[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 17th 2012
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) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 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
333/20:57:54
424 0
2 2
5 2
5
N/A -1
6 -0
1 228
4
000/00:05:48
847 -1
9 -0
1 218
3
Coasting Arc #1 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2012/321/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2219919
60 A = 6795592
71 meter
Y = -6143307
21 meter E =
0001958
Z = 1877171
83 I = 52
01266
XDOT = 4060
406193 Wp = 290
89574
YDOT = -3193
352339 meter/sec RA = 83
10122 deg
ZDOT = -5652
979006 TA = 228
59005
MA = 228
60688
Ha = 225
743 n
mi
Hp = 219
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7283200
78 X = -2160177
88
Y = -20155207
39 feet Y = -6167797
84 meter
Z = 6158700
25 Z = 1866532
07
XDOT = 13321
542629 XDOT = 4123
274465
YDOT = -10476
877752 feet/sec YDOT = -3147
594418 meter/sec
ZDOT = -18546
519050 ZDOT = -5633
100951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11805838
60 X = 3598419
61
Y = -17900619
05 feet Y = -5456108
69 meter
Z = 6115308
66 Z = 1863946
08
XDOT = 15119
539941 XDOT = 4608
435774
YDOT = 3668
572896 feet/sec YDOT = 1118
181019 meter/sec
ZDOT = -18463
728657 ZDOT = -5627
744495
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 12321
73385872
00016717 00000-0 10270-3 0 9009
2 25544 51
6481 83
7153 0015883 293
3664 66
5816 15
51471244 1717
Satellite: ISS
Catalog Number: 25544
Epoch time: 12321
73385872 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 83
7153 deg
Eccentricity:
0015883
Arg of perigee: 293
3664 deg
Mean anomaly: 66
5816 deg
Mean motion: 15
51471244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 171
Checksum: 310
Coasting Arc #2 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2012/322/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2181136
97 A = 6796697
50 meter
Y = 6335963
29 meter E =
0016894
Z = -1069796
65 I = 52
01101
XDOT = -4211
610583 Wp = 331
05589
YDOT = 2453
965207 meter/sec RA = 78
16657 deg
ZDOT = 5922
502276 TA = 17
40508
MA = 17
34725
Ha = 226
139 n
mi
Hp = 219
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7155961
17 X = 2115321
68
Y = 20787281
14 feet Y = 6359986
20 meter
Z = -3509831
52 Z = -1059360
15
XDOT = -13817
620024 XDOT = -4267
508814
YDOT = 8051
066953 feet/sec YDOT = 2406
555447 meter/sec
ZDOT = 19430
781745 ZDOT = 5901
906604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12084572
05 X = -3683377
56
Y = 18373312
88 feet Y = 5600185
77 meter
Z = -3467311
19 Z = -1056836
45
XDOT = -13545
213720 XDOT = -4128
581142
YDOT = -5242
929435 feet/sec YDOT = -1598
044892 meter/sec
ZDOT = 19345
093366 ZDOT = 5896
384458
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 12322
70005529
00016717 00000-0 10270-3 0 9016
2 25544 51
6477 78
9182 0015881 297
3772 62
5763 15
51436806 1860
Satellite: ISS
Catalog Number: 25544
Epoch time: 12322
70005529 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 78
9182 deg
Eccentricity:
0015881
Arg of perigee: 297
3772 deg
Mean anomaly: 62
5763 deg
Mean motion: 15
51436806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 186
Checksum: 320
Coasting Arc #3 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2012/323/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2144014
46 A = 6796916
49 meter
Y = -6445135
89 meter E =
0004231
Z = 247754
20 I = 52
00583
