[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 21st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
358/11:40:00
773 -0
5 1
6 1
6
N/A -1
5 -0
1 230
5
000/00:04:01
546 -0
0 0
1 212
5
Coasting Arc #1 (Orbit 679)
---------------------------------------
Vector Time (GMT): 2012/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3372105
38 A = 6785608
31 meter
Y = -3331691
13 meter E =
0026884
Z = -4876290
89 I = 51
28772
XDOT = 3105
783441 Wp = 79
11966
YDOT = -6576
955211 meter/sec RA = 280
19059 deg
ZDOT = 2362
028787 TA = 214
11197
MA = 214
28503
Ha = 230
593 n
mi
Hp = 212
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11063337
85 X = -3310911
27
Y = -10930745
19 feet Y = -3369057
74 meter
Z = -15998329
69 Z = -4892523
88
XDOT = 10189
578220 XDOT = 3167
623356
YDOT = -21577
937043 feet/sec YDOT = -6541
878743 meter/sec
ZDOT = 7749
438277 ZDOT = 2377
266372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11366853
58 X = 3464616
97
Y = -10513253
58 feet Y = -3204439
69 meter
Z = -16065221
03 Z = -4896679
37
XDOT = 20382
450909 XDOT = 6212
571037
YDOT = 10178
144361 feet/sec YDOT = 3102
298401 meter/sec
ZDOT = 7813
450279 ZDOT = 2381
539645
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 12354
51194519
00016717 00000-0 10270-3 0 9007
2 25544 51
6473 280
9037 0017280 60
3655 299
9215 15
51938758 6803
Satellite: ISS
Catalog Number: 25544
Epoch time: 12354
51194519 = yrday
fracday
Element set: 900
Inclination: 51
6473 deg
RA of node: 280
9037 deg
Eccentricity:
0017280
Arg of perigee: 60
3655 deg
Mean anomaly: 299
9215 deg
Mean motion: 15
51938758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 324
Coasting Arc #2 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2012/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3133732
38 A = 6787468
84 meter
Y = 4135223
24 meter E =
0026702
Z = 4361029
24 I = 51
28976
XDOT = -3268
782043 Wp = 66
47010
YDOT = 6066
747699 meter/sec RA = 275
19255 deg
ZDOT = -3376
788015 TA = 57
98516
MA = 57
72599
Ha = 230
541 n
mi
Hp = 212
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10281274
21 X = 3066073
67
Y = 13567005
37 feet Y = 4169888
08 meter
Z = 14307838
70 Z = 4376088
60
XDOT = -10724
350535 XDOT = -3319
975100
YDOT = 19904
027884 feet/sec YDOT = 6029
908059 meter/sec
ZDOT = -11078
700837 ZDOT = -3392
791641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13801779
93 X = -4206782
52
Y = 9874366
20 feet Y = 3009706
82 meter
Z = 14369768
45 Z = 4379905
43
XDOT = -18929
571656 XDOT = -5769
733441
YDOT = -10110
335029 feet/sec YDOT = -3081
630117 meter/sec
ZDOT = -11145
818540 ZDOT = -3397
245491
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 12355
54221774
00016717 00000-0 10270-3 0 9016
2 25544 51
6473 275
7846 0017280 64
3363 295
9571 15
51973368 6967
Satellite: ISS
Catalog Number: 25544
Epoch time: 12355
54221774 = yrday
fracday
Element set: 901
Inclination: 51
6473 deg
RA of node: 275
7846 deg
Eccentricity:
0017280
Arg of perigee: 64
3363 deg
Mean anomaly: 295
9571 deg
Mean motion: 15
51973368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 337
Coasting Arc #3 (Orbit 710)
---------------------------------------
Vector Time (GMT): 2012/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2994688
28 A = 6789458
52 meter
Y = -4807683
26 meter E =
0022378
Z = -3758035
42 I = 51
29544
XDOT = 3402
556863 Wp = 76
56553
YDOT = -5399
918103 meter/sec RA = 270
19753 deg
ZDOT = 4223
134018 TA = 238
32531
MA = 238
54374
Ha = 230
526 n
mi
Hp = 211
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9825092
79 X = -2922449
48
Y = -15773239
03 feet Y = -4840767
62 meter
Z = -12329512
54 Z = -3772408
30
XDOT = 11163
