coasting Arc #7 (Orbit 524)
---------------------------------------
Vector Time (GMT): 2012/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6029847
31 A = 6795448
23 meter
Y = 3122921
63 meter E =
0015234
Z = -377717
43 I = 51
49289
XDOT = -1908
203065 Wp = 61
19475
YDOT = -4385
608450 meter/sec RA = 330
08334 deg
ZDOT = -5973
731362 TA = 122
87509
MA = 122
72838
Ha = 229
557 n
mi
Hp = 213
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19782963
63 X = -6062485
43
Y = 10245805
89 feet Y = 3055309
64 meter
Z = -1239230
41 Z = -407089
75
XDOT = -6260
508745 XDOT = -1830
000938
YDOT = -14388
479168 feet/sec YDOT = -4406
509610 meter/sec
ZDOT = -19598
856175 ZDOT = -5982
811750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5844222
78 X = -1781319
10
Y = -21491149
27 feet Y = -6550502
30 meter
Z = -1361412
29 Z = -414958
47
XDOT = 13794
060653 XDOT = 4204
429687
YDOT = -2540
597237 feet/sec YDOT = -774
374038 meter/sec
ZDOT = -19635
903165 ZDOT = -5985
023285
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 12344
53145683
00016717 00000-0 10270-3 0 9062
2 25544 51
6457 330
4860 0016626 20
7639 339
4184 15
51996110 5254
Satellite: ISS
Catalog Number: 25544
Epoch time: 12344
53145683 = yrday
fracday
Element set: 906
Inclination: 51
6457 deg
RA of node: 330
4860 deg
Eccentricity:
0016626
Arg of perigee: 20
7639 deg
Mean anomaly: 339
4184 deg
Mean motion: 15
51996110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 525
Checksum: 310
Coasting Arc #8 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2012/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5989699
02 A = 6794599
99 meter
Y = -2871057
54 meter E =
0028726
Z = 1344714
48 I = 51
46423
XDOT = 1040
694894 Wp = 40
37804
YDOT = 4914
115163 meter/sec RA = 325
11113 deg
ZDOT = 5808
396206 TA = 334
31657
MA = 334
45896
Ha = 229
426 n
mi
Hp = 213
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19651243
52 X = 6014826
19
Y = -9419480
12 feet Y = -2803936
59 meter
Z = 4411792
92 Z = 1373873
48
XDOT = 3414
353326 XDOT = 957
450519
YDOT = 16122
425077 feet/sec YDOT = 4925
286972 meter/sec
ZDOT = 19056
417999 ZDOT = 5813
250118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5431541
58 X = 1655533
87
Y = 21078701
47 feet Y = 6424788
21 meter
Z = 4533055
77 Z = 1381675
40
XDOT = -14920
058013 XDOT = -4547
633682
YDOT = -290
752164 feet/sec YDOT = -88
621260 meter/sec
ZDOT = 19075
871589 ZDOT = 5814
325660
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 12345
56170498
00016717 00000-0 10270-3 0 9079
2 25544 51
6454 325
3672 0016383 24
5339 335
6589 15
52044285 5417
Satellite: ISS
Catalog Number: 25544
Epoch time: 12345
56170498 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 325
3672 deg
Eccentricity:
0016383
Arg of perigee: 24
5339 deg
Mean anomaly: 335
6589 deg
Mean motion: 15
52044285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 320
Coasting Arc #9 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2012/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5884690
59 A = 6793096
13 meter
Y = 2503098
95 meter E =
0016037
Z = -2321390
95 I = 51
43479
XDOT = -191
963301 Wp = 47
36651
YDOT = -5430
850561 meter/sec RA = 320
13377 deg
ZDOT = -5382
519198 TA = 158
50775
MA = 158
44034
Ha = 229
719 n
mi
Hp = 213
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19306727
65 X = -5900966
43
Y = 8212266
89 feet Y = 2437201
90 meter
Z = -7616112
04 Z = -2350018
23
XDOT = -629
800855 XDOT = -105
072658
YDOT = -17817
751185 feet/sec YDOT = -5432
510816 meter/sec
ZDOT = -17659
183720 ZDOT = -5383
241274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4669502
21 X = -1423264
27
Y = -20409797