XDOT = 4407
684872 Wp = 267
20167
YDOT = -1694
572857 meter/sec RA = 73
23265 deg
ZDOT = -6028
699639 TA = 270
14727
MA = 270
19575
Ha = 226
240 n
mi
Hp = 219
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7034168
19 X = -2072987
80
Y = -21145458
94 feet Y = -6468714
47 meter
Z = 812841
87 Z = 237510
83
XDOT = 14460
908372 XDOT = 4455
592667
YDOT = -5559
622235 feet/sec YDOT = -1645
015248 meter/sec
ZDOT = -19779
198291 ZDOT = -6007
170820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12133106
74 X = 3698170
94
Y = -18693949
04 feet Y = -5697915
67 meter
Z = 771140
56 Z = 235043
64
XDOT = 12080
647533 XDOT = 3682
181368
YDOT = 7041
278379 feet/sec YDOT = 2146
181650 meter/sec
ZDOT = -19689
724607 ZDOT = -6001
428060
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 12323
73064705
00016717 00000-0 10270-3 0 9022
2 25544 51
6482 73
8015 0015792 301
4471 58
5136 15
51511634 2020
Satellite: ISS
Catalog Number: 25544
Epoch time: 12323
73064705 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 73
8015 deg
Eccentricity:
0015792
Arg of perigee: 301
4471 deg
Mean anomaly: 58
5136 deg
Mean motion: 15
51511634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 202
Checksum: 276
Coasting Arc #4 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2012/324/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2050745
17 A = 6796878
25 meter
Y = 6439306
92 meter E =
0017574
Z = 608814
49 I = 51
99517
XDOT = -4681
853365 Wp = 351
46239
YDOT = 926
940171 meter/sec RA = 68
29794 deg
ZDOT = 6005
421164 TA = 15
07607
MA = 15
02375
Ha = 226
634 n
mi
Hp = 219
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6728166
57 X = 1975629
57
Y = 21126335
05 feet Y = 6461819
63 meter
Z = 1997422
86 Z = 618594
70
XDOT = -15360
411303 XDOT = -4721
043862
YDOT = 3041
142292 feet/sec YDOT = 874
365486 meter/sec
ZDOT = 19702
825340 ZDOT = 5982
581568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12001152
52 X = -3657951
29
Y = 18638726
25 feet Y = 5681083
76 meter
Z = 2037198
70 Z = 620938
16
XDOT = -10851
096132 XDOT = -3307
414101
YDOT = -9116
256166 feet/sec YDOT = -2778
634879 meter/sec
ZDOT = 19608
005070 ZDOT = 5976
519945
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 12324
76122359
00016717 00000-0 10270-3 0 9037
2 25544 51
6477 68
6842 0015827 306
0543 53
9142 15
51481633 2182
Satellite: ISS
Catalog Number: 25544
Epoch time: 12324
76122359 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 68
6842 deg
Eccentricity:
0015827
Arg of perigee: 306
0543 deg
Mean anomaly: 53
9142 deg
Mean motion: 15
51481633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 218
Checksum: 303
Coasting Arc #5 (Orbit 232)
---------------------------------------
Vector Time (GMT): 2012/325/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1930488
85 A = 6795950
26 meter
Y = -6356230
44 meter E =
0007801
Z = -1438006
32 I = 51
98111
XDOT = 4984
668041 Wp = 294
70506
YDOT = -193
228005 meter/sec RA = 63
36192 deg
ZDOT = -5809
817242 TA = 260
87337
MA = 260
96164
Ha = 226
723 n
mi
Hp = 218
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6333624
83 X = -1852283
09
Y = -20853774
41 feet Y = -6377381
09 meter
Z = -4717868
50 Z = -1447194
74
XDOT = 16353
897772 XDOT = 5014
681337
YDOT = -633
950149 feet/sec YDOT = -137
318454 meter/sec
ZDOT = -19061
080191 ZDOT = -5785
528814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11739355
83 X = 3578155
66