244302 XDOT = 3442
171948
YDOT = -17716
266741 feet/sec YDOT = -5361
647318 meter/sec
ZDOT = 13855
426568 ZDOT = 4239
759424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15833232
37 X = 4825969
23
Y = -9652863
22 feet Y = -2942192
71 meter
Z = -12388518
15 Z = -3776020
33
XDOT = 16943
548403 XDOT = 5164
393553
YDOT = 10031
038144 feet/sec YDOT = 3057
460426 meter/sec
ZDOT = 13925
035612 ZDOT = 4244
350854
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 12356
50807731
00016717 00000-0 10270-3 0 9027
2 25544 51
6476 270
9853 0017248 67
8382 292
4598 15
52014340 7114
Satellite: ISS
Catalog Number: 25544
Epoch time: 12356
50807731 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 270
9853 deg
Eccentricity:
0017248
Arg of perigee: 67
8382 deg
Mean anomaly: 292
4598 deg
Mean motion: 15
52014340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 711
Checksum: 315
Coasting Arc #4 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2012/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890854
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2808008
87 A = 6791773
09 meter
Y = 5436837
27 meter E =
0029667
Z = 2925941
90 I = 51
30411
XDOT = -3619
933969 Wp = 83
00300
YDOT = 4575
424312 meter/sec RA = 265
20566 deg
ZDOT = -4980
666156 TA = 63
44339
MA = 63
13960
Ha = 230
519 n
mi
Hp = 211
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9212627
52 X = 2732790
72
Y = 17837392
63 feet Y = 5467817
42 meter
Z = 9599546
91 Z = 2939400
78
XDOT = -11876
423784 XDOT = -3646
633278
YDOT = 15011
234620 feet/sec YDOT = 4534
795000 meter/sec
ZDOT = -16340
768229 ZDOT = -4998
316215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17735296
52 X = -5405718
38
Y = 9351073
48 feet Y = 2850207
20 meter
Z = 9654691
34 Z = 2942749
92
XDOT = -14458
058137 XDOT = -4406
816120
YDOT = -10315
024079 feet/sec YDOT = -3144
019339 meter/sec
ZDOT = -16414
523112 ZDOT = -5003
146644
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 12357
53830648
00016717 00000-0 10270-3 0 9035
2 25544 51
6476 265
8655 0017234 71
7558 288
5468 15
52031961 7278
Satellite: ISS
Catalog Number: 25544
Epoch time: 12357
53830648 = yrday
fracday
Element set: 903
Inclination: 51
6476 deg
RA of node: 265
8655 deg
Eccentricity:
0017234
Arg of perigee: 71
7558 deg
Mean anomaly: 288
5468 deg
Mean motion: 15
52031961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 727
Checksum: 337
Coasting Arc #5 (Orbit 741)
---------------------------------------
Vector Time (GMT): 2012/358/11:42:01
546
Vector Time (MET): N/A
Weight (LBS) : 890688
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4141164
52 A = 6784239
50 meter
Y = 1011297
18 meter E =
0030521
Z = -5304103
90 I = 51
28050
XDOT = -1491
839421 Wp = 81
01390
YDOT = -7490
357388 meter/sec RA = 260
29987 deg
ZDOT = -260
005111 TA = 186
46700
MA = 186
50648
Ha = 230
483 n
mi
Hp = 212
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13586497
78 X = -4126399
08
Y = 3317904
13 feet Y = 965071
08 meter
Z = -17401915
67 Z = -5324185
59
XDOT = -4894
486290 XDOT = -1406
706742
YDOT = -24574
663345 feet/sec YDOT = -7506
564044 meter/sec
ZDOT = -853
035141 ZDOT = -267
046248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2634312
41 X = -802938
42
Y = -13629088
67 feet Y = -4154146
23 meter
Z = -17485320
10 Z = -5329525
57
XDOT = 23795
727052 XDOT = 7252
937606
YDOT = -3454
537561 feet/sec YDOT = -1052
943049 meter/sec
ZDOT = -881
320786 ZDOT = -268
626576
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 12358
50412634
00016717 00000-0 10270-3 0 9045
2 25544 51
6482 261
0656 0015916 74
5342 285
7566 15
51779824 7422
Satellite: ISS
Catalog Number: 25544