86 feet Y = -6220906
39 meter
Z = -7735122
71 Z = -2357665
40
XDOT = 16141
177702 XDOT = 4919
830964
YDOT = 2984
475448 feet/sec YDOT = 909
668117 meter/sec
ZDOT = -17661
438351 ZDOT = -5383
206409
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 12346
52755640
00016717 00000-0 10270-3 0 9085
2 25544 51
6455 320
5665 0016700 27
8978 332
3066 15
52025133 5566
Satellite: ISS
Catalog Number: 25544
Epoch time: 12346
52755640 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 320
5665 deg
Eccentricity:
0016700
Arg of perigee: 27
8978 deg
Mean anomaly: 332
3066 deg
Mean motion: 15
52025133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 305
Coasting Arc #10 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2012/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5631449
14 A = 6790980
20 meter
Y = -2035991
91 meter E =
0025988
Z = 3167209
08 I = 51
40550
XDOT = -555
002873 Wp = 54
76392
YDOT = 5963
834493 meter/sec RA = 315
15336 deg
ZDOT = 4807
405678 TA = 341
97708
MA = 342
06905
Ha = 229
531 n
mi
Hp = 213
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18475883
00 X = 5638411
73
Y = -6679763
47 feet Y = -1972979
00 meter
Z = 10391105
90 Z = 3194583
36
XDOT = -1820
875569 XDOT = -645
004015
YDOT = 19566
386133 feet/sec YDOT = 5957
124265 meter/sec
ZDOT = 15772
328339 ZDOT = 4804
491618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3642827
58 X = 1110333
85
Y = 19243966
32 feet Y = 5865560
93 meter
Z = 10504862
78 Z = 3201882
18
XDOT = -17604
196215 XDOT = -5365
759006
YDOT = -5293
651835 feet/sec YDOT = -1613
505079 meter/sec
ZDOT = 15759
437456 ZDOT = 4803
476537
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 12347
55778425
00016717 00000-0 10270-3 0 9096
2 25544 51
6457 315
4476 0016470 31
4383 328
7750 15
52067435 5724
Satellite: ISS
Catalog Number: 25544
Epoch time: 12347
55778425 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 315
4476 deg
Eccentricity:
0016470
Arg of perigee: 31
4383 deg
Mean anomaly: 328
7750 deg
Mean motion: 15
52067435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 324
Coasting Arc #11 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2012/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5350188
72 A = 6788711
53 meter
Y = 1453063
12 meter E =
0022432
Z = -3944296
30 I = 51
37736
XDOT = 1214
923509 Wp = 45
31723
YDOT = -6398
836828 meter/sec RA = 310
16633 deg
ZDOT = -4003
935698 TA = 182
58525
MA = 182
59686
Ha = 229
839 n
mi
Hp = 213
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17553112
60 X = -5346878
95
Y = 4767267
46 feet Y = 1393253
02 meter
Z = -12940604
67 Z = -3970279
16
XDOT = 3985
969519 XDOT = 1305
836648
YDOT = -20993
559147 feet/sec YDOT = -6384
741918 meter/sec
ZDOT = -13136
271974 ZDOT = -3997
813683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2214742
29 X = -675053
45
Y = -17975787
03 feet Y = -5479019
89 meter
Z = -13048518
97 Z = -3977188
58
XDOT = 18884
871554 XDOT = 5756
108850
YDOT = 7192
901969 feet/sec YDOT = 2192
396520 meter/sec
ZDOT = -13110
025527 ZDOT = -3995
935781
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 12348
52361602
00016717 00000-0 10270-3 0 9101
2 25544 51
6462 310
6472 0016716 34
9851 325
2396 15
52053088 5877
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
52361602 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 310
6472 deg
Eccentricity:
0016716
Arg of perigee: 34
9851 deg
Mean anomaly: 325
2396 deg
Mean motion: 15
52053088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 587
Checksum: 302
Coasting Arc #12 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2012/348/14:50:50
475
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3793202