Y = -18352892
22 feet Y = -5593961
55 meter
Z = -4755193
59 Z = -1449383
00
XDOT = 9857
170118 XDOT = 3004
465452
YDOT = 11241
195275 feet/sec YDOT = 3426
316320 meter/sec
ZDOT = -18960
340156 ZDOT = -5779
111679
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 12325
72736979
00016717 00000-0 10270-3 0 9044
2 25544 51
6482 63
8869 0015767 309
2778 50
6974 15
51547731 2338
Satellite: ISS
Catalog Number: 25544
Epoch time: 12325
72736979 = yrday
fracday
Element set: 904
Inclination: 51
6482 deg
RA of node: 63
8869 deg
Eccentricity:
0015767
Arg of perigee: 309
2778 deg
Mean anomaly: 50
6974 deg
Mean motion: 15
51547731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 233
Checksum: 346
Coasting Arc #6 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2012/326/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1715061
96 A = 6794669
59 meter
Y = 6163936
43 meter E =
0015289
Z = 2257960
30 I = 51
96161
XDOT = -5345
655172 Wp = 6
24309
YDOT = -514
644742 meter/sec RA = 58
42331 deg
ZDOT = 5476
583741 TA = 18
75226
MA = 18
69600
Ha = 227
042 n
mi
Hp = 218
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5626843
69 X = 1635039
26
Y = 20222888
56 feet Y = 6182667
89 meter
Z = 7408006
24 Z = 2266097
74
XDOT = -17538
238752 XDOT = -5366
107333
YDOT = -1688
467000 feet/sec YDOT = -574
537571 meter/sec
ZDOT = 17967
794425 ZDOT = 5450
564793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11429815
69 X = -3483807
82
Y = 17592502
70 feet Y = 5362194
82 meter
Z = 7440988
53 Z = 2268013
31
XDOT = -9162
443020 XDOT = -2792
712632
YDOT = -13491
310585 feet/sec YDOT = -4112
151466 meter/sec
ZDOT = 17859
966780 ZDOT = 5443
717875
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 12326
75791204
00016717 00000-0 10270-3 0 9051
2 25544 51
6475 58
7693 0015804 313
9236 46
0610 15
51546711 2491
Satellite: ISS
Catalog Number: 25544
Epoch time: 12326
75791204 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 58
7693 deg
Eccentricity:
0015804
Arg of perigee: 313
9236 deg
Mean anomaly: 46
0610 deg
Mean motion: 15
51546711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 306
Coasting Arc #7 (Orbit 263)
---------------------------------------
Vector Time (GMT): 2012/327/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1454540
94 A = 6792877
73 meter
Y = -5919103
39 meter E =
0011984
Z = -3005635
32 I = 51
93979
XDOT = 5699
689256 Wp = 326
62281
YDOT = 1139
900481 meter/sec RA = 53
48191 deg
ZDOT = -4983
957404 TA = 247
55105
MA = 247
67802
Ha = 227
179 n
mi
Hp = 218
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4772115
96 X = -1373643
26
Y = -19419630
54 feet Y = -5934916
64 meter
Z = -9861008
26 Z = -3012505
03
XDOT = 18699
767899 XDOT = 5710
730342
YDOT = 3739
830974 feet/sec YDOT = 1203
699713 meter/sec
ZDOT = -16351
566287 ZDOT = -4956
241327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11121953
34 X = 3389971
38
Y = -16602689
80 feet Y = -5060499
85 meter
Z = -9888754
74 Z = -3014092
44
XDOT = 8746
750792 XDOT = 2666
009641
YDOT = 15567
548630 feet/sec YDOT = 4744
988822 meter/sec
ZDOT = -16236
782546 ZDOT = -4948
971320
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 12327
72402781
00016717 00000-0 10270-3 0 9069
2 25544 51
6480 53
9720 0015836 317
1263 42
8653 15
51592590 2640
Satellite: ISS
Catalog Number: 25544
Epoch time: 12327
72402781 = yrday
fracday
Element set: 906
Inclination: 51
6480 deg
RA of node: 53
9720 deg