Epoch time: 12358
50412634 = yrday
fracday
Element set: 904
Inclination: 51
6482 deg
RA of node: 261
0656 deg
Eccentricity:
0015916
Arg of perigee: 74
5342 deg
Mean anomaly: 285
7566 deg
Mean motion: 15
51779824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 742
Checksum: 321
Coasting Arc #6 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2012/359/11:42:01
546
Vector Time (MET): N/A
Weight (LBS) : 890688
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4291700
42 A = 6784199
89 meter
Y = -179244
95 meter E =
0018836
Z = 5235890
51 I = 51
28690
XDOT = 1306
064245 Wp = 75
18128
YDOT = 7523
557126 meter/sec RA = 255
29980 deg
ZDOT = -805
806774 TA = 22
58943
MA = 22
50662
Ha = 230
199 n
mi
Hp = 212
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14080381
96 X = 4267951
00
Y = -588073
99 feet Y = -131385
77 meter
Z = 17178118
47 Z = 5256681
72
XDOT = 4284
987679 XDOT = 1225
751608
YDOT = 24683
586372 feet/sec YDOT = 7537
713378 meter/sec
ZDOT = -2643
723011 ZDOT = -799
656316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 123638
28 X = 37684
95
Y = 13986314
55 feet Y = 4263028
67 meter
Z = 17264369
67 Z = 5262179
88
XDOT = -23792
417393 XDOT = -7251
928821
YDOT = 3472
218705 feet/sec YDOT = 1058
332261 meter/sec
ZDOT = -2619
127672 ZDOT = -798
310114
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 12359
53451085
00016717 00000-0 10270-3 0 9053
2 25544 51
6479 255
9475 0015731 78
0968 282
1946 15
51845664 7583
Satellite: ISS
Catalog Number: 25544
Epoch time: 12359
53451085 = yrday
fracday
Element set: 905
Inclination: 51
6479 deg
RA of node: 255
9475 deg
Eccentricity:
0015731
Arg of perigee: 78
0968 deg
Mean anomaly: 282
1946 deg
Mean motion: 15
51845664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 758
Checksum: 350
Coasting Arc #7 (Orbit 772)
---------------------------------------
Vector Time (GMT): 2012/360/11:42:01
546
Vector Time (MET): N/A
Weight (LBS) : 890688
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4515658
41 A = 6785150
13 meter
Y = -601506
21 meter E =
0028378
Z = -5053371
68 I = 51
29920
XDOT = -1066
960276 Wp = 91
74078
YDOT = -7342
945804 meter/sec RA = 250
30097 deg
ZDOT = 1835
602324 TA = 196
13528
MA = 196
22583
Ha = 230
370 n
mi
Hp = 212
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14815152
25 X = -4484048
50
Y = -1973445
58 feet Y = -651825
84 meter
Z = -16579303
42 Z = -5075231
82
XDOT = -3500
525839 XDOT = -993
687545
YDOT = -24091
029540 feet/sec YDOT = -7354
467729 meter/sec
ZDOT = 6022
317336 ZDOT = 1830
596267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2208710
47 X = 673214
95
Y = -14679663
18 feet Y = -4474361
34 meter
Z = -16669901
39 Z = -5080985
94
XDOT = 23073
415294 XDOT = 7032
776981
YDOT = -3314
442271 feet/sec YDOT = -1010
242004 meter/sec
ZDOT = 6002
438484 ZDOT = 1829
543250
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 12360
50047981
00016717 00000-0 10270-3 0 9069
2 25544 51
6485 251
1492 0015791 81
6075 278
6866 15
51836453 7736
Satellite: ISS
Catalog Number: 25544
Epoch time: 12360
50047981 = yrday
fracday
Element set: 906
Inclination: 51
6485 deg
RA of node: 251
1492 deg
Eccentricity:
0015791
Arg of perigee: 81
6075 deg
Mean anomaly: 278
6866 deg
Mean motion: 15
51836453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 773
Checksum: 329
Coasting Arc #8 (Orbit 788)
---------------------------------------
Vector Time (GMT): 2012/361/11:42:01
546
Vector Time (MET): N/A
Weight (LBS) : 890688
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4731644
37 A = 6786535
76 meter
Y = 1385049
83 meter E =
0023406
Z = 4646106
74 I = 51
31526
XDOT = 744
280760 Wp = 77
99631
YDOT = 7088