61 A = 6796000
93 meter
Y = 5584569
87 meter E =
0021253
Z = 789523
45 I = 51
39819
XDOT = -4376
866565 Wp = 77
38048
YDOT = -2116
775575 meter/sec RA = 309
54274 deg
ZDOT = -5915
856855 TA = 94
07174
MA = 93
82878
Ha = 230
169 n
mi
Hp = 213
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12444890
46 X = -3859203
87
Y = 18322079
62 feet Y = 5541782
76 meter
Z = 2590300
03 Z = 770936
63
XDOT = -14359
798440 XDOT = -4324
133040
YDOT = -6944
801756 feet/sec YDOT = -2165
424767 meter/sec
ZDOT = -19408
979183 ZDOT = -5936
991757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22157391
06 X = -6753572
80
Y = 144838
39 feet Y = 44146
74 meter
Z = 2512488
34 Z = 765806
45
XDOT = -2356
195972 XDOT = -718
168532
YDOT = -14050
616563 feet/sec YDOT = -4282
627928 meter/sec
ZDOT = -19496
312676 ZDOT = -5942
476104
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 12348
65240117
00016717 00000-0 10270-3 0 9113
2 25544 51
6481 310
0083 0016073 39
1423 321
0888 15
51749473 5899
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
65240117 = yrday
fracday
Element set: 911
Inclination: 51
6481 deg
RA of node: 310
0083 deg
Eccentricity:
0016073
Arg of perigee: 39
1423 deg
Mean anomaly: 321
0888 deg
Mean motion: 15
51749473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 296
Coasting Arc #13 (Orbit 604)
---------------------------------------
Vector Time (GMT): 2012/349/14:50:50
475
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3912604
71 A = 6796238
51 meter
Y = -5538757
38 meter E =
0028445
Z = 99591
05 I = 51
38031
XDOT = 3853
315930 Wp = 43
97683
YDOT = 2847
947794 meter/sec RA = 304
56536 deg
ZDOT = 5994
722855 TA = 317
10010
MA = 317
32164
Ha = 230
214 n
mi
Hp = 213
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12836629
61 X = 3973765
67
Y = -18171776
19 feet Y = -5494662
23 meter
Z = 326742
30 Z = 118746
09
XDOT = 12642
112631 XDOT = 3792
062268
YDOT = 9343
660741 feet/sec YDOT = 2890
694707 meter/sec
ZDOT = 19667
725903 ZDOT = 6013
293629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22246699
77 X = 6780794
09
Y = -134351
96 feet Y = -40950
48 meter
Z = 406901
78 Z = 124023
66
XDOT = -325
252578 XDOT = -99
136986
YDOT = 13998
502367 feet/sec YDOT = 4266
743521 meter/sec
ZDOT = 19744
337879 ZDOT = 6018
074185
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 12349
68280481
00016717 00000-0 10270-3 0 9126
2 25544 51
6481 304
8905 0016136 42
5548 317
6851 15
51756294 6058
Satellite: ISS
Catalog Number: 25544
Epoch time: 12349
68280481 = yrday
fracday
Element set: 912
Inclination: 51
6481 deg
RA of node: 304
8905 deg
Eccentricity:
0016136
Arg of perigee: 42
5548 deg
Mean anomaly: 317
6851 deg
Mean motion: 15
51756294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 605
Checksum: 318
Coasting Arc #14 (Orbit 619)
---------------------------------------
Vector Time (GMT): 2012/350/14:50:50
475
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4033262
56 A = 6795665
03 meter
Y = 5369593
17 meter E =
0017837
Z = -1071123
16 I = 51
36293
XDOT = -3315
592560 Wp = 77
93966
YDOT = -3642
990429 meter/sec RA = 299
58652 deg
ZDOT = -5857
208280 TA = 113
69335
MA = 113
50608
Ha = 230
234 n
mi
Hp = 213
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13232488
72 X = -4087803
48
Y = 17616775
49 feet Y = 5324185
87 meter
Z = -3514183
61 Z = -1090848
30
XDOT = -10877
928346 XDOT = -3246
156668
YDOT = -11952
068338 feet/sec YDOT = -3679
678560 meter/sec
ZDOT = -19216
562597 ZDOT = -5873
146916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22019297
60 X = -6711481
91
Y = -115976
31 feet Y = -35349
58 meter
Z = -3596679
78 Z = -1096268
00
XDOT = 3182
571946 XDOT = 970