Eccentricity:
0015836
Arg of perigee: 317
1263 deg
Mean anomaly: 42
8653 deg
Mean motion: 15
51592590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 264
Checksum: 303
Coasting Arc #8 (Orbit 279)
---------------------------------------
Vector Time (GMT): 2012/328/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1069211
53 A = 6790854
45 meter
Y = 5586810
66 meter E =
0011444
Z = 3697844
20 I = 51
91360
XDOT = -6072
743799 Wp = 8
38106
YDOT = -1715
571016 meter/sec RA = 48
53604 deg
ZDOT = 4357
164261 TA = 35
44600
MA = 35
37000
Ha = 227
442 n
mi
Hp = 218
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3507911
86 X = 988695
56
Y = 18329431
29 feet Y = 5598317
03 meter
Z = 12132034
76 Z = 3702842
94
XDOT = -19923
700129 XDOT = -6074
275087
YDOT = -5628
513831 feet/sec YDOT = -1783
488829 meter/sec
ZDOT = 14295
158337 ZDOT = 4327
658873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10924736
83 X = -3329859
79
Y = 15114147
32 feet Y = 4606792
10 meter
Z = 12152054
99 Z = 3703946
36
XDOT = -8600
431013 XDOT = -2621
411373
YDOT = -17587
337189 feet/sec YDOT = -5360
620375 meter/sec
ZDOT = 14173
032980 ZDOT = 4319
940452
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 12328
75453678
00016717 00000-0 10270-3 0 9075
2 25544 51
6473 48
8541 0015894 321
4714 38
5302 15
51608439 2800
Satellite: ISS
Catalog Number: 25544
Epoch time: 12328
75453678 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 48
8541 deg
Eccentricity:
0015894
Arg of perigee: 321
4714 deg
Mean anomaly: 38
5302 deg
Mean motion: 15
51608439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 280
Checksum: 319
Coasting Arc #9 (Orbit 294)
---------------------------------------
Vector Time (GMT): 2012/329/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -639453
24 A = 6788846
37 meter
Y = -5240700
67 meter E =
0015961
Z = -4276864
70 I = 51
88648
XDOT = 6392
272023 Wp = 354
74528
YDOT = 2177
502081 meter/sec RA = 43
58691 deg
ZDOT = -3607
415033 TA = 238
38810
MA = 238
54396
Ha = 227
598 n
mi
Hp = 218
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2097943
70 X = -560026
63
Y = -17193899
83 feet Y = -5247407
25 meter
Z = -14031708
33 Z = -4279778
37
XDOT = 20972
021074 XDOT = 6384
972014
YDOT = 7144
035699 feet/sec YDOT = 2248
943716 meter/sec
ZDOT = -11835
351159 ZDOT = -3576
378713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10850251
88 X = 3307156
77
Y = -13490118
33 feet Y = -4111788
07 meter
Z = -14043117
16 Z = -4280342
11
XDOT = 8677
291519 XDOT = 2644
838455
YDOT = 19222
554449 feet/sec YDOT = 5859
034596 meter/sec
ZDOT = -11706
943364 ZDOT = -3568
276337
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 12329
72062289
00016717 00000-0 10270-3 0 9088
2 25544 51
6475 44
0570 0015931 325
0067 35
0037 15
51640211 2952
Satellite: ISS
Catalog Number: 25544
Epoch time: 12329
72062289 = yrday
fracday
Element set: 908
Inclination: 51
6475 deg
RA of node: 44
0570 deg
Eccentricity:
0015931
Arg of perigee: 325
0067 deg
Mean anomaly: 35
0037 deg
Mean motion: 15
51640211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 295
Checksum: 284
Coasting Arc #10 (Orbit 310)
---------------------------------------
Vector Time (GMT): 2012/330/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 72451
81 A = 6786949
33 meter
Y = 4838685
02 meter E =
0010263
Z = 4755557
58 I = 51
85702
XDOT = -6677
692505 Wp = 350
98277
YDOT = -2582
404532 meter/sec RA = 38