296637 meter/sec RA = 245
30409 deg
ZDOT = -2854
076867 TA = 40
53040
MA = 40
35633
Ha = 230
141 n
mi
Hp = 212
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15523767
61 X = 4693235
13
Y = 4544126
74 feet Y = 1437746
74 meter
Z = 15243132
36 Z = 4668999
64
XDOT = 2441
866010 XDOT = 678
827025
YDOT = 23255
566395 feet/sec YDOT = 7096
254009 meter/sec
ZDOT = -9363
769249 ZDOT = -2850
619361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4525542
88 X = -1379385
47
Y = 15435572
21 feet Y = 4704762
41 meter
Z = 15337930
27 Z = 4675001
15
XDOT = -22126
097600 XDOT = -6744
034549
YDOT = 2859
063538 feet/sec YDOT = 871
442566 meter/sec
ZDOT = -9350
274452 ZDOT = -2849
963653
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 12361
53082438
00016717 00000-0 10270-3 0 9070
2 25544 51
6480 246
0307 0015716 85
0508 275
2437 15
51899396 7894
Satellite: ISS
Catalog Number: 25544
Epoch time: 12361
53082438 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 246
0307 deg
Eccentricity:
0015716
Arg of perigee: 85
0508 deg
Mean anomaly: 275
2437 deg
Mean motion: 15
51899396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 789
Checksum: 328
Coasting Arc #9 (Orbit 803)
---------------------------------------
Vector Time (GMT): 2012/362/11:42:01
546
Vector Time (MET): N/A
Weight (LBS) : 890688
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4987317
95 A = 6788486
40 meter
Y = -2052520
83 meter E =
0023026
Z = -4144319
33 I = 51
33542
XDOT = -353
230724 Wp = 95
70998
YDOT = -6661
663524 meter/sec RA = 240
31104 deg
ZDOT = 3740
115233 TA = 212
99665
MA = 213
14055
Ha = 230
225 n
mi
Hp = 212
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16362591
71 X = -4943863
55
Y = -6733992
23 feet Y = -2108048
68 meter
Z = -13596848
20 Z = -4168442
01
XDOT = -1158
893452 XDOT = -296
880846
YDOT = -21855
851457 feet/sec YDOT = -6665
298944 meter/sec
ZDOT = 12270
719268 ZDOT = 3738
535349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6433047
77 X = 1960792
96
Y = -16400370
98 feet Y = -4998833
07 meter
Z = -13696680
90 Z = -4174748
34
XDOT = 20632
487233 XDOT = 6288
782109
YDOT = -2107
020023 feet/sec YDOT = -642
219703 meter/sec
ZDOT = 12264
953842 ZDOT = 3738
357931
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 12362
49675498
00016717 00000-0 10270-3 0 9081
2 25544 51
6481 241
2323 0015646 88
6523 271
6421 15
51894825 8041
Satellite: ISS
Catalog Number: 25544
Epoch time: 12362
49675498 = yrday
fracday
Element set: 908
Inclination: 51
6481 deg
RA of node: 241
2323 deg
Eccentricity:
0015646
Arg of perigee: 88
6523 deg
Mean anomaly: 271
6421 deg
Mean motion: 15
51894825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 804
Checksum: 326
Coasting Arc #10 (Orbit 819)
---------------------------------------
Vector Time (GMT): 2012/363/11:42:01
546
Vector Time (MET): N/A
Weight (LBS) : 890688
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5192503
06 A = 6790645
95 meter
Y = 2692906
23 meter E =
0027991
Z = 3424640
48 I = 51
35850
XDOT = -168
463537 Wp = 91
06846
YDOT = 6169
264026 meter/sec RA = 235
32160 deg
ZDOT = -4563
815322 TA = 48
62506
MA = 48
38471
Ha = 230
108 n
mi
Hp = 212
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17035771
18 X = 5145368
55
Y = 8834994
20 feet Y = 2750708
11 meter
Z = 11235697
10 Z = 3449750
97
XDOT = -552
701894 XDOT = -215
267289
YDOT = 20240
367541 feet/sec YDOT = 6167
118991 meter/sec
ZDOT = -14973
147383 ZDOT = -4564
746678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8224949
20 X = -2506964
52
Y = 17270782
60 feet Y = 5264134
54 meter
Z = 11339567
48 Z = 3456300
17
XDOT = -18983
423539 XDOT = -5786
147495
YDOT = 861
420753 feet/sec YDOT = 262