047929
YDOT = -14157
354467 feet/sec YDOT = -4315
161642 meter/sec
ZDOT = -19282
164139 ZDOT = -5877
203629
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 12350
64879767
00016717 00000-0 10270-3 0 9136
2 25544 51
6488 300
0920 0016032 46
3735 313
8743 15
51772779 6206
Satellite: ISS
Catalog Number: 25544
Epoch time: 12350
64879767 = yrday
fracday
Element set: 913
Inclination: 51
6488 deg
RA of node: 300
0920 deg
Eccentricity:
0016032
Arg of perigee: 46
3735 deg
Mean anomaly: 313
8743 deg
Mean motion: 15
51772779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 620
Checksum: 316
Coasting Arc #15 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2012/351/14:50:50
475
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4034264
20 A = 6794526
95 meter
Y = -5091570
56 meter E =
0029724
Z = 1935282
80 I = 51
34475
XDOT = 2881
572268 Wp = 57
85314
YDOT = 4420
848386 meter/sec RA = 294
60547 deg
ZDOT = 5576
676203 TA = 323
59214
MA = 323
79394
Ha = 230
254 n
mi
Hp = 213
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13235774
94 X = 4081498
30
Y = -16704627
81 feet Y = -5046192
96 meter
Z = 6349353
00 Z = 1954995
17
XDOT = 9453
977256 XDOT = 2804
833262
YDOT = 14504
095753 feet/sec YDOT = 4452
642357 meter/sec
ZDOT = 18296
181768 ZDOT = 5590
488625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21286089
86 X = 6488000
19
Y = 282029
57 feet Y = 85962
61 meter
Z = 6431753
27 Z = 1960398
40
XDOT = -5786
467231 XDOT = -1763
715212
YDOT = 14694
242874 feet/sec YDOT = 4478
805228 meter/sec
ZDOT = 18352
874594 ZDOT = 5593
956176
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 12351
67918094
00016717 00000-0 10270-3 0 9148
2 25544 51
6486 294
9742 0016168 49
8820 310
3746 15
51787674 6362
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
67918094 = yrday
fracday
Element set: 914
Inclination: 51
6486 deg
RA of node: 294
9742 deg
Eccentricity:
0016168
Arg of perigee: 49
8820 deg
Mean anomaly: 310
3746 deg
Mean motion: 15
51787674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 636
Checksum: 344
Coasting Arc #16 (Orbit 650)
---------------------------------------
Vector Time (GMT): 2012/352/14:50:50
475
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4060085
01 A = 6792671
76 meter
Y = 4675955
94 meter E =
0018457
Z = -2816413
94 I = 51
32743
XDOT = -2459
675223 Wp = 66
35924
YDOT = -5175
557333 meter/sec RA = 289
62102 deg
ZDOT = -5066
173350 TA = 145
66423
MA = 145
54479
Ha = 230
268 n
mi
Hp = 212
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13320488
88 X = -4098389
39
Y = 15341062
80 feet Y = 4630339
55 meter
Z = -9240203
23 Z = -2836230
20
XDOT = -8069
800599 XDOT = -2377
008131
YDOT = -16980
174978 feet/sec YDOT = -5202
600395 meter/sec
ZDOT = -16621
303641 ZDOT = -5077
921798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20262731
60 X = -6176080
59
Y = -817840
91 feet Y = -249277
91 meter
Z = -9322973
33 Z = -2841642
27
XDOT = 8259
739053 XDOT = 2517
568463
YDOT = -15334
214167 feet/sec YDOT = -4673
868478 meter/sec
ZDOT = -16669
350463 ZDOT = -5080
818021
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 12352
64515443
00016717 00000-0 10270-3 0 9158
2 25544 51
6489 290
1756 0015998 53
3454 306
9166 15
51807577 6510
Satellite: ISS
Catalog Number: 25544
Epoch time: 12352
64515443 = yrday
fracday
Element set: 915
Inclination: 51
6489 deg
RA of node: 290
1756 deg
Eccentricity:
0015998
Arg of perigee: 53
3454 deg
Mean anomaly: 306
9166 deg
Mean motion: 15
51807577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 651
Checksum: 332
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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