63227 deg
ZDOT = 2739
955342 TA = 72
04329
MA = 71
93144
Ha = 227
857 n
mi
Hp = 217
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 237702
77 X = -4762
70
Y = 15874950
86 feet Y = 4839063
33 meter
Z = 15602223
03 Z = 4755722
17
XDOT = -21908
439976 XDOT = -6661
629583
YDOT = -8472
455813 feet/sec YDOT = -2656
988946 meter/sec
ZDOT = 8989
354798 ZDOT = 2707
553631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11025969
68 X = -3360715
56
Y = 11423524
25 feet Y = 3481890
19 meter
Z = 15602276
01 Z = 4755573
73
XDOT = -8895
080366 XDOT = -2711
220496
YDOT = -20632
338627 feet/sec YDOT = -6288
736813 meter/sec
ZDOT = 8855
344947 ZDOT = 2699
109140
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 12330
75109961
00016717 00000-0 10270-3 0 9093
2 25544 51
6469 38
9388 0016038 329
0157 31
0047 15
51656683 3113
Satellite: ISS
Catalog Number: 25544
Epoch time: 12330
75109961 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 38
9388 deg
Eccentricity:
0016038
Arg of perigee: 329
0157 deg
Mean anomaly: 31
0047 deg
Mean motion: 15
51656683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 311
Checksum: 310
Coasting Arc #11 (Orbit 325)
---------------------------------------
Vector Time (GMT): 2012/331/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 515466
04 A = 6785529
04 meter
Y = -4466348
67 meter E =
0018147
Z = -5091637
35 I = 51
82799
XDOT = 6865
323752 Wp = 17
30897
YDOT = 2868
365704 meter/sec RA = 33
67490 deg
ZDOT = -1805
853916 TA = 235
14705
MA = 235
31782
Ha = 227
992 n
mi
Hp = 217
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1691161
54 X = 590105
94
Y = -14653374
90 feet Y = -4460166
80 meter
Z = -16704846
94 Z = -5088952
11
XDOT = 22524
028059 XDOT = 6841
511455
YDOT = 9410
648636 feet/sec YDOT = 2945
004997 meter/sec
ZDOT = -5924
717573 ZDOT = -1772
559444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11390579
16 X = 3471848
53
Y = -9392956
61 feet Y = -2862973
17 meter
Z = -16693124
54 Z = -5088064
36
XDOT = 9197
142231 XDOT = 2803
288952
YDOT = 21526
684980 feet/sec YDOT = 6561
333582 meter/sec
ZDOT = -5787
050160 ZDOT = -1763
892889
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 12331
71715615
00016717 00000-0 10270-3 0 9101
2 25544 51
6468 34
1416 0016040 332
7551 27
2758 15
51682197 3265
Satellite: ISS
Catalog Number: 25544
Epoch time: 12331
71715615 = yrday
fracday
Element set: 910
Inclination: 51
6468 deg
RA of node: 34
1416 deg
Eccentricity:
0016040
Arg of perigee: 332
7551 deg
Mean anomaly: 27
2758 deg
Mean motion: 15
51682197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 326
Checksum: 290
Coasting Arc #12 (Orbit 341)
---------------------------------------
Vector Time (GMT): 2012/332/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1231038
86 A = 6784601
05 meter
Y = 4070630
33 meter E =
0013875
Z = 5288107
55 I = 51
79872
XDOT = -6960
632443 Wp = 344
06159
YDOT = -3107
958427 meter/sec RA = 28
71241 deg
ZDOT = 785
519916 TA = 98
52216
MA = 98
36490
Ha = 228
243 n
mi
Hp = 217
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4038841
41 X = -1302154
97
Y = 13355086
38 feet Y = 4056466
09 meter
Z = 17349434
22 Z = 5281954
63
XDOT = -22836
720613 XDOT = -6929
177221
YDOT = -10196
714000 feet/sec YDOT = -3185
620747 meter/sec
ZDOT = 2577
165079 ZDOT = 751
780972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12082843
46 X = -3682850
69
Y = 7041224
60 feet Y = 2146165