561046 meter/sec
ZDOT = -14977
734104 ZDOT = -4565
213355
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 12363
52706074
00016717 00000-0 10270-3 0 9092
2 25544 51
6476 236
1132 0015695 92
2506 268
0443 15
51938041 8203
Satellite: ISS
Catalog Number: 25544
Epoch time: 12363
52706074 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 236
1132 deg
Eccentricity:
0015695
Arg of perigee: 92
2506 deg
Mean anomaly: 268
0443 deg
Mean motion: 15
51938041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 820
Checksum: 299
Coasting Arc #11 (Orbit 834)
---------------------------------------
Vector Time (GMT): 2012/364/11:42:01
546
Vector Time (MET): N/A
Weight (LBS) : 890688
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5391528
12 A = 6792597
04 meter
Y = -3175376
33 meter E =
0019507
Z = -2658636
78 I = 51
38290
XDOT = 749
005020 Wp = 86
64091
YDOT = -5582
208081 meter/sec RA = 230
33650 deg
ZDOT = 5182
397026 TA = 243
32575
MA = 243
52563
Ha = 230
067 n
mi
Hp = 212
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17688740
54 X = -5342704
81
Y = -10417901
35 feet Y = -3235394
51 meter
Z = -8722561
61 Z = -2684709
95
XDOT = 2457
365552 XDOT = 786
196223
YDOT = -18314
330973 feet/sec YDOT = -5573
624829 meter/sec
ZDOT = 17002
614914 ZDOT = 5186
125362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9471832
49 X = 2887014
54
Y = -18160835
54 feet Y = -5535422
67 meter
Z = -8830386
93 Z = -2691501
94
XDOT = 17087
548993 XDOT = 5208
284933
YDOT = 690
804299 feet/sec YDOT = 210
557150 meter/sec
ZDOT = 17018
731342 ZDOT = 5187
309313
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 12364
49295342
00016717 00000-0 10270-3 0 9102
2 25544 51
6472 231
3142 0015494 95
7109 264
5810 15
51951279 8354
Satellite: ISS
Catalog Number: 25544
Epoch time: 12364
49295342 = yrday
fracday
Element set: 910
Inclination: 51
6472 deg
RA of node: 231
3142 deg
Eccentricity:
0015494
Arg of perigee: 95
7109 deg
Mean anomaly: 264
5810 deg
Mean motion: 15
51951279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 835
Checksum: 310
Coasting Arc #12 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2012/365/11:42:01
546
Vector Time (MET): N/A
Weight (LBS) : 890688
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5480714
34 A = 6794353
34 meter
Y = 3614252
70 meter E =
0029264
Z = 1703792
08 I = 51
40868
XDOT = -1477
013766 Wp = 107
27586
YDOT = 4948
720506 meter/sec RA = 225
35579 deg
ZDOT = -5674
327796 TA = 53
97741
MA = 53
70654
Ha = 230
061 n
mi
Hp = 212
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17981346
25 X = 5431615
16
Y = 11857784
44 feet Y = 3675266
80 meter
Z = 5589869
03 Z = 1730297
77
XDOT = -4845
845689 XDOT = -1504
677475
YDOT = 16235
959665 feet/sec YDOT = 4932
049435 meter/sec
ZDOT = -18616
561012 ZDOT = -5681
569706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10572322
49 X = -3222443
90
Y = 18732984
12 feet Y = 5709813
56 meter
Z = 5699456
41 Z = 1737194
31
XDOT = -15160
043800 XDOT = -4620
781350
YDOT = -2811
860701 feet/sec YDOT = -857
055142 meter/sec
ZDOT = -18647
179585 ZDOT = -5683
660337
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 12365
52322083
00016717 00000-0 10270-3 0 9111
2 25544 51
6468 226
1946 0015601 99
7759 260
5156 15
51966781 8519
Satellite: ISS
Catalog Number: 25544
Epoch time: 12365
52322083 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 226
1946 deg
Eccentricity:
0015601
Arg of perigee: 99
7759 deg
Mean anomaly: 260
5156 deg
Mean motion: 15
51966781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 324
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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