26 meter
Z = 17323379
87 Z = 5280166
18
XDOT = -9435
561810 XDOT = -2875
959240
YDOT = -22079
856818 feet/sec YDOT = -6729
940358 meter/sec
ZDOT = 2437
692151 ZDOT = 743
008567
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 12332
74760110
00016717 00000-0 10270-3 0 9116
2 25544 51
6463 29
0232 0016171 336
5608 23
4805 15
51701323 3421
Satellite: ISS
Catalog Number: 25544
Epoch time: 12332
74760110 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 29
0232 deg
Eccentricity:
0016171
Arg of perigee: 336
5608 deg
Mean anomaly: 23
4805 deg
Mean motion: 15
51701323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 342
Checksum: 261
Coasting Arc #13 (Orbit 356)
---------------------------------------
Vector Time (GMT): 2012/333/16:45:07
692
Vector Time (MET): N/A
Weight (LBS) : 905703
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1923276
25 A = 6784391
44 meter
Y = -3741186
89 meter E =
0017416
Z = -5330322
41 I = 51
77088
XDOT = 6930
380049 Wp = 32
08202
YDOT = 3250
529948 meter/sec RA = 23
74857 deg
ZDOT = 233
896256 TA = 240
05961
MA = 240
23266
Ha = 228
373 n
mi
Hp = 217
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6309961
45 X = 1990862
01
Y = -12274235
19 feet Y = -3719301
28 meter
Z = -17487934
41 Z = -5320815
19
XDOT = 22737
467354 XDOT = 6892
380619
YDOT = 10664
468334 feet/sec YDOT = 3327
817302 meter/sec
ZDOT = 767
376167 ZDOT = 267
472311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12943675
40 X = 3945232
26
Y = -4932391
03 feet Y = -1503392
79 meter
Z = -17448011
31 Z = -5318153
85
XDOT = 9582
826605 XDOT = 2920
845549
YDOT = 22113
402579 feet/sec YDOT = 6740
165106 meter/sec
ZDOT = 906
150405 ZDOT = 276
194643
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 12333
71362811
00016717 00000-0 10270-3 0 9121
2 25544 51
6462 24
2257 0016181 340
3395 19
7130 15
51721639 3578
Satellite: ISS
Catalog Number: 25544
Epoch time: 12333
71362811 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 24
2257 deg
Eccentricity:
0016181
Arg of perigee: 340
3395 deg
Mean anomaly: 19
7130 deg
Mean motion: 15
51721639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 357
Checksum: 283
Coasting Arc #14 (Orbit 359)
---------------------------------------
Vector Time (GMT): 2012/333/21:00:48
847
Vector Time (MET): N/A
Weight (LBS) : 905450
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6104462
95 A = 6797530
06 meter
Y = -2963893
69 meter E =
0005630
Z = -454798
46 I = 51
80833
XDOT = 2431
644504 Wp = 22
63336
YDOT = -4091
569600 meter/sec RA = 22
87564 deg
ZDOT = -5993
526400 TA = 162
24743
MA = 162
22775
Ha = 228
422 n
mi
Hp = 218
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20027765
58 X = -6068657
02
Y = -9724060
68 feet Y = -3031957
37 meter
Z = -1492120
92 Z = -484367
47
XDOT = 7977
836300 XDOT = 2506
332278
YDOT = -13423
784777 feet/sec YDOT = -4063
959327 meter/sec
ZDOT = -19663
800524 ZDOT = -5981
532295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22216986
89 X = -6771737
60
Y = -1301784
05 feet Y = -396783
78 meter
Z = -1614319
32 Z = -492044
53
XDOT = 2234
367406 XDOT = 681
035185
YDOT = -13884
530847 feet/sec YDOT = -4232
005002 meter/sec
ZDOT = -19613
518088 ZDOT = -5978
200313
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 12333
90684310
00016717 00000-0 10270-3 0 9134
2 25544 51
6491 23
2668 0014369 339
2167 20
8399 15
51272754 3608
Satellite: ISS
Catalog Number: 25544
Epoch time: 12333
90684310 = yrday
fracday
Element set: 913
Inclination: 51
6491 deg
RA of node: 23
2668 deg
Eccentricity:
0014369
Arg of perigee: 339
2167 deg
Mean anomaly: 20
8399 deg
Mean motion: 15
51272754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 360
Checksum: 306
Coasting Arc #15 (Orbit 375)
---------------------------------------
Vector Time (GMT): 2012/334/21:00:48
847
Vector Time (MET): N/A
Weight (LBS) : 905450
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5987807
99 A = 6796936
12 meter
Y = 2943231
69 meter E =
0022304
Z = 1215402
55 I = 51
77775
XDOT = -3090
548299 Wp = 19
31766
YDOT = 3859
195497 meter/sec RA = 17
92758 deg
ZDOT = 5870
261755 TA = 353
86866
MA = 353
89591
Ha = 228
579 n
mi
Hp = 217
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19645039
33 X = 5948546
89
Y = 9656271
95 feet Y = 3009971
47 meter
Z = 3987541
17 Z = 1244396
38
XDOT = -10139
594157 XDOT = -3161
989750
YDOT = 12661
402549 feet/sec YDOT = 3824
235065 meter/sec
ZDOT = 19259
388959 ZDOT = 5855
074614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21844179
04 X = 6658105
77
Y = 1016423
67 feet Y = 309805
94 meter
Z = 4107355
31 Z = 1251921
90
XDOT = -4272
180310 XDOT = -1302
160558
YDOT = 14112
951517 feet/sec YDOT = 4301
627622 meter/sec
ZDOT = 19195
894746 ZDOT = 5850
908719
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 12334
93755856
00016717 00000-0 10270-3 0 9143
2 25544 51
6487 18
1505 0014502 343
3706 16
6968 15
51291372 3769
Satellite: ISS
Catalog Number: 25544
Epoch time: 12334
93755856 = yrday
fracday
Element set: 914
Inclination: 51
6487 deg
RA of node: 18
1505 deg
Eccentricity:
0014502
Arg of perigee: 343
3706 deg
Mean anomaly: 16
6968 deg
Mean motion: 15
51291372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 376
Checksum: 316
Coasting Arc #16 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2012/335/21:00:48
847
Vector Time (MET): N/A
Weight (LBS) : 905450
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5813015
85 A = 6795809
77 meter
Y = -2932119
95 meter E =
0008945
Z = -1968261
48 I = 51
74566
XDOT = 3738
437076 Wp = 5
76695
YDOT = -3657
837642 meter/sec RA = 12
97673 deg
ZDOT = -5585
459212 TA = 195
85679
MA = 195
88481
Ha = 228
695 n
mi
Hp = 217
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19071574
30 X = -5770234
75
Y = -9619816
12 feet Y = -2996885
34 meter
Z = -6457550
78 Z = -1996397
52
XDOT = 12265
213505 XDOT = 3806
195129
YDOT = -12000
779666 feet/sec YDOT = -3615
652724 meter/sec
ZDOT = -18324
997414 ZDOT = -5567
133608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21307865
65 X = -6494637
45
Y = -851863
43 feet Y = -259647
97 meter
Z = -6573808
66 Z = -2003696
88
XDOT = 6216
212020 XDOT = 1894
701424
YDOT = -14503
415053 feet/sec YDOT = -4420
640908 meter/sec
ZDOT = -18248
515028 ZDOT = -5562
147381
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 12335
90383884
00016717 00000-0 10270-3 0 9150
2 25544 51
6493 13
3542 0014437 346
5896 13
4870 15
51318434 3919
Satellite: ISS
Catalog Number: 25544
Epoch time: 12335
90383884 = yrday
fracday
Element set: 915
Inclination: 51
6493 deg
RA of node: 13
3542 deg
Eccentricity:
0014437
Arg of perigee: 346
5896 deg
Mean anomaly: 13
4870 deg
Mean motion: 15
51318434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 313
